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Design Guidelines FOR THE TYPE 2A & 2B LIMITED S P ACE CRITICAL POWER DISTRIBUTION SYSTEM (CPDS) Contract Number CONTRACTOR EYP/MCF 54 State Street  Albany, New York Design Guidelines developed for U.S. DE P ARTMENT OF TRA NSPORTA TION FEDERAL AVIATION ADMINISTRATION July 11, 2008
Transcript
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Design Guide

F O R T H E

TYPE 2A & 2B LIMITCRITICAL PO

DISTRIBUTION SYST

Contract Number

CONTRACTOR

EYP/MCF

54 State Street Albany, New York

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July 11, 2008 Design Guidel

FAA Pow

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

Table of Contents

Table of Contents...............................................

SECTION 1 GENERAL INFORMATION..........

1.1 PURPOSE ..........................................................

1.2 ORGANIZATION.................................................

1.3 USE ....................................................................

1.4 RESPONSIBILITIES ...........................................

1.5 SUBMITTALS .....................................................

1.5.1 Deliverables for Review ..................................

1.5.1.1 Overview ..................................................

1.5.1.2 Schematic Design....................................1.5.1.3 Design Development................................

1.5.1.4 75% Contract Documents ........................

1.5.1.5 95% Contract Documents ........................

1.5.1.6 100% Contract Documents ......................

1.6 FAA DOCUMENTS.............................................

1.6.1 Federal Aviation Administration Orders ..........

1.6.2 Federal Aviation Administration Standards.....

1.6.3 Federal Aviation Administration technical INS

1.6.4 Occupational Safety And Health Administratio

1.6.5 Institute of Electrical and Electronics Enginee

SECTION 2 CPDS DESCRIPTION ...................

2.1 OVERVIEW.........................................................

2.2 SUBSYSTEM DESCRIPTIONS TYPE 2A ..........2.2.1 Engine Generator (GEN).................................

2.2.2 Generator Switchboard (GSH).......................

2.2.3 Service Disconnects (SESH) ..........................

2.2.4 Automatic Transfer Switches (ATS) ................

2.2.5 Essential Switchboard (ESH)..........................

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July 11, 2008 Design Guidel

Table of Contents FAA Pow

2.2.14 Static Transfer Switches (STS)............................

2.2.15 Critical & Essential Panels (CPL & EPL) ..............

2.2.16 Load Bank.............................................................

2.2.17 Electrical Power Monitoring System (EPMS)........

2.2.17.1 Event Criticality ..............................................

2.2.17.2 EPMS Software..............................................

2.2.17.3 EPMS Hardware ............................................

2.2.17.3.1 Aggregating Switch Cabinet ...........

2.2.17.3.2 Workstation.....................................

2.3 SUBSYSTEM DESCRIPTIONS TYPE 2B................2.3.1 Essential Distribution Panels (EDPH)...................

2.3.2 UPS Output Distribution Panels (UDPH) ..............

2.3.3 Critical & Essential Transformers (T-UDPL-CAB,

EDPL) ..................................................................

2.3.4 Essential 480/277V Distribution Panels (EDPH)...

2.3.5 UPS Output 208V Distribution Panel (UDPL) .......

2.3.6 Essential 208V Distribution Panel (EDPL) ............

2.3.7 Static Transfer Switches (STS)............................

2.3.8 Critical Distribution Panels (CDPL) .......................

2.3.9 Critical & Essential Panels (CPL, UPL & EPL) .....

2.3.10 Electrical Power Monitoring System (EPMS)........

2.3.10.1 Event Criticality ..............................................

2.3.10.2 EPMS Software..............................................

2.3.10.3 EPMS Hardware ............................................

2.3.10.3.1 Aggregating Switch Cabinet ...........2.3.10.3.2 Workstation.....................................

2.4 RELATIONSHIP OF UNITS .....................................

SECTION 3 DESIGN IMPLEMENTATION REQUI

3.1 CODES AND STANDARDS.....................................

3.2 DRAWING INFORMATION......................................3.2.1 Grounding .............................................................

3.2.2 Seismic Considerations ........................................

3.2.3 Equipment Layout and Space Allocation ..............

3.2.4 Transient Voltage Surge Suppression .................

3 3 FACILITY LOADS

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

3.5 SUBSYSTEM QUANTITIES ...............................

3.6 GENERAL CPDS DESIGN CRITERIA ...............3.6.1 Breaker Quantities and Sizes..........................

3.6.2 Feeder Circuit Sizing and Location.................

3.6.3 Breaker Trip Settings ......................................

3.6.4 Switchboard or Distribution Panels .................

3.6.5 Load Evaluation and Demand Factors............

3.6.6 Equipment Physical Data................................

3.7 EPMS DESIGN CRITERIA AND EQUIPMENT L3.7.1 EPMS Design Criteria ....................................

3.7.1.1 EPMS System Components ....................

3.7.1.2 EPMS System Design Guidelines............

3.7.1.2.1 Distances Requirments.............

3.7.1.2.2 SER and PQM Connection Qua

3.7.1.2.3 Use of the VDTs ......................

3.7.1.2.4 Adding Breakers .......................

3.7.1.2.5 Powering EPMS Located in Pow3.7.2 EPMS Equipment Locations ...........................

3.7.2.1 Sequence of Events Recorders (SERs)...

3.7.2.2 Video Display Terminals (VDT)................

3.7.2.3 Power Quality Meters (PQM) ...................

3.7.2.4 Global Positioning System (GPS) ............

3.7.2.5 EGX-400 Gateways .................................

3.8 EPMS POINTS SUMMARY ................................3.8.1 Switchgear & I-Line Points..............................

3.8.2 Panelboard Points...........................................

3.8.3 UPS System Points........................................

3.8.4 Automatic Transfer Switches without Mainten

3.8.5 Static Transfer Switch Points ..........................

3.8.6 Generators and Generator Controller Points ..

3.9 STUDY REQUIREMENTS AND ASSUMPTIONS

3.9.1 General ..........................................................

3.9.2 Software Application for Study Calculations ...

3.9.3 Source of Data................................................

3.9.4 Protective Devices ..........................................

Appendix A —Acronyms and Abbreviations

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July 11, 2008 Design Guidel

Table of Contents FAA Pow

 Automatic Transfer Switch ............................................

C.2 Mitsubishi Equipment............................................

Uninterruptible Power Supply........................................

C.3 L–3 Equipment......................................................

Static Transfer Switch ..................................................

C.4 Square D Equipment............................................

Switchboards................................................................

Panelboards.................................................................

I-Line panelboards ........................................................

EPMS .......................................................................

Appendix D —Construction Specifications ........

Appendix E —Drawings ........................................

E 1 Drawing List ..........................................................

Appendix F —Timetable for Scheduling...............

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

SECTION 1 GENERAL INFORMATION

These Design Guidelines were developed to facil2B Limited Space Critical Power Distribution Syst

National Air Space (NAS) Level 10-11 consolidat

(TRACON) facilities as based upon terminal man

2B Limited Space CPDS meets reliability, mainta

requirements regarding critical power distribution

1.1 PURPOSEThe purpose of these Design Guidelines is to pro

information required to incorporate the Type 2A a

facility design.

1.2 ORGANIZATION

These guidelines are organized to facilitate the si

Design Engineer, as follows:

Section 1 – Provides information regarding this d

responsibilities of the Design Engineer, Regional

(PSG); and the applicable FAA standards.

Section 2 – Provides a description of the Type 2A

Section 3 – Provides the requirements for implem

Space CPDS at the intended site.

 Appendix A – Provides a list of acronyms and abb

 Appendix B – Provides a report template for the S

Protective Device Coordination studies. Guideline

also provided. The sample provided is in SKM P

provided in the prototype designs.

 Appendix C – Provides manufacturer’s document

 Appendix D – Provides generic construction spec

equipment and installation requirements.

 Appendix E – Provides electrical drawings for lim

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July 11, 2008 Design Guidel

Section 1 General Information FAA Pow

Size certain CPDS equipment such a

panels, Load Bank, etc.

Size interconnecting feeders between

Determine quantities of CPDS equipm

CPLs and EPL’s

Identify connections of building power sys

CPDS equipment power source.

 Allocate space for CPDS equipment withi

Properly layout CPDS equipment within t Develop a Short Circuit (SC) study.

Develop a Load Flow (LF) study.

Develop a Protective Device Coordination

1.4 RESPONSIBILITIESThe FAA Power Services Group (PSG) CPDS Progra

this Design Guidelines document to the FAA Regiona

the document to the designated Design Engineer.

The Design Engineer shall incorporate the CPDS into

information set forth in this document. All questions r

shall be addressed directly to the CPDS Program Off

The Regional Office shall provide the Design Engine

to implement the CPDS at the intended site. This info

the facility’s critical loads, and a list of applicable stan

specifically mentioned in this document.

The Design Engineer shall submit the Design Packag

responsible Regional Office. This office shall forward

Design Package to the CPDS Program Office for rev

Type 2A and 2B Limited Space CPDS design. Comm

Program Office shall be submitted to the Regional Of

the Design Engineer for disposition. If the CPDS Pro

a meeting shall be arranged with the Design Enginee

CPDS into the facility design.

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

Program Office for review. The CPDS Program O

the change requests with Regional Office and the

Figure below provides a graphic representation o

above. Note: It is not the purpose or intention of t

between the Regional Office and the Design Eng

exchange necessary to support efficient impleme

DESIGN

ENGINEER

FAA

REGIONAL

OFFICE

PROVIDE CLARIFICATION OF DESIGN GUI

SUBMIT QUESTIONS REGARDING USAGE OF D

FORWARD DESIGN GUIDELINES

PROVIDE LIST OF CRITICAL LOADS,

STANDARDS, ETC

SUBMIT DESIGN PACKAGES

FORWARD COMMENTS ON

DESIGN PACKAGES

SUBMIT STUDIES

FORWARD COMMENTS ON STUDIES

SUBMIT CHANGE REQUEST

FORWARD DISPOSITION OFCHANGE REQUEST

F

SUBMIT

SU

F

SUBMIT

Information Flow and Responsi

1.5 SUBMITTALS

In addition to the Design Packages, the Design E

and Voltage Drop study and the Short Circuit and

and Voltage Drop study shall verify proper equipm

piece of equipment. The Short Circuit and Coordi

rating for each piece of equipment and include co

d i ti ll i it b k tti

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July 11, 2008 Design Guidel

Section 1 General Information FAA Pow

1.5.1 DELIVERABLES FOR REVIEW

1.5.1.1 OVERVIEWThe Power Services Office has outlined the following

reviewed for compliance with the standard design. It

contains the appropriate level of information requeste

1.5.1.2 SCHEMATIC DESIGN

The Schematic Design deliverable shall indicate 20%

the following information:

 A single line diagram with equipment nam

Floor plans with room size allocations. T

compartmentalization of rooms with room

power design,

 An acknowledgment letter indicating that

following the current standard with all mo Appendix A, Engineering Acknowledgeme

of TI6480.3, CPDS for additional informat

 A load calculation that identifies the critica

loads as well as assumptions regarding d

Refer to Appendix B, Load Calculations, i

TI6480.3, CPDS for additional information

 A Schedule of the future deliverables.Upon receipt of a deliverable, the Power Services Of

10 business days using overnight delivery. If a confe

the Consulting Firm or Power Services Office, it shall

the request date.

1.5.1.3 DESIGN DEVELOPMENT

The Design Development deliverable shall indicate 4

of the following information:

 A 100% complete single line diagram with

Floor plans with equipment locations. Th

compartmentalization of rooms and equip

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

 A load calculation that identifies the c

loads as well as assumptions regardin

Refer to Appendix B, Load CalculationTI6480.3, CPDS for additional informa

 A cost estimate with Government Fur

and

 A schedule of the future deliverables.

Upon receipt of a deliverable, the Power Services

10 business days using overnight delivery. If a c

the consulting firm or Power Services Office, it shthe request date.

1.5.1.4 75% CONTRACT DOCUMENTS

The 75% Contract Documents deliverable, which

completion, consists of the following information:

100% complete single line diagram w 75% complete floor plans with equipm

compartmentalization of rooms and e

from the standard power design,

Fully developed system block diagram

oil, fire alarm, power monitoring syste

systems,

 An acknowledgment letter indicating tfollowing the current standard with all

 Appendix A, Engineering Acknowledg

of TI6480.3, CPDS for additional infor

 A load calculation that identifies the c

loads and all assumptions regarding d

 Appendix B, Load Calculations, in Vo

CPDS for additional information,  A cost estimate with GFE information

Details of installation along with book

 An inventory of GFE, including contra

prior to requisition, and

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July 11, 2008 Design Guidel

Section 1 General Information FAA Pow

1.5.1.5 95% CONTRACT DOCUMENTS

The 95% Contract Documents deliverable, which shacompletion, consists of the following information:

100% complete single line diagram with e

100% complete floor plans with equipmen

compartmentalization of rooms and equip

from the standard power design.

Fully developed diagrams for ancillary sys

power monitoring systems, and emergenc

 An acknowledgment letter indicating that

following the current standard with all mo

 Appendix A, Engineering Acknowledgeme

of TI6480.3, CPDS for additional informat

 A load calculation that identifies the critica

loads and all assumptions regarding dem

 Appendix B, Load Calculations, in Volume

CPDS for additional information,

 A cost estimate with GFE information,

Details of installation along with book spe

 An inventory of GFE, including contract n

prior to requisition, and

 A schedule of the future deliverables.

Upon receipt of a deliverable, the Power Services Of

10 business days using overnight delivery. If a confe

the consulting firm or Power Services Office, it shall o

the request date.

1.5.1.6 100% CONTRACT DOCUMENTS

The 100% Contract Documents deliverable, which sh

completion plus all comments, consists of the followi

 An acknowledgment letter indicating that

have been incorporated.

All d t b f 95% b i i

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

1.6.1 FEDERAL AVIATION ADMINISTRATION OR

6480.3 CPDS Technical Instruction Manuals/Electrical Draw

6480.7D Airport Traffic Control Tower and Terminal Radar Ap

Revision 8/11/04.

6950.27 Short Circuit Analysis and Protective Device Coordin

1.6.2 FEDERAL AVIATION ADMINISTRATION STA

FAA-STD-019D Lightning Protection, Grounding, Bonding, and Shield

FAA-STD-032 Design Standards For National Airspace System (NA

FAA-C-1217F Electrical Work, Interior

1.6.3 FEDERAL AVIATION ADMINISTRATION TEC

TI 6480.3 Technical Instruction Book Volume 10: Site Procurem

Part 2: Type 2 CPDS IRD, Book 1: Type 2 CPDS Inte

1.6.4 OCCUPATIONAL SAFETY AND HEALTH ADSTANDARDS

OSHA CFR 29 Part 1910 Occupational Safety and Health Stan

1.6.5 INSTITUTE OF ELECTRICAL AND ELECTRO

IEEE 241-1999 IEEE Recommended Practice for Electric Power Sys

IEEE 242-1986 IEEE Recommended Practice for Protection and Coo

Systems (IEEE Buff Book)

IEEE 399-1997 IEEE Recommended Practice for Industrial and Com

Book)IEEE 446-1995 IEEE Recommended Practice for Emergency and Sta

Commercial Applications (IEEE Orange Book)

IEEE 493 1997 IEEE Recommended Practice for the Design of Relia

(IEEE Gold Book)

IEEE books can be obtained from ww

This document is available on CD from the CPDS

included on this CD, refer to www.FAA.gov. In a

drawings are provided in AutoCAD 2005, for editi

preparing the facility design. A sample of the CP

Protection Device Coordination Study in SKM Po

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July 11, 2008 Design Guidel

Section 1 General Information FAA Pow

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

SECTION 2 CPDS DESCRIPTION

The CPDS is a collection of tightly integrated subcomprised of commercial-off-the-shelf (COTS) ite

provided below, the reader is encouraged to refe

clarity.

Subsystem Name Des

Engine Generators with load bank GEN-A1 with LBH

Generator Switchboard GSHA & GSHB

Service Disconnect SESHA & SESHB

 Automatic Transfer Switch ATS-A & ATS-B

Essential Switchboard ESHA & ESHB

Essential Distribution Panels EDPHA & EDPHB

Uninterruptible Power System UPS-A & UPS-B

UPS Output Switchboard USHA & USHB Load Bank Distribution Panel LBDPH

UPS Output 208V Distribution Panel UDPLA & UDPLB

UPS Output Maintenance Distribution Panel UDPLM

Critical & Essential Transformers T-UDPLA, T-EDPL

EDPLB

Essential 208V Distribution Panels EDPLA & EDPLB

Static Transfer Switch STS1 thru STS6

Critical & Essential Panels with TVSS CPL1-6, EPLA1-4

Load Bank for UPS LBHU

Electrical Power Monitoring System EPMS

Subsystem Designations for Type 2A Limited Sp

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

Subsystem Name DesignaEssential Distribution Panels EDPHA1-CAB & EDPH

UPS Output Distribution Panel UDPHA-CAB & UDPH

Critical & Essential Transformers T-EDPHA2-CAB, T-ED

UDPLA-CAB, T-UDPL

CAB, T-EDPHB2-CAB

Essential 480/277V Distribution Panel EDPHA2-CAB & EDPH

UPS Output 208V Distribution Panel UDPLA-CAB & UDPLBEssential 208V Distribution Panels EDPLA-CAB & EDPLB

Static Transfer Switch STS

Critical Distribution Panel CDPL-CAB

Critical & Essential Panels with TVSS UPLA-CAB,CPL1-CAB

CPL3-CAB, UPLB-CAB

Electrical Power Monitoring System EPMS

Subsystem Designations for Type 2B Limited Space

2.1 OVERVIEW

The CPDS utilizes two utility feeders, two standby En

essential distribution switchboards, 2N Uninterruptibl

Static Transfer Switches (STSs), etc to manage pow

essential, and non-essential loads. The Electrical Po

displays electrical power distribution status througho

diagnosis of the system and facilitates maintenance

The CPDS is considered to be in a normal configurat

on line and providing power within specifications, bot

switchboards are active, all circuit breakers and com

positions, and the generators are available. In this c

essential switchboards ESHA and ESHB is powered

utility service disconnect which is fed by separate ind

The CPDS incorporates two independent essential s

sources (2 utilities & 2 generators) to maintain power

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

If either utility feeder fails and both generators do

sized to carry the entire building load. If the build

one generator fails and both utility feeders are sticarry the entire building power without interruptio

carry entire building.

For other essential loads (mechanical, lighting, re

from both Essential Distribution Panels (EDPHA &

the B side panels will carry the load thru automat

loads. If a utility outage occurs and both feeders

powered once the generators have started and co

The CPDS supplies critical loads with filtered and

independent Uninterruptible Power Systems (UP

the UPS-A and UPS-B via the UPS Output Switc

Output Distribution Panels (UDPLA & UDPLB), th

and one or more Critical Power Panels (CPLs).

To provide continuous power to critical loads, the

or bypass power to supply the UPS output USHAthe UPS can switch to battery with no loss of pow

UPS output switchboard (USHA & USHB) feeds a

(UDPLA & UDPLB respectively) via a step down

then feed the Static Transfer Switches which then

For maintenance and redundancy, the CPLs are

the second main breaker is fed by UDPLM which

so both utility services and both generators can b

Each critical panel (CPL) is fed by a STS. The S

alternate source is UDPLB. Like the UPSs, the S

continuous power to the CPLs. If the primary sou

transfer within 4 ms to keep continuous power to

for service, the second main breaker in the CPL,

is “wrapped” around the STS to keep the load up

2.2 SUBSYSTEM DESCRIPTIONS TYPE 2A

The sections below describe the intended use an

subsystems as they apply to the overall CPDS. A

comprising each subsystem is included. The desc

based on the Type 2A Limited Space CPDS The

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

Circuit Monitors (CM), electronic trip units, and speci

also discussed. The hardwired input devices are mo

Hardwired input devices include circuit breakers, certrelays, Transient Voltage Surge Suppressors (TVSS

2.2.1 ENGINE GENERATOR (GEN)

The Type 2A and 2B Limited Space CPDS implemen

standby power is available to both essential switchbo

outage. The generator sizes indicated on drawings a

designer should determine the generator size based protect. Each generator is capable of handling the e

generator fails. When the CPDS is in a normal config

down, but are ready to start when required.

In the event of a utility outage, the A or B ATS autom

respective generator. Once the generator reaches its

 ATS will transfer the load to the generator.

Each generator is supplied with dual breakers and a

generator.

2.2.2 GENERATOR SWITCHBOARD (GSH)

There are two generator switchboards that each feed

generator. The GSHA and GSHB is constructed usin

Each switchboard feeds an Automatic Transfer Switc

there is a loss of utility service, the respective ATS se

respective generator and the generator switchboard f

Each generator switchboard is also provided with UP

needs to be maintained, the generator can feed the c

2.2.3 SERVICE DISCONNECTS (SESH)

There are two main utility service disconnects that ar

feeders. Each feeder only serves one service discon

fused bolted pressure switches with TVSS. If the A s

the loads can be fed from the B side since it is sized

2.2.4 AUTOMATIC TRANSFER SWITCHES (ATS)

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

2.2.5 ESSENTIAL SWITCHBOARD (ESH)

The CPDS implements two ESH’s (ESHA & ESH

services and generator services, if required. Theequipment in the building; critical, essential and n

Power Style QED 2 enclosures.

In a normal configuration, bus A and bus B are in

service disconnects and separate utility feeders.

 ATSs start the generator and both buses are fed

required speed and voltage.

2.2.6 ESSENTIAL DISTRIBUTION PANELS (EDPH

The CPDS utilizes two EDPHs (EDPHA & EDPH

mechanical equipment, receptacles, lights, and o

utilize I-Line type distribution panel construction.

through the essential switchboards, ESHA and E

2.2.7 UNINTERRUPTIBLE POWER SYSTEM (UPS

The CPDS implements 2N independant UPSs to

power from the utility or generator sources to all c

side and each system sized to accommodate ent

UPS consists of a stand alone UPS module with

The UPS sizes indicated on drawings are a typica

should determine the UPS size based on the criti

The batteries are located in a room separate fromcables shall be sized to limit to voltage drop to 2V

Group (PSG) prefers wet cell batteries. Wet cell

space does not allow for wet cells, use sealed VR

accommodate all critical loads only in the CPDS.

the second UPS can protect all the critical loads.

Each UPS receives normal input power from ESH

also supplied by ESHA or ESHB. There also is aavailable from ESHA or ESHB. If the UPS is dow

bypass feature can be utilized to keep the critical

can be connected to the second UPS for “clean”

The UPS has three modes of operation: normal,

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

bypass mode. The UPS uses a static switch to maint

critical loads as the necessary contacts open or close

input source to the loads. While in bypass mode, the power to the critical loads.

2.2.8 UPS OUTPUT SWITCHBOARD (USH)

The CPDS implements two USHs (USHA & USHB) s

from the UPS system to the critical loads via static tra

testing, USHA and USHB are connected to a load ba

USHA and USHB utilize Power Style QED 2 enclosuspecific keyed breakers which allow the UPS to be lo

without impacting any of the critical loads or other CP

If a UPS needs to be tested under load, the appropria

and/or closed and the load bank circuit is operated. T

to be tested while the UPS maintenance bypass feed

loads.

2.2.9 LOAD BANK DISTRIBUTION PANEL (LBDPH)

The CPDS implements one LBDPH to facilitate load

systems using one load bank in lieu individual load b

have specific keyed functions so only one UPS syste

constructed using the I-Line distribution panel enclos

USHA and USHB and the load bank.

2.2.10 UPS OUTPUT 208V DISTRIBUTION PANEL (UD

The CPDS implements two UDPLs to distribute powe

the critical power panels (CPL) via static transfer swi

constructed using the I-Line distribution panel enclos

from USHA and USHB via a 480V-208Y/120V step d

UDPLA and UDPLB feed the primary sides and alter

If UDPLA is down for maintenance, the alternate side

critical loads and vice versa.

2.2.11 UPS OUTPUT 208V MAINTENANCE DISTRIBUT

The CPDS implements one UDPLM to connect UDP

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

UDPLM is constructed using the I-Line distributio

from UDPLA and UDPLB.

2.2.12 ESSENTIAL 208V DISTRIBUTION PANEL (E

The CPDS implements two EDPLs (EDPLA & ED

essential switchboards to the essential loads. All

are constructed using the I-Line distribution pane

ESHA and EDPLB is fed from ESHB. They are a

transformers.

EDPLA and EDPLB feed the primary and alterna

If one side is down for maintenance, the alternate

is fed continuous power.

2.2.13 CRITICAL & ESSENTIAL TRANSFORMERS

The transformers are used to step down the 480V

208Y/120V. The transformers are all located nea

harmonics is an issue at the site, provide a minim

If needed, design engineer shall also provide a 4

any 277V loads in the building. This is not indica

2.2.14 STATIC TRANSFER SWITCHES (STS)

The CPDS implements six STSs to distribute con

(UPS-A) and from side B (UPS-B). Each STS feshall be dispersed through-out the critical facility

Each STS is a 3-phase, two-position switching de

load between two power sources, designated Pri

Programmable Logic Controller (PLC) is built into

transfer.

 A STS has two modes of operation: static and by

static mode, while the bypass mode is only used itself is damaged. When in the static mode, the p

the Silicon Controlled Rectifier (SCR) module. Th

SCR, while the other source is halted. If the PLC

the SCR performs the transfer without causing a

time between power sources is within 4 milliseco

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

needs to be split between UDPLA and UDPLB so the

shared. All STSs provide power to the primary side o

Note that the grounding electrode of T-UDPLA & T-U

indicated on drawings since the static transfer switch

2.2.15 CRITICAL & ESSENTIAL PANELS (CPL & EPL)

The CPDS implements six CPLs and eight EPLs to d

critical loads and the EDPLs for essential loads. The

the EPLs are fed from the essential switchboards ES

panels are fed by the generator. All critical and esse

panelboard construction but with the dual main circui

voltage surge suppressor (TVSS) device connected

primary side of the CPLs is fed from the STS and the

UDPLM. For the A EPLs, the primary side is fed from

fed from EDPLB. For the B EPLs, the layout is rever

EDPLB and the alternate side from EDPLA.

In a normal configuration, the primary feeder powersprimary device is down for scheduled maintenance, t

feed the loads. This is accomplished by transferring

source and using a Kirk key interlock. The tie breake

provide the alternate feed directly to the CPLs. Once

maintenance bypass breaker in the panel and open t

the loads to be maintained in a continuous fashion.

2.2.16 LOAD BANK

The CPDS implements a one load bank for the UPS

generator. Each load bank is supplied with a remote

generator load bank can also be used to prevent und

adding a resistive load to the total facility load, when

resistors generate a large amount of heat, so a safety

cooling blower is running before a load is applied. If 500kW, it is recommended that they be installed outd

Each Load Bank Control Panel allows load to be app

to a total of maximum size of the load bank. The loa

respective generator and UPS. The control panels a

l t d t t th i t th t it i l d t ti

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

equipment out-of-range conditions detected as a

designed to operate in a distributed processing e

processors and other specified components timeusing an external time standard, Global Positionin

IRIG-B time code signal to ensure an accurate se

The EPMS equipment is connected appropriately

equipment using the following connections: RS-4

converter) connections, GPS (RIG-B) time synch

The EPMS communicates with each circuit break

sequence of event recorder, and various gatewaysystem. The visual touch screen displays operate

digital inputs have a one-millisecond timing resolu

communicates serially has a timing resolution of o

are connected to the Power Quality Meter inputs.

to a Sequence of Events recorder.

2.2.17.1 EVENT CRITICALITYThe EPMS system monitors the CPDS equipmen

below:

Criticality 1. Trip condition. This condition causes

power down stream of the tripped circuit breaker.

failure and an alarm sounds.

Criticality 2. Pre-trip condition. This condition indialarm sounds.

Criticality 3. Equipment “out-of-normal” condition.

breaker or other equipment is functioning outside

indicated on the appropriate video display termina

Criticality 4. EPMS Trending Reports. The EPMS

time to determine trends indicating equipment ou

2.2.17.2 EPMS SOFTWARE

The EPMS server software uses a Microsoft Wind

full screen editing to facilitate the programming a

software has an online help system showing all d

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

EPMS software takes incoming monitored data and p

operations for control, viewing, logging or alarms.

The EPMS screens show all parameters that are avaequipment, including metered values, load status, ala

device state, equipment position, equipment status, e

capture, and sag/swell events.

2.2.17.3 EPMS HARDWARE

EPMS hardware components are used in the distribu

maintain in memory a permanent time-stamped even

events for database reconstruction. Each component

connection.

The following paragraphs provide a physical descript

the EPMS hardware.

2.2.17.3.1 AGGREGATING SWITCH CABINET A typical EPMS aggregating switch cabinet is 24 inch

inches deep. Mounted in the aggregating switch cabi

a server monitor, the GPS system, a dedicated UPS

distances are less than 328 feet, Ethernet switches.

to-switch distances are greater than 328 feet, horizon

Connections between the aggregating switches, serv

6 CFCI ¾ inch conduit.

2.2.17.3.2 WORKSTATION

 An operator workstation and video display terminals

interface for operators to perform system monitoring.

access to information provided by the power monitor

display, data logging, alarming, event recording, and

functions. Both the workstation and VDTs can monito

2.3 SUBSYSTEM DESCRIPTIONS TYPE 2B

The sections below describe the intended use and ca

D i G id li T 2A & 2B Li it d S CPDS

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

The CPDS subsystems include various monitorin

data which are managed remotely by the EPMS.

Circuit Monitors (CM), electronic trip units, and spalso discussed. The hardwired input devices are

Hardwired input devices include circuit breakers,

relays, Transient Voltage Surge Suppressors (TV

2.3.1 ESSENTIAL DISTRIBUTION PANELS (EDPH

The Type 2B CPDS utilizes two EDPHs, EDPHA

distribute power to mechanical equipment, receploads located in the Tower. The EDPHs utilize I-L

construction. Normal input power is received fro

ESHB located in the base building.

2.3.2 UPS OUTPUT DISTRIBUTION PANELS (UDP

The Type 2B Tower CPDS implements two UDPH

distribute power from the UPS systems, located iloads located in the tower. Both UDPHA-CAB an

distribution panel enclosures.

2.3.3 CRITICAL & ESSENTIAL TRANSFORMERS T-EDPL)

The transformers are used to step down the 480V

208Y/120V. The transformers are all located neaserve. If harmonics is an issue at the site, provid

transformer. The transformers T-EDPHA2-CAB a

480/277V to feed any 277V loads in the tower.

2.3.4 ESSENTIAL 480/277V DISTRIBUTION PANE

The Type 2B CPDS utilizes two EDPHs (EDPHA

power to all 277V loads which might include mecnon-essential loads located in the tower. The ED

panel construction. Normal input power is receiv

and ESHB located in the base building.

July 11 2008 Design Guidel

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

UDPLA-CAB feeds the primary side of the static swit

maintenance, the alternate side, UDPLB-CAB, of the

UDPLA-CAB also feeds UPLA-CAB which provides cnot fed via a static switch. UDPLB-CAB also feeds U

power in the tower but is not fed via a static switch.

2.3.6 ESSENTIAL 208V DISTRIBUTION PANEL (EDP

The Type 2B CPDS implements two EDPLs (EDPLA

power from the essential switchboards to the essenti

tower. Both essential distribution panels are constru

panel enclosures. EDPLA-CAB is fed from ESHA via

from ESHB via EDPHB1-CAB. They are all fed via 4

transformers.

EDPLA-CAB and EDPLB-CAB feed the primary and

breaker essential panel EPL-CAB. If one side is dow

side will feed the panels so the load is fed continuous

2.3.7 STATIC TRANSFER SWITCHES (STS)

The Type 2B CPDS implements one STS to distribut

side A (UPS-A) and side B (UPS-B). The STS feeds

CDPL. The STS shall be dispersed somewhere in th

STS is a 3-phase, two-position switching device whic

between two power sources, designated Primary andProgrammable Logic Controller (PLC) is built into the

transfer.

 A STS has two modes of operation: static and bypas

static mode, while the bypass mode is only used in th

itself is damaged. When in the static mode, the powe

the Silicon Controlled Rectifier (SCR) module. The se

SCR, while the other source is halted. If the PLC ordthe SCR performs the transfer without causing a sign

time between power sources is within 4 milliseconds

manufacturer. Considering the impact on the critical

short enough to be deemed continuous. When in the

i t d t f l f t

Design Guidelines—Type 2A & 2B Limited Space CPDS

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

2.3.8 CRITICAL DISTRIBUTION PANELS (CDPL)

The Type 2B CPDS implements one CDPL-CAB

automatic static transfer switches to multiple criticGenerally, the critical panels are not fully utilized

so these distribution panels allow additional critic

The distribution panel is constructed using the I-L

CDPL-CAB is fed from STS. This distribution pa

Transfer Switch (STS).

2.3.9 CRITICAL & ESSENTIAL PANELS (CPL, UPThe Type 2B CPDS implements three CPLs, two

power from the STS for critical loads (CPL), the U

and the essential loads (EPL). The CPL-CABs, U

from the UPS and the EPL-CAB is fed from the e

ESHB with no UPS. All critical and essential pan

construction but with the dual main circuit breake

suppressor (TVSS) device connected to each pa

the CPL-CABs is fed from the STS via a CDPL-C

UDPLB-CAB. For the EPL-CAB, the primary side

alternate side is fed from EDPLB-CAB. For the U

from UDPLA-CAB and the secondary side is not

primary side is fed from UDPLB-CAB and the sec

In a normal configuration, the primary feeder pow

primary device is down for scheduled maintenanc

feed the loads. This is accomplished by transferrsource and using a Kirk key interlock, close the m

panel and open the main breaker. This will allow

continuous fashion. The two panels that do not h

power until the primary feeder is back in service.

2.3.10 ELECTRICAL POWER MONITORING SYSTE

The Electrical Power Monitoring System (EPMS) monitors points on switchgear, low-voltage distrib

 ATSs, STSs, generators, and generator controlle

instantaneous events such as equipment failures

report trending events such as equipment degrad

July 11, 2008 Design Guidel

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July 11, 2008 Design Guidel

Section 2 CPDS Description FAA Pow

The EPMS communicates with each circuit breaker,

sequence of event recorder, and various gateways o

system. The visual touch screen displays operate wit

digital inputs have a one-millisecond timing resolution

communicates serially has a timing resolution of one

are connected to the Power Quality Meter inputs. Dis

to a Sequence of Events recorder.

2.3.10.1 EVENT CRITICALITY

The EPMS system monitors the CPDS equipment usbelow:

Criticality 1. Trip condition. This condition causes a c

power down stream of the tripped circuit breaker. Thi

failure and an alarm sounds.

Criticality 2. Pre-trip condition. This condition indicate

alarm sounds.

Criticality 3. Equipment “out-of-normal” condition. Th

breaker or other equipment is functioning outside of i

indicated on the appropriate video display terminal.

Criticality 4. EPMS Trending Reports. The EPMS mo

time to determine trends indicating equipment out-of-

2.3.10.2 EPMS SOFTWAREThe EPMS server software uses a Microsoft Window

full screen editing to facilitate the programming and m

software has an online help system showing all desc

EPMS operation.

The power management servers, workstations, and w

vital system parameters and provide a scaleable sys

replacement of the EPMS system hardware or softwa

Diagnostics provide information on communication fa

mismatches.

EPMS software takes incoming monitored data and p

Design Guidelines—Type 2A & 2B Limited Space CPDS

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g yp p

FAA Power Services Group, CPDS Program Office

2.3.10.3 EPMS HARDWARE

EPMS hardware components are used in the dist

maintain in memory a permanent time-stamped eevents for database reconstruction. Each compon

connection.

The following paragraphs provide a physical desc

the EPMS hardware.

2.3.10.3.1 AGGREGATING SWITCH CABINET

 A typical EPMS aggregating switch cabinet is 24

inches deep. Mounted in the aggregating switch c

a server monitor, the GPS system, a dedicated U

distances are less than 328 feet, Ethernet switch

to-switch distances are greater than 328 feet, hor

Connections between the aggregating switches,

6 CFCI ¾ inch conduit.

2.3.10.3.2 WORKSTATION

 An operator workstation and video display termin

interface for operators to perform system monitor

access to information provided by the power mon

display, data logging, alarming, event recording, a

functions. Both the workstation and VDTs can mo

July 11, 2008 Design Guidel

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Section 2 CPDS Description FAA Pow

2.4 RELATIONSHIP OF UNITS

 A block diagram representing the Type 2A and 2B C

Figure below. This illustration does not include the EP

identified by their respective designations. The illustr

basic interconnections between units, and their relati

Design Guidelines—Type 2A & 2B Limited Space CPDS

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FAA Power Services Group, CPDS Program Office S

SECTION 3 DESIGN IMPLEMENTATION REQ

This section provides the requirements for effectiv2B Limited Space CPDS at the intended site. De

Interface Requirement Document (IRD) for additi

all equipment sizing.

3.1 CODES AND STANDARDS

The Design Engineer shall be familiar with the FA

implementation, as listed in Section 1.6 and as spDesign Engineer is also responsible for ensuring

designed in accordance with all applicable local c

3.2 DRAWING INFORMATION

The Design Engineer shall be familiar with the de

Type 2A and 2B Limited Space CPDS engineerin

briefly described in the sections below.

The CPDS One-Line diagrams are provided in dr

which contains all the components of the Type 2A

incorporated into the facility design. It is noted th

CPDS is 3 wire except there are two panelboards

Design Engineer shall add isolation transformers

wire loads in the base building and step down tra

208Y/120V loads.The reference drawings shall be reviewed by Des

aspects and adapted to each site as applicable.

used by the design engineer to develop equipme

systems, etc.

3.2.1 GROUNDING

The Design Engineer shall employ standard IEEE

CPDS equipment in coordination with FAA STD-0

3.2.2 SEISMIC CONSIDERATIONS

A h i d b i t t th i

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Section 3 Design Implementation Requirements FAA Pow

shown on E120LS is a guide only and exact dimensio

the design engineer. The equipment shall be located

Design Engineer shall use good engineering practice

and recommendations to properly layout equipment.

3.2.4 TRANSIENT VOLTAGE SURGE SUPPRESSION

The designer shall perform a transient analysis to ev

TVSS devices throughout system. Currently, TVSS

main incoming service disconnects and all CPL, EPL

are minimum requirements. Due to facility layout, TV

on the UPS input and output switchboards. Designe

FAA.

3.3 FACILITY LOADS

The sections provided below describe the requireme

essential, and non-essential loads within the facility.

3.3.1 CRITICAL LOADS

 All electronic loads that the FAA has certified as critic

critical power system. The Regional Office will provid

of all the facility’s critical loads. Refer to FAA Order 6

on critical loads.

Critical branch circuit power panels shall be rated as

main breaker, forty two 20A-1-pole bolt-on breakers. shall be connected to STSs via CDPLs as shown on

Line diagram. For panelboard UPLA-CAB and UPLB

panels are not fed by STS but are backed up by UPS

Each critical load shall be connected to the nearest p

drop and shall be properly balanced.

3.3.2 ESSENTIAL LOADS

 All feeders as shown on the CPDS One-Line diagram

essential loads shall be supported by either generato

FAA STD 6480.7C for additional information on esse

Design Guidelines—Type 2A & 2B Limited Space CPDS

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FAA Power Services Group, CPDS Program Office S

power paths. If redundant equipment is not prov

provide automatic transfer switches (ATS) as nec

any essential HVAC equipment components whic

3.4 EQUIPMENT SIZING

The CPDS One-Line diagram shows the maximu

the GENs. If it is determined that smaller sizes ar

load, the Design Engineer shall contact the CPDS

shop drawings. The maximum number of CPDS

Panels, STSs, etc) are also shown on the CPDS

3.4.1 UTILITY TRANSFORMER SIZING

The utility transformers shall be sized using the d

Evaluation and Demand Factors section of this d

sized to carry the entire load if one transformer fa

3.4.2 UPS SIZINGOnce the Regional Office provides a listing of all

the critical power system, each UPS shall be size

demand factor. Each UPS unit shall be of sufficie

carry the total critical load requirements for the fa

UPS should be designed around is 90% red-line.

carry the entire load if one UPS fails.

3.4.3 GENERATOR SIZING

Generators shall be sized to carry the facility’s co

The generator shall be sized based on load analy

electrical demand factors provided in Section 3.6

shall be sized to carry the entire load if one gene

3.4.4 LOAD BANK SIZINGThe Load Banks for the generators and UPSs sh

and UPS ratings respectively.

3 5 SUBSYSTEM QUANTITIES

July 11, 2008 Design Guidel

S ti 3 D i I l t ti R i t FAA P

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Section 3 Design Implementation Requirements FAA Pow

3.6 GENERAL CPDS DESIGN CRITERIA

3.6.1 BREAKER QUANTITIES AND SIZESThe minimum quantity of the breakers are indicated

Design Engineer must allocate each load to the appr

breakers are needed for other loads, add breakers as

additional loading. For I-Line distribution panels, the

mounting space per breaker and the LE frame break

The PJ and LE breakers are used in different areas b

requirements. For QED 2 style breakers, see Sq D s

information.

3.6.2 FEEDER CIRCUIT SIZING AND LOCATION

Feeder circuits between CPDS equipment shall be si

specified by the Regional Office. Where possible, rac

furnished equipment shall be located under slab.

3.6.3 BREAKER TRIP SETTINGS

 Adjustable circuit breakers shall be set to coordinate

load served, and also with upstream/downstream dev

Section 3.9.4 for additional information.

3.6.4 SWITCHBOARD OR DISTRIBUTION PANELS

Designer shall evaluate the use of QED 2 or I-Line eqavailable space in the facility. Single line diagrams in

is the preferred method. Coordinate all requirement

3.6.5 LOAD EVALUATION AND DEMAND FACTORS

The Design Engineer shall evaluate the loads connec

accordance with NEC. As these panels interface wit

shall again evaluate loads at that level, utilizing demato the switchgear, in order not to oversize the utility tr

The following is a brief list of demand factors to be us

Mechanical Load Demand Factors

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group CPDS Program Office S

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FAA Power Services Group, CPDS Program Office S

 All winter heating load – 0% demand

Electrical Load Demand Factors

Lighting – 100% demand

Receptacle – First 10KVA 100% dem

Critical Load – 100% demand (value p

Kitchen Load – 50% demand

Vacuum System – 10% demand

3.6.6 EQUIPMENT PHYSICAL DATAPhysical information (e.g.: size, weight, bus/break

size) of equipment can be found in the manufactu

provided in the Appendix.

3.7 EPMS DESIGN CRITERIA AND EQUIPMENT LO

3.7.1 EPMS DESIGN CRITERIA

3.7.1.1 EPMS SYSTEM COMPONENTS

The following components make up the electrical

Server 

Switch

GPS receiver

Workstation

UPS at EPMS rack (The UPS is sized

monitor, and GPS receiver)

Electrical distribution monitoring devic

Visual Display Terminals (VDT)

3.7.1.2 EPMS SYSTEM DESIGN GUIDELINES

3.7.1.2.1 DISTANCES REQUIRMENTS

The distances with-in the base building may be a

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Section 3 Design Implementation Requirements FAA Pow

change of state (Tripping). Time resolution of 1ms is

SERs and PQMs incorporated in this prototype syste

Each SER has 32 digital inputs and each PQM has 1used to sense either one or both of the dry contact cl

from individual circuit breakers. Within boards contain

PQM is used to pick up tripped conditions. The PQM

triggers to create a wave form capture. UPS bypass c

digital input on the PQM to trigger a wave form captu

3.7.1.2.3 USE OF THE VDTSThe VDTs allow technicians to monitor the EPMS at

There should be a VDT available for each power pat

equipment in the base building. If multiple switchboar

serving the same power path, a single VDT may be u

EPMS interface and can used instead of a VDT in the

3.7.1.2.4 ADDING BREAKERSThe design shown represents the minimum use of m

breakers are added, the quantity of available digital i

mind that the PQM is used to monitor tripping events

capture. If the breakers to be added don't require mo

without impacting the monitoring equipment.

3.7.1.2.5 POWERING EPMS LOCATED IN POWER DISTPower for EPMS equipment located in power distribu

among multiple critical panelboards (CPLs). This arra

system monitoring is available even if one of these cr

service. Each electrical distribution board that contain

dedicated circuit from one of these panelboards.

3.7.2 EPMS EQUIPMENT LOCATIONS

3.7.2.1 SEQUENCE OF EVENTS RECORDERS (SERS)

EPMS sequence of events recorders are connected t

(IRIG-B) Time Synch cable and to the EPMS horizon

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office S

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FAA Power Services Group, CPDS Program Office S

Path B high-voltage essential input sw

Path A high-voltage essential input sw

Path B high-voltage essential input sw

Path A high-voltage UPS switchboard

Path B high-voltage UPS switchboard

Path A high-voltage essential distribu

Path B high-voltage essential distribu

Path A low-voltage essential distributi

Path B low-voltage essential distributi

Low-voltage maintenance switchboar

High-voltage load bank switchboard L

Path A low-voltage critical distribution

Path B low-voltage critical distribution

One wall mounted enclosure in the ba

One wall mounted enclosure in the CA

Each Sequence of Events recorder has 32 digital

a capacity of 8,000 events. The recorders use 10

Modbus TCP as well as RS-232/RS-485 program

3.7.2.2 VIDEO DISPLAY TERMINALS (VDT)EPMS video display terminals are connected by C

horizontal cabinets and are located on the followi

Path A service entrance disconnect S

Path B service entrance disconnect S

Path A high-voltage Generator switch

Path B high-voltage Generator switch

Path A high-voltage essential switchb

Path B high-voltage essential switchb

Path A high-voltage UPS switchboard

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g p q

768 resolution with 256 colors, Windows, a hard drive

connection and is 24 VDC.

3.7.2.3 POWER QUALITY METERS (PQM)

The power quality meters time-synchronize to within

time standard. They are connected to the EPMS Hor

Ethernet cables. In addition, they are connected by R

The PQMs are located on the following equipment:

Path A high-voltage essential switchboard

Path B high-voltage essential switchboard

Path A high-voltage UPS switchboard US

Path B high-voltage UPS switchboard US

Critical panelboards CPL1, CPL2, CLP3,

Critical distribution panelboard UPLA-CA

Each power quality meter has a detection rate of 256

and uses sixteen programmable oscillographic wavevoltage inputs that measure from 0 to 347 voltage roo

neutral) or from 0 to 600 Vrms (line-to-line). PQMs ea

measure up to 20A Vrms (600 Vrms maximum voltag

memory and uses 10/100 BaseT Ethernet to support

485 programmable baud rates. The Ethernet port opt

communication to the meter and gateway capability t

network by way of the meter’s RS-485 ports.

3.7.2.4 GLOBAL POSITIONING SYSTEM (GPS)

The global positioning system (GPS) DCF-77 time sig

the EPMS GPS time synchronization .signal receiver

These time signal converters are located on the follow

Path A high-voltage essential switchboard

Within the EPMS distributed processing environment

components time-synchronize to within one milliseco

3.7.2.5 EGX-400 GATEWAYS

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office S

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Path A high-voltage essential switchb

Path B high-voltage essential switchb

Path A high-voltage UPS switchboard

Path B high-voltage UPS switchboard

Path A low-voltage UPS Critical distri

Path B low-voltage UPS Critical distrib

Path A high-voltage UPS Critical distr

3.8 EPMS POINTS SUMMARYThe EPMS system monitors points for switchgea

switchboards, UPS system, automatic transfer sw

generators, and generator controllers.

3.8.1 SWITCHGEAR & I-LINE POINTS

Switchgear and I-Line panelboards are factory-w

termination section. Metering accuracy class curras required by the manufacturer. Switchgear/I-Lin

conditions:

High-speed sag/swell detection of vol

High-speed voltage transient detectio

Harmonics calculations for all phase c

phase-to-phase voltage up to the 128

Total harmonic distortion up to the 12

and phase-to-neutral or phase-to-pha

K-factors calculation for all phase cur

Bus voltage,

Bus current,

Hard wired protective relays unless th

millisecond time stamp,

Open, closed, tripped, and withdrawn

Circuit breaker serial interface points

chain RS-485 wiring,

July 11, 2008 Design Guidel

Section 3 Design Implementation Requirements FAA Pow

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3.8.2 PANELBOARD POINTS

Lighting and appliance, power distribution, feeder dis

panelboards are factory wired to terminal strips in a dMetering accuracy class CTs are supplied as require

CPL panelboard points monitor the following conditio

Open and closed (hard wired) condition o

Open and closed (hard wired) condition o

breaker.

EPL panelboard points monitor the following conditio

Open and closed (hard wired) condition o

Open and closed (hard wired) condition o

breaker.

3.8.3 UPS SYSTEM POINTS

Serial interface points are available per manufacturer

the UPS system.

Serial interface points monitor the following condition

High-speed sag/swell detection of voltage

High-speed voltage transient detection, c

Harmonics calculations for all phase curre

phase-to-phase voltages up to the 128th h

Total harmonic distortion up to the 128th h

and phase-to-neutral or phase-to-phase v

K-factors calculation for all phase current

Bus voltage, and

Bus current.

3.8.4 AUTOMATIC TRANSFER SWITCHES WITHOUTPOINTS

Serial interface points are available per manufacturer

 Automatic Transfer switches without maintenance by

monitor the following conditions:

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office S

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3.8.5 STATIC TRANSFER SWITCH POINTS

Serial interface points are available per manufact

the Static Transfer switches. The serial interface

conditions:

Input source energy consumption,

Input source power conditions,

Input source voltage conditions,

Input source phase conditions,

Input source power demand, Device communications,

Source useability,

Out-of-phase alarm,

Isolation breaker conditions, and

Bypass breaker conditions.

3.8.6 GENERATORS AND GENERATOR CONTRO

Generators and generator controllers use digital p

(hard wired), analog points as available per manu

points as available per manufacturer, if available

programmable logic controllers (daisy chain – RS

switch positions, PLC routines, and PLC diagnos

3.9 STUDY REQUIREMENTS AND ASSUMPTIONS

The Short Circuit, Load Flow, and Protective Dev

developed in accordance with the information pro

3.9.1 GENERAL

The Load Flow study, the Short Circu

Coordination study shall be developedapplication. Samples are provided in

Tools format.

The Load Flow study shall provide loa

various points on the power system a

July 11, 2008 Design Guidel

Section 3 Design Implementation Requirements FAA Pow

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The circuit breaker settings shown on the

the Design Engineer’s Final Design Pack

shown in the Protective Device Coordinat

Settings table.

3.9.2 SOFTWARE APPLICATION FOR STUDY CALCU

EDSA Release 2.95 or higher is the only software ap

used in the Load Flow study, the Short Circuit study,

Coordination study. A sample study is provided but

3.9.3 SOURCE OF DATA

Engineering Data – Facility load and equi

from design documents.

Utility Data – The available fault shall be o

either the primary or the secondary side o

primary side, the utility transformer imped

obtained.

Installation Data – Cable lengths, sizes, a

obtained from site specific design docume

EDSA Data – Cable, circuit breaker, fuse

be obtained from EDSA’s library.

3.9.4 PROTECTIVE DEVICES

The following information describes the FAA’s PhilosDevices:

Series Protective Devices – Protective de

require coordination since the same outag

opens.

Main-Tie-Main Breakers – Tie breakers s

breakers (set to overlap). This approach a

coordinate as required by FAA Order 695load, so the probability of overlapping fau

distribution equipment (i.e.: loss of source

occurring simultaneously) is extremely low

Feeder Breakers – Feeder breakers shall

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office S

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Branch Breakers – Non-adjustable bra

coordination with upstream protective

Circuit. Since the Critical Circuit requi

step-down transformer is specified at

available fault in order to provide bran

upstream feeder/main device. Also, u

been specified at larger frame/sensor

pickup, which aids in obtaining coordi

Hi-Low Fixed Magnetic Breakers – Al

adjustment shall be set to Hi in EDSA

In keeping with IEEE recommendations, the Shordeveloped at the earliest possible stage of the de

and length can be implemented efficiently and in

and coordination problems.

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

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APPENDIX A—ACRONYMS AND ABBREVIAT

Acronym/Abbreviation  A AMPERE

 AA AMBIENT AIR

 AC ALTERNATING CURRE

 A/C AIR CONDITIONING

 AF AMPERE FRAME

 AI ANALOG INPUT

 AIC AMPERE INTERUPTIN ALT ALTERNATE

 ANSI AMERICAN NATIONAL

 AT AMPERE TRIP

 ATS AUTOMATIC TRANSFE

 AUX AUXILLIARY

 AVG AVERAGE

 AWG AMERICAN WIRE GAU

 AX AMPERE RATING PLU

BATT BATTERY

BC BARE COPPER

BD BUS DUCT

BI BYPASS INPUT

BKR BREAKER

BLDG BUILDING

BP III BALANCED POWER III

BTU BRITISH THERMAL UN

CAT CATEGORY

CB CIRCUIT BREAKER

CCP CRITICAL CONTROL P

CFG CONFIGURATION

CHG CHARGER

CM CIRCUIT MONITORCOMM COMMUNICATIONS

COTS COMMERCIAL OFF TH

CPDS CRITICAL POWER DIS

CPL CRITICAL POWER PAN

July 11, 2008 Design Guidel

 Appendix A—Acronyms and Abbreviations FAA Pow

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Acronym/Abbreviation D

DI DIGITAL INPUT

DIA DIAMETERDISC DISCONNECT

DIST DISTRIBUTION

DPC CRITICAL DISTRIBUTION P

DPE ESSENTIAL DISTRIBUTION

DPN NON-ESSENTIAL DISTRIBU

DO DIGITAL OUTPUT

DS DISCONNECT SWITCH

DWG DRAWING

EA EACH

ECMS ENVIRONMENTAL CONTR

EG ENGINE GENERATOR

ELEC ELECTRIC

ELEM ELEMENTARY

ELEV ELEVATION

EMCC ESSENTIAL MOTOR CONT

ENCL ENCLOSURE

EPA ENVIRONMENTAL PROTEC

EPO EMERGENCY POWER OFF

EQUIP EQUIPMENT

EST ESTIMATE

EXT EXTERIOR

FA FORCED AIR

FAA FEDERAL AVIATION ADMIN

FDR FEEDER

FLA FULL LOAD AMPERES

FT FEET

FVNR FULL VOLTAGE NON-REVE

FWD FORWARD

GA GAUGEGEN ENGINE GENERATOR

GFE GOVERNMENT FURNISHE

GFI GROUND FAULT INTERUP

GFM GOVERNMENT FURNISHE

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

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Acronym/Abbreviation

IAW IN ACCORDANCE WIT

IC INTEGRATED CIRCUITILS INTEGRATED LOGIST

IN INCH

INSTR INSTRUMENT

INT INTERIOR

JB JUNCTION BOX

JCT JUNCTION

KCM KILO-CIRCULAR MIL

kVA KILO-VOLTS AMPERE

KW KILOWATT

L LENGTH

LAT LATERAL

LBS POUND

LDP LOAD BANK DISTRIBU

LH LEFT HAND

MAINT MAINTENANCE

MAX MAXIMUM

MCC MOTOR CONTROL CE

MCM MILLI-CIRCULAR MIL

MCS MOLDED CASE SWITC

MECH MECHANICAL

MED MEDIUM

MFR MANUFACTURER

MIN MINIMUM

MISC MISCELLANEOUS

MM MILLIMETER

MOD MODIFY, MODIFICATIO

MTBF MEAN TIME BETWEEN

MTD MOUNTED

MTM MAIN - TIE - MAIN (CIRMTTR MEAN TIME TO REPAI

N NEUTRAL, NORTH

N/A NOT APPLICABLE

NEC NATIONAL ELECTRIC

July 11, 2008 Design Guidel

 Appendix A—Acronyms and Abbreviations FAA Pow

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Acronym/Abbreviation D

OD OUTSIDE DIAMETER

OWS OPERATOR WORKSTATIOPC PERSONAL COMPUTER

PDU POWER DISTRIBUTION UN

PF POWER FACTOR

PH PHASE

PLC PROGRAMMABLE LOGIC C

PMCS POWER MONITORING AND

PNL PANEL

POS POSITIVE

PSG PARALLELING SWITCHGE

PSI POUNDS PER SQUARE INC

PT POTENTIAL TRANSFORME

PWR POWER

PZ POWER ZONE

QTY QUANTITY

REF REFERENCE

REV REVISION

RH RIGHT HAND

RIO REMOTE INPUT OUTPUT

RM ROOM

RPM REVOLUTIONS PER MINUT

SA SURGE ARRESTER

STS STATIC TRANSFER SWITC

SB SWITCHBOARD

SCHED SCHEDULE

SECT SECTION

SG SWITCHGEAR

SGL SINGLE

SOW STATEMENT OF WORK

SPEC SPECIFICATIONSQ SQUARE

SQ FT SQUARE FEET

STA STATION

SW SWITCH

Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

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Acronym/Abbreviation

UL UNDERWRITERS LABO

UPS UNINTERRUPTIBLE POV VOLT/VOLTAGE

VM VOLT METER

W WATT

WBS WORK BREAKDOWN S

WT WEIGHT

Z IMPEDANCE

July 11, 2008 Design Guidel

 Appendix A—Acronyms and Abbreviations FAA Pow

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

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APPENDIX B—REPORT TEMPLATE FOR STU

This appendix provides a report template for the

Protective Device Coordination studies. This sam

but Engineer shall provide studies in EDSA forma

template shall be made available with the Design

May 1, 2006

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Coordination Study Overview

Overview

The objective of this short circuit study is to estab

ratings in order to establish a basis of design for t

System (CPDS). The results of the short circuit st

ratings selected and shown.

The coordination study is performed to determine

adjustable trip breakers specified herein.

Purpose

Overload and short circuit conditions occur in eve

system. Protective devices are used to detect th

appropriate action. The distribution system relay

personnel, equipment and property under high cu

and calibrated, they selectively operate to remove

condition at the device closest to the fault.

The purpose of the protective device coordination

settings so that the protective devices operate as

appropriately to system disturbances while still m

protection and selectivity. Selectivity is achieved

and current intervals (sometimes referred to as m

protective devices from the power source to the f

closest to the fault operates first.

The purpose of the short circuit study is to determ

through the system under fault conditions. These

equipment interrupting capability to verify that dev

short circuit currents calculated without catastrop

System Description

The normal, emergency, and critical power distribmodeled using the single line drawing for the corr

drawing E410. In order to establish worst-case fa

systems are operating with utility power from any

generators are assumed to be operating to estab

TI 6480.3, CPDS

CPDS Type 1 Coordination Studies

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The available fault current for the utility source for a T

65,000A symmetrical for three phase faults and 22,0

faults.

In order to obtain worst-case fault currents, it is assu

mode while on utility input power.

It is assumed that 60% of the full load capacity of the

comprised of induction motors to model motor contrib

currents.

Typical, permanent magnet-excited, synchronous geutilized to develop the generator fault currents and de

Time-Current Curves

Plots of protective device time-current curves (TCC)

coordination. Included in each TCC plot is the corres

a simplified single-line diagram illustrating the circuit

characteristic curves are shown. The following TCC p

TCC Plot Descr

ESHA_U Incoming service, utility power to ES

ESHA_G Facility power on generator, generato

EDSLA Power to EDSLA

UPSA_IN_U UPSA on incoming utility power

UPSA_IN_G UPSA on incoming generator power

UPSA_BP_U UPSA on bypass utility powerUDSLA Power to UDSLA

UDSLA_GBP UDSLA on generator bypass power

SES-GFP Service entrance switch with ground

Summary Results and Settings Tables.

The summary short circuit current tables, suggested

voltage circuit breakers, time current curves and compage.

T h r  e eP h 

 S i  n gl   eL   

L i  n e t   oL 

L i  n e t   oL 

M o t   or  C  o

T r  an sf   or 

X f   or m er 

B u sN am e

AT S -AE

AT  S -A

AT  S A-F -B

AT S -AL

E  S HA-F 

AT S -A N

AT  S -A

AT  S A-F -A

AT S -BE

AT  S -B

AT  S B-F -B

AT S -BL

E  S HB-F 

 ol   um e1 

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h a s eF  a ul   t  

Y e  s 

F  a ul   t   e d B u s

Al  l  B u s  e  s 

in e t   o Gr  o un

 d 

Y e  s 

B u sV  ol   t   a g e s

F i  r  s  t  B u s F r  omF  a  ul   t  

Li  n eF  a ul   t  

 N o

Br  an ch  C  ur r  en t   s

F i  r  s  t  Br  a n c h F r  omF  a  u

l   t  

Li  n e t   o Gr  o un

 d 

 N o

P h  a s e or  S  e q u en

 c e

R e  p or  t   ph  a  s  e  q u a n t  i   t  i   e 

 s 

on t  r i   b  u t  i   on

Y e  s 

F  a ul   t   C  ur r  en t   C  a

l   c ul   a t  i   on

I  ni   t  i   a l   S  ymm e  t  r i   c  a l  RM S  (   wi   t  h 1  /  2  C  y c l   e A s  ym )  

rm er T  a p

Y e  s 

A s ym F  a ul   t   C  ur r  en t   a t  T i  m e

 0  . 5  0 

 C  y cl   e s

P h  a s e S h i  f   t  

Y e  s 

e

 3 P h  a s e

 S L  G

L L  G

L L 

L L  G

 S L  G

 3 P h  a s e

----------------I  ni   t  i   al   S  ymm e t  r i   c al  Am p s----------------

----------------------

----A s ymm e t  r i   c al  Am p s------------------------

 0 

1 2  , 0  8  7 

1 1  , 8  8 4 

 0 

 0 

1  8  , 3  8  9 

1  7  , 7  0  6 

 0 

 7 1  6 

2  , 3  9  3 

 5  3 4 

 0 

 0 

 3  ,1  5  6 

 0 

 0 

D o wn s  t  r  e  a m

I  n

B

1  7  , 7  0  6 

1 2  , 0  8  7 

1 1  , 8  8 4 

 0 

 0 

1  8  , 3  8  9 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

 6  3  , 7 1  9 

2 1  , 3  3 1 

 0 

 0 

 8 4  , 0 1  3 

2  8  , 5  8  6 

 0 

 7 1  6 

2  , 3  9  3 

 5  3 4 

 0 

 0 

 3  ,1  5  6 

 0 

 0 

D o wn s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

 6  3  , 7 1  9 

2 1  , 3  3 1 

 0 

 0 

 8 4  , 0 1 4 

2  8  , 5  8  6 

 0 

2  7  , 8  7 1 

 6 1  , 3  3  0 

2  0  , 7  9  8 

 0 

 0 

 8  0  , 8  6  3 

 0 

 0 

 U p s  t  r  e  a m

I  n

A

2  7  , 8  7 1 

 6 1  , 3  3  0 

2  0  , 7  9  8 

 0 

 0 

 8  0  , 8  6 4 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

1 2  ,1 1  7 

1 1  , 9 2  8 

 0 

 0 

1  8  ,4  7 4 

1  7  , 8  3 4 

 0 

 7 2 1 

2  , 3  9  3 

 5 4  8 

 0 

 0 

 3  , 0  7  6 

 0 

 0 

D o wn s  t  r  e  a m

I  n

B

1  7  , 8  3 4 

1 2  ,1 1  7 

1 1  , 9 2  8 

 0 

 0 

1  8  ,4  7 4 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

 6  0  ,2  6  3 

2  0  , 7  0  9 

 0 

 0 

 7  7  ,4 4  7 

2  7  ,2  5  0 

 0 

 7 2 1 

2  , 3  9  3 

 5 4  8 

 0 

 0 

 3  , 0  7  6 

 0 

 0 

D o wn s  t  r  e  a m

I  n

 C  a  b l   e 

1 ,P  ar  t  4  ,B  o ok 1 

 

AT S-B N

AT  S -B

AT  S B-F -A

 CP L1 -M

 C P L 1 -F 

 C P L 1 -MF 

 CP L2 

 C P L 2 -F 

 C P L 2 -MF 

 CP L 3 

 C P L  3 -F 

 C P L  3 -MF 

EDP HM

E DP HM-F 

E DP HM- G

T -E D S L M

ED S HA

E D S HA-F 

ED S HB

E D S HB-F 

ED S LA

E D S L A-F 

E P L A1 -F 

E P L A2 -F 

E P L A 3 -F 

E P L A4 -F 

 ol   um e1  

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 0

 6 0 ,2 64

2 0 , 7 0 9

 0

 0

 7 7 ,44 8

2 7 ,2 5 0

 0

2  6  , 5  3  0 

 5  7  , 8  7  7 

2  0  ,1  6 2 

 0 

 0 

 7 4  , 3  8 1 

 0 

 0 

 U p s  t  r  e  a m

I  n

A

2  6  , 5  3 1 

 5  7  , 8  7  8 

2  0  ,1  6 2 

 0 

 0 

 7 4  , 3  8 1 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

4  , 6  8  5 

 3  , 7  3  5 

 0 

 0 

4  , 6  9  5 

 3  , 7  3  6 

 0 

 3  , 7  3  6 

4  , 6  8  5 

 3  , 7  3  5 

 0 

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EPLB2-MF

E P L B 3 -MF 

E P L B4 -MF 

ED S LB

E D S L B-F 

E P L A1 -MF 

E P L A2 -MF 

E P L A 3 -MF 

E P L A4 -MF 

E P L B1 -F 

E P L B2 -F 

E P L B 3 -F 

E P L B4 -F 

ED S LM

 C P L 1 -MF 

 C P L 2 -MF 

 C P L  3 -MF 

E D S L M-F 

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 S T  S 2 -F -B

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EP LA1 -M

E P L A1 -F 

E P L A1 -MF 

EP LA2 

E P L A2 -F 

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EP LA 3 

E P L A 3 -F 

 ol   um e1  ,

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P  ar  t  4  ,B  o ok 

 

 3 

EP LA4 

E P L A4 -F 

E P L A4 -MF 

EP LB1 

E P L B1 -F 

E P L B1 -MF 

EP LB2 

E P L B2 -F 

E P L B2 -MF 

EP LB 3 

E P L B 3 -F 

E P L B 3 -MF 

EP LB4 

E P L B4 -F 

E P L B4 -MF 

E S HA

E D S HA-F 

E  S HA-F 

MT RI  -E  S HA

T -E D S L A-F 

 UP  S A-F 

 UP  S A-MF 

 U S HA-MBB

E S HB

E DP HM-F 

E D S HB-F 

 ol   um e1  , 

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MTRI -E SHB

T -E D S L B-F 

 GE N-B1 - O U

 GE  N-B1 

 G S HB-F 

 G S HB

AT  S A-F -B

AT  S B-F -B

E DP HM- GM

 G S HB-F 

L BH G-F 

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LBH G

L BH G-F 

LBH U

L BH U-F 

 S E S HA /  B

AT  S A-F -A

AT  S B-F -A

 UT I  L - 0  0  0 1 

 S T S 1 A

 S T  S 1 

 S T  S 1 -F -B

 S T S 1 L

 C P L 1 -F 

 ol   um e1  ,P 

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 S T S 2 L

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 S T S 2 P 

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T -E D S L A

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T-ED S LA-L

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 8  ,2  8  7 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

D o wn s  t  r  e  a m

I  

n

 C  a  b l   e 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

D o wn s  t  r  e  a m

I  

n

 C  a  b l   e 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

D o wn s  t  r  e  a m

I  

n

 C  a  b l   e 

 8  ,2  8  7 

 7  , 6  7  0 

 7  , 9  8  5 

 0 

 0 

 7  , 9 4  8 

 0 

 0 

 U p s  t  r  e  a m

I  

n

 C  a  b l   e 

ar  t  4  ,B  o ok 

 

 UP SA-F

 U S HA

L BH U-F 

T - UD S L A-F 

 U S HA-F 

 U S HA- GMBB

 U S HA-MBB-F 

 ol   um e1  ,P  a

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1 6 , 7 51

 34 , 824

1 5 , 0 6 9

 0

 0

 3 7 , 341

 0

 0

 U p s  t r  e  a m

I n

 C a  bl  e 

 0 

2 4  , 7 1  8 

1 1  , 8  9 4 

 0 

 0 

2 4  , 9 4 4 

1 2  ,1  3  8 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

D o wn s  t  r  e  a m

I  n

 C  a  b l   e 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

D o wn s  t  r  e  a m

I  n

 C  a  b l   e 

1 2  ,1  3  8 

2 4  , 7 1  8 

1 1  , 8  9 4 

 0 

 0 

2 4  , 9 4 4 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

B-F 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

F

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 0 

 U p s  t  r  e  a m

I  n

 C  a  b l   e 

ar  t  4  ,B  o ok 

 

 8 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE AKE R S E T T I  N G S 

 S E  S HA-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

 S E  S HA -M S 

 S  Q UA RE D-B P  S 

 G C -2  0  0 E 

1  0  0  0 

A  S 

---

---

---

---

---

---

1  ,2  0  0 A 

 0 .4 

 O UT 

 S E  S HB-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

 S E  S HB -M S 

 S  Q UA RE D-B P  S 

 G C -2  0  0 E 

1  0  0  0 

A  S 

---

---

---

---

---

---

1  ,2  0  0 A 

 0 .4 

 O UT 

E  S HA-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E  S HA -MB 

 S  Q UA RE D

NW2  0 H

2  0  0  0 

A P 

2  0  0  0 

A  S 

1 . 5 

 0 .1 

I  N

 6 

---

---

---

E D S HA -F B 

 S  Q UA RE D

NW1  6 H

1  0  0  0 

A P 

1  6  0  0 

A  S 

 8 

 3 

 0 . 3 

I  N

1  0 

---

---

---

T -E D S L A -F B 

 S  Q UA RE D

NW 0  8 H

4  0  0 A 

 8  0  0 A 

 S 

1 2 

 5 

 0 .4 

I  N

1  5 

---

---

---

 UP  S A -RI  B -F B 

 S  Q UA RE D

NW 0  8 H

4  5  0 A 

 8  0  0 A 

 S 

 0 .7 

2 4 

 6 

 0 .4 

I  N

1  5 

---

---

---

 UP  S A - S B B -F B 

 S  Q UA RE D

NW 0  8 H

4  0  0 A 

 8  0  0 A 

 S 

 0 . 9 

2 4 

 6 

 0 .4 

I  N

1  5 

---

---

---

 U S HA -MB B -F B 

 S  Q UA RE D

NW 0  8 H

4  0  0 A 

 8  0  0 A 

 S 

 0 . 9 

 3 

 0 .2 

I  N

 8 

---

---

---

L .T .-L  ON GT I  ME 

 S .T .

- S H ORT T I  ME 

I  N S T 

.-I  N S T A NT A NE  O U S 

 GND

- GR O UNDF A  UL T 

P . U.

-P I   C K  UP  S E T T I  N G

T I  ME 

-DE L A Y  S E T T I  N G

 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE AKE R S E T T I  N G S 

E  S HB-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L 

 U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S 

.D.I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E  S HB -MB 

 S  Q UA RE D

NW2  0 H

2  0  0  0 

A P 

2  0  0  0 

A  S 

1 . 5 

 0 .1 

I  N

 6 

---

---

---

E D S HB -F B 

 S  Q UA RE D

NW1  6 H

1  0  0  0 

A P 

1  6  0  0 

A  S 

 8 

 3 

 0 . 3 

I  N

1  0 

---

---

---

T -E D S L B -F B 

 S  Q UA RE D

NW 0  8 H

4  0  0 A P 

 8  0  0 A  S 

1 2 

 5 

 0 .4 

I  N

1  5 

---

---

---

E DP HM-F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 .7 

2 4 

 6 

 0 .4 

I  N

1  5 

---

---

---

E D S HA-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L 

 U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S 

.D.I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E D S HA -MB 

 S  Q UA RE D

NW 0  8 H

 8  0  0 A P 

 8  0  0 A  S 

1 . 5 

 0 .1 

I  N

 6 

---

---

---

2 2  5 A F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 9 

2 4 

 5 

 0 .4 

I  N

1 2 

---

---

---

E D S HB-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE A

KE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S 

 OR

 & P L 

 U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S 

.D.I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E D S HB -MB 

 S  Q UA RE D

NW 0  8 H

 8  0  0 A P 

 8  0  0 A  S 

 0 .1 

I  N

 6 

---

---

---

2 2  5 A F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 9 

2 4 

 5 

 0 .4 

I  N

1 2 

---

---

---

L .T .-L  ON GT I  ME 

 S .T .- S H ORT T I  ME 

I  N S 

T .-I  N S T A NT A NE  O U S 

 GND- GR O UNDF A  UL T 

P . U

.-P I   C K  UP  S E T T I  N G

T I  M

E -DE L A Y  S E T T I  N G

 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE A

KE R S E T T I  N G S 

 U S HA-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AKE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  OR

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

 UP  S A -MI  B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 9 

 8 

 0 . 3 

I  N

1  0 

---

---

---

 U S HA -MB B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 8 

 0 . 3 

I  N

1  5 

---

---

---

 U S HA - GMB B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

1 2 

 3 

 0 . 3 

I  N

1 2 

---

---

---

T - UD S L A -F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

2 . 5 

 0 .1 

I  N

 8 

---

---

---

 UP  S A -L B B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 8 

 3 

 0 .2 

I  N

1 2 

---

---

---

E DP HM-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AKE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  OR

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E DP HM-MB 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 9 

 8 

 0 . 3 

I  N

1  0 

---

---

---

E DP HM- GMB B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

1 2 

 3 

 0 . 3 

I  N

1 2 

---

---

---

L .T .-

L  ON GT I  ME 

 S .T .-

 S H ORT T I  ME 

I  N S T .-I  N S T A NT A NE  O U S 

 GND

- GR O UNDF A  UL T 

P . U.-P I   C K  UP  S E T T I  N G

T I  ME 

-DE L A Y  S E T T I  N G

 

 3 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE A

KE R S E T T I  N G S 

E D S L A-2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AKE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  OR

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E D S L A -MB 

 S  Q UA RE D

NW 0  8 H

 8  0  0 A 

 8  0  0 A 

 S 

 8 

 0 .1 

I  N

1  5 

---

---

---

E P L A 1 -F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 6 

2 4 

1  0 

 0 .2 

I  N

1  0 

---

---

---

T Y P I   C A L F  ORA L L 

F E 

E DE RB RE A K E R S 

E D S L B-2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AKE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  OR

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E D S L B -MB 

 S  Q UA RE D

NW 0  8 H

 8  0  0 A 

 8  0  0 A 

 S 

 8 

 0 .1 

I  N

1  5 

---

---

---

E P L B 1 -F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 6 

2 4 

1  0 

 0 .2 

I  N

1  0 

---

---

---

T Y P I   C A L F  ORA L L 

F E 

E DE RB RE A K E R S 

 UD S L A-2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AKE R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  OR

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

 UD S L A -MB 

 S  Q UA RE D

NW 0  8 H

 6  0  0 A 

 8  0  0 A 

 S 

 0 . 8 

1  6 

 0 .1 

I  N

 8 

---

---

---

 S T  S 1 -F B -A 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 6 

2 4 

 8 

 0 .1 

I  N

1  0 

---

---

---

 S T  S 2 -F B -A 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 6 

2 4 

 8 

 0 .1 

I  N

1  0 

---

---

---

 S T  S  3 -F B -A 

 S  Q UA RE D

NW 0  8 H

2  5  0 A 

 8  0  0 A 

 S 

 0 . 6 

2 4 

 8 

 0 .1 

I  N

1  0 

---

---

---

L .T .-

L  ON GT I  ME 

 S .T .- S H ORT T I  ME 

I  N S T 

.-I  N S T A NT A NE  O U S 

 GND

- GR O UNDF A  UL T 

P . U.-P I   C K  UP  S E T T I  N G

T I  ME 

-DE L A Y  S E T T I  N G

 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE AKE R S E T T I  N G S 

E D S L M-2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AK

E R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  O

R

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D

.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E D S L M-MB 

 S  Q UA RE D

NW 0  8 H

 6  0  0 A P 

 8  0  0 A  S 

 0 . 8 

1  6 

 0 .1 

I  N

 8 

---

---

---

 S T  S 1 -F B -B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 6 

2 4 

 8 

 0 .1 

I  N

1  0 

---

---

---

T Y 

P I   C A L F  ORA L L 

F E E 

DE RB RE A K E R S 

 C P L 1 -MB B -F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 6 

2 4 

 8 

 0 .1 

I  N

1  0 

---

---

---

T Y 

P I   C A L F  ORA L L 

F E E 

DE RB RE A K E R S 

 C P L 1  (  T Y P I   C AL F  ORAL L  C P L  )  -2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AK

E R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  O

R

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D

.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

 C P L 1 -MB 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

---

---

---

 C P L 1 -MB B 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

---

---

---

E P L A1  (  T Y P I   C AL F  ORAL L E P L A )  -2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AK

E R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  O

R

 & P L  U G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D

.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E P L A 1 -MB 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

---

---

---

E P L A 1 -MB B 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

---

---

---

L .T .-L  ON GT I  ME 

 S .T .- S H ORT T I  ME 

I  N S T .-I  N S T A NT A NE  O U S 

 GND-

 GR O UNDF A  UL T 

P . U.-P I   C K  UP  S E T T I  N G

T I  ME -DE L A Y  S E T T I  N G

 

 5 

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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AD J  U S T ABL E L  OW V  OL T A GE BRE A

KE R S E T T I  N G S 

E P L B1  (  T Y P I   C AL F  ORAL L E P L B )  -2  0  8 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AK

E R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  O

R

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

E P L B 1 -MB 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

1  0 

---

---

---

E P L B 1 -MB B 

 S  Q UA RE D

K A 

1  5  0 A P 

1  5  0 A F 

---

---

---

---

---

1  0 

---

---

---

 G S HB-4  8  0 V 

 C I  R C  UI  T BRE AKE RI  NF  ORMAT I   ON

 C I  R C  UI  T BRE AK

E R S E T T I  N G S 

BRE AKE R OR

 C I  R C  UI  T I  D

BRE AKE R

T Y P E 

 S E N S  O

R

 & P L  U

 G

L .T .

P . U.

L .D.

T I  ME 

 S .D.

P . U.

 S .D.

T I  ME 

 S .D.

I  ²   t  

I  N S T .

P . U.

 GND

P . U.

 GND

T I  ME 

 GND

I  ²   t  

N OT E  S 

A T  S A - GM-F B 

 S  Q UA RE D

NW2  0 H

2  0  0  0 A 

2  0  0  0 A 

 S 

 0 .2 

I  N

 8 

---

---

---

A T  S B - GM-F B 

 S  Q UA RE D

NW2  0 H

2  0  0  0 A 

2  0  0  0 A 

 S 

 0 .2 

I  N

 8 

---

---

---

 GE N-B 1 - GB 

 S  Q UA RE D

NW2  0 H

2  0  0  0 A 

2  0  0  0 A 

 S 

2 . 5 

 0 .4 

I  N

1  5 

---

---

---

 U S HA - GMB B -F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 9 

 3 

 0 .2 

I  N

 8 

---

---

---

E DP HM- GMB B -

F B 

 S  Q UA RE D

NW 0  8 H

2  5  0 A P 

 8  0  0 A  S 

 0 . 9 

 3 

 0 .2 

I  N

 9 

---

---

---

 G S HB -L B B 

 S  Q UA RE D

NW2  0 H

2  0  0  0 A 

2  0  0  0 A 

 S 

 0 . 3 

I  N

 8 

---

---

---

L .T .-

L  ON GT I  ME 

 S .T .-

 S H ORT T I  ME 

I  N S T .-I  N S T A NT A NE  O U S 

 GND

- GR O UNDF A  UL T 

P . U.-P I   C K  UP  S E T T I  N G

T I  ME 

-DE L A Y  S E T T I  N G

 

 6 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  N

W , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 

E D S HA-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  N

T  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p 8  0  0 . 0 A 

E  S HA

4  8  0 V 

E D S HA-F 

E D S HA-MB

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  N

T  , 5 . 0 P  /  H

 S  en s  or  /  T r i   p 8  0  0 . 0 A 

E D S HA

4  8  0 V 

2 2  5 A

F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  N

T  , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  5  0 . 0 A 

E  S HA-F 

N

E AT  S -A

AT  S A-F -A

M S - GF R

 S  Q UA RE D

 G C -2  0  0 E 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g1  0  0  0 . 0 A 

T  y  p e G C -2  0  0 E 

 S  en s  or  /  T r i   p1  0  0  0 . 0 A 

M S -F  u s e

B  U S  S MA NN

K RP - C 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g2  0  0  0 . 0 A 

T  y  p e 6  0 1 -4  0  0  0 A 

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 S E  S HA-M S 

 S E  S HA /  B

4  8  0 V 

 S  c  al   eX 1  0 ^ 1 

 C  ur v  e: E  S HA  _ U

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2 

 0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E  S HA-F 

N

E AT  S -A

AT  S A-F -B

AT  S A- GM-F B

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW ,

 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 G S HB

4  8  0 V 

 GE N-B1  

1 2  5  0 . 0 k W

4  8  0 V 

 GE N-B1  -I   B

 G S HB-F 

 GE N-B1  - GB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW ,

 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E D S HA-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8 

 0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 

P  /  H

 S  en s  or  /  T r i   p 8  0  0 . 0 A 

E  S HA

4  8  0 V 

 S  c  al   eX 1  0 ^ 1 

 C  ur v  e: E  S HA  _ G

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

 8 

  

  

 

  

   

   

   

   

     

       

     

    

   

     

    

   

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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T -E D S L A

 2 2  5 . 0 k V A 

T -E D S L A-F 

T -E D S L A-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

E P L A-1 -F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 5 

. 0  &  5 . 0 A 

 S  en s  or  /  T r i   p2  5  0 . 0 A 

E P L A1 -F 

E D S L A-MB

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p 8  0  0 . 0 A 

E D S L A-F 

E D S L A

2  0  8 V 

E P L A1 -MB

 S  Q UA RE D

K A 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g1  5  0 . 0 A 

T  y  p eK A 

 S  en s  or  /  T r i   p1  5  0 . 0 A 

E P L A1 -M

2  0  8 V 

  E  S HA

4  8  0 V 

E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 C B7  0 A

 3 P 

 S  Q UA RE D

 Q O-V H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g7  0 . 0 A 

T  y  p e Q O-V H , 3 -P  ol   e

 S  en s  or  /  T r i   p7  0 . 0 A 

 S  c  al   eX 1  0 ^ 1 

 C  ur v  e: E D S L A 

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

 9 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  

i  n g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW

 , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E  S HA

4  8  0 V 

E  S HA-F 

N

E AT  S -A

AT  S A-F -A

M S - GF R

 S  Q UA RE D

 G C -2  0  0 E 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g

1  0  0  0 . 0 A 

T  y  p e G C -2  0  0 E 

 S  en s  or  /  T r i   p1  0  0  0 . 0 A 

M S -F  u s e

B  U S  S MA NN

K RP - C 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g

2  0  0  0 . 0 A 

T  y  p e 6  0 1 -4  0  0  0 A 

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 S E  S HA-M S 

 S E  S HA /   B

4  8  0 V 

 UP  S A-RI   B-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  

i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

 UP  S A-F 

RE  C - 0   0   0  1  

 d  cB U S - 0   0   0  4  

 S  c  al   eX 1  0 ^ 1 

 C  ur v  e:  UP  S A  _I  N _ U

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1  0 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g

2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW , 5 

. 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E  S HA

4  8  0 V 

E  S HA-F 

N

E AT  S -A

 UP  S A-RI   B-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g

 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

 UP  S A-F 

RE  C - 0   0   0  1  

 d  cB U S - 0   0   0  4  

AT  S A-F -B

AT  S A- GM-F B

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW

 , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 G S HB

4  8  0 V 

 S  c  al   eX 1  0 

^ 1 

 C  ur v  e:  UP  S A  _I  N _ G

V  ol   t   a g e4  8 

 0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1 1 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2 

 0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW , 5 . 0 

P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E  S HA

4  8  0 V 

E  S HA-F 

N

E AT  S -A

AT  S A-F -A

M S - GF R

 S  Q UA RE D

 G C -2  0  0 E 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g1  0  0  0 . 0 A 

T  y  p e G C -2  0  0 E 

 S  en s  or  /  T r i   p1  0  0  0 . 0 A 

M S -F  u s e

B  U S  S MA NN

K RP - C 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p e 6  0 1 -4  0  0  0 A 

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 S E  S HA-M S 

 S E  S HA /   B

4  8  0 V 

 UP  S A- S BB-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8 

 0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p2  5  0 . 0 A 

 UA

4  8  0 V 

 U S HA-F 

 UP  S A-MI   B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8 

 0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

 U S HA

4  8  0 V 

 UP  S A-MF 

T - UD S L A-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8 

 0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 . 0 P  /  H

 S  en s  or  /  T r i   p2  5  0 . 0 A 

 S  c  al   eX 1  0 ^ 

 C  ur v  e:  UP  S A  _B P  _ U

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1 2 

    

 

     

     

    

     

       

    

    

    

    

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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 UP  S A-MI  B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

T - UD S L A-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p2  5  0 . 0 A 

T - UD S L A-F 

T - UD S L A

 1  5  0 . 0 k V A 

 UD S L A-MB

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 5 

. 0 P  /  H

 S  en s  or  /  T r i   p 6  0  0 . 0 A 

 UD S L A-F 

 UD S L A

2  0  8 V 

 S T  S 1 -F B-A

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n

 g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 5 

. 0  &  5 . 0 A 

 S  en s  or  /  T r i   p2  5  0 . 0 A 

 S T  S 1 -F -A

 U S HA

4  8  0 V 

A

 S T  S 1 

 C P L 1 -F 

 C P L 1 -M

2  0  8 V 

 C P L 1 -MB

 S  Q UA RE D

K A 

F r  am e /   C  ar  t  r i   d  g e /  R a

 t  i  n g1  5  0 . 0 A 

T  y  p eK A 

 S  en s  or  /  T r i   p1  5  0 . 0 A 

 Q OB

7  0 A

 S  Q UA RE D

 Q O-V H

F r  am e /   C  ar  t  r i   d  g e /  R a

 t  i  n g7  0 . 0 A 

T  y  p e Q O-V H , 3 -P  ol   e

 S  en s  or  /  T r i   p7  0 . 0 A 

 S  c  al   e

X 1  0 

^  0 

 C  ur v  e:  UD S L A 

V  ol   t   a g e4  8 

 0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1  3 

    

 

     

     

    

     

       

    

    

    

    

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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T - UD S L A-F B

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p2  5  0 . 0 A 

T - UD S L A-F 

T - UD S L A

 1  5  0 . 0 k V A 

 UD S L A-MB

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 5 

. 0 P  /  H

 S  en s  or  /  T r i   p 6  0  0 . 0 A 

 UD S L A-F 

 UD S L A

2  0  8 V 

 S T  S 1 -F B-A

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 5 

. 0  &  5 . 0 A 

 S  en s  or  /  T r i   p2  5  0 . 0 A 

 S T  S 1 -F -A

 U S HA

4  8  0 V 

A

 S T  S 1 

 C P L 1 -F 

 C P L 1 -M

2  0  8 V 

 C P L 1 -MB

 S  Q UA RE D

K A 

F r  am e /   C  ar  t  r i   d  g e /  R a

 t  i  n g1  5  0 . 0 A 

T  y  p eK A 

 S  en s  or  /  T r i   p1  5  0 . 0 A 

 Q OB

7  0 A

 S  Q UA RE D

 Q O-V H

F r  am e /   C  ar  t  r i   d  g e /  R a

 t  i  n g7  0 . 0 A 

T  y  p e Q O-V H , 3 -P  ol   e

 S  en s  or  /  T r i   p7  0 . 0 A 

 U S HA- GMBB

 S  Q UA RE D

NT  0  8 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g 8  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NT  , 6 

. 0 P  /  H

 S  en s  or  /  T r i   p4  0  0 . 0 A 

 S  c  al   e

X 1  0 ^ 1 

 C  ur v  e:  UD S L A - GB P 

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1 4 

  

  

 

  

   

   

   

   

     

       

V  ol   um e1  ,P  ar  t  4  ,B  o ok 1 

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E  S HA-MB

 S  Q UA RE D

NW2  0 H

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p eM a s  t   er  p a c  t  NW , 5 . 0 P  /  H

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

E  S HA-F 

N

E AT  S -A

AT  S A-F -A

M S - GF R

 S  Q UA RE D

 G C -2  0  0 E 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g1  0  0  0 . 0 A 

T  y  p e G C -2  0  0 E 

 S  en s  or  /  T r i   p1  0  0  0 . 0 A 

M S -F  u s e

B  U S  S MA NN

K RP - C 

F r  am e /   C  ar  t  r i   d  g e /  R a t  i  n g2  0  0  0 . 0 A 

T  y  p e 6  0 1 -4  0  0  0 A 

 S  en s  or  /  T r i   p2  0  0  0 . 0 A 

 S E  S HA-M S 

 S E  S HA /   B

4  8  0 V 

 S  c  al   eX 1  0 ^ 1 

 C  ur v  e:  S E  S - GF P 

V  ol   t   a g e4  8  0 

I   s  s  u e d : A  pr i  l  2  5  ,2  0  0  5 

 

1  5 

 

SHORT CIRCUIT ANALYSIS REPORT

May 1, 2006

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 SHORT CIRCUIT ANALYSIS REPORT

 

  

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

   

 

 

 

 

 

 

 

 

 

 

   

 

 

 

 

 

 

 

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FEEDER DATA

May 1, 2006

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

APPENDIX C—MANUFACTURER’S DOCUMEN

C.1 KOHLER EQUIPMENT

GENERATOR

Refer to Volume 3 of TI6480 3 CPDS

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Refer to Volume 3 of TI6480.3, CPDS

AUTOMATIC TRANSFER SWITCH

Refer to Volume 8, Part 1, Book 1 of TI64

C.2 MITSUBISHI EQUIPMENT

UNINTERRUPTIBLE POWER SUPPLY

Refer to Volume 6 of TI6480.3, CPDS

C.3 L–3 EQUIPMENT

STATIC TRANSFER SWITCH Refer to Volume 7 of TI6480.3, CPDS

C.4 SQUARE D EQUIPMENT

SWITCHBOARDS

Refer to Volume 2, Part 1, Book 1 of TI64

For shop drawings, refer to Square D draw

PANELBOARDS

Refer to Volume 5, Part 1, Book 1 of TI64

For shop drawings, refer to Square D draw

I-LINE PANELBOARDS

Refer to Volume 5, Part 1, Book 1 of TI64

For shop drawings, refer to Square D draw

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

APPENDIX D—CONSTRUCTION SPECIFICAT

Specifications attached are a sample document a

modify them to fit their specific application. Thes

minimum standards allowed and more stringent lo

shall be followed.

DIVISION 2 - SITE CONSTRUCTION

SECTION 02555 - EXTERIOR FUEL DISTRIBUT

DIVISION 13 - SPECIAL CONSTRUCTION

SECTION 13080 - SEISMIC PROTECTION FOR

DIVISION 15 - MECHANICAL

SECTION 15491H - FUEL-OIL SYSTEM

DIVISION 16 - ELECTRICAL

SECTION 16050 - BASIC ELECTRICAL MATER

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SECTION 16070 - SEISMIC PROTECTION FOR

SECTION 16075 - ELECTRICAL IDENTIFICATIO

SECTION 16081 - APPARATUS INSPECTION A

SECTION 16231 – INSTALLATION OF PACKAG

SECTION 16402 — INTERIOR DISTRIBUTION

SECTION 16410 — INSTALLATION OF AUTOM

SECTION 16412 — INSTALLATION OF STATIC

SECTION 16442 — INSTALLATION OF SWITCH

SECTION 16461 – INSTALLATION OF DRY TYP

LESS)

SECTION 16610 INSTALLATION OF UNINTER

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 02555 - EXTERIOR FUEL DISTRIBUTION

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope,

mental conditions and seismic requirements.

 Include references to all applicable related sections, suchthrough 14 sections, mechanical division 15 sections, othe section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this speThe publications are referred to in the text by the bas

1. AMERICAN PETROLEUM INSTITUTE (API)

a. API Spec 5L(2000) Line Pipeb. API Spec 6D (2002) Pipeline Valves

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Valves)c. API Std 594 (1997) Wafer and Wafer-Lugd. API Std 609 (1997) Lug- and Wafer-Typee. API RP 1110 (1997) Pressure Testing f. API BULL 2209 (1978) Pipe Plugging Pra

2. ASME INTERNATIONAL (ASME)

a. ASME B16.3 (1998) Malleable Iron Thb. ASME B16.5 (1996) Pipe Flanges

Through NPS 24c. ASME B16.9 (2001) Factory-Made Wrd. ASME B16.11 (2001) Forged Fittings, Se. ASME B16.34 (1996) Valves - Flanged,f. ASME B16.39 (1998) Malleable Iron Th

250, and 300g. ASME B31.3 (2002) Process Piping

3 AMERICAN SOCIETY FOR TESTING AND MA

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

d. ASTM A 194/A 194M (2001; Rev. A) Bolts for High-Pressure and High-Tempe

e. ASTM D 229 (2001) Rigid Sheet and Insulation

4. MANUFACTURERS STANDARDIZATION SOFITTINGS INDUSTRY (MSS)

a. MSS SP-58 (1993) Pipe Hangers and SManufacture

b. MSS SP-69 (2002) Pipe Hangers and Su

5. NATIONAL ELECTRICAL MANUFACTURERS

a. NEMA MG 1 (1998) Motors and Gene

6. NATIONAL FIRE PROTECTION ASSOCIATIOa. NFPA 30 (2000) Flammable and Combb. NFPA 70 (2002) National Electrical Co

1.2 SYSTEM DESCRIPTION

 A. Provide new exterior fuel distribution system co

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System shall include aboveground piping, piping related work.

1.3 SUBMITTALS

 A. Government approval is required for submittals withhaving a "G" designation are for information only orused, a designation following the "G" designation idthe submittal for the Government. The following shaSection 01330 SUBMITTAL PROCEDURES:

1. SD-03 Product Data

a. Pipeb. Valvesc. Strainersd. Pipe hangers and supports

e Expansion joints

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2. SD-10 Operation and Maintenance Data

a. Fuel pumps, Data Package 2; Gb. Submit in accordance with Section 017

Data."

1.4 QUALITY ASSURANCE

 A. Certification of Welder's Qualifications

1. Submit prior to site welding. Certifications shal

PART 2 - PRODUCTS

2.1 STEEL FUEL PIPE

 A. ASTM A 53/A 53M; Type E (electric-resistance we(seamless, Grade A or B), black steel. Provide Wwelding end connections. Provide Weight Class XSconnections.

B. API Spec 5L; seamless, submerged-arc weld or gasteel. Provide Weight Class STD (Standard) for w

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Weight Class XS (Extra-Strong) for threaded end con

2.2 FITTINGS

 A. Threaded Fittings: ASME B16.11 or ASME B16.3.

B. Socket Welded Fittings: ASME B16.11.

C. Buttwelding Fittings: ASME B16.9. Provide the s

piping in which fittings are installed. Backing rings sbe compatible with materials being welded.

D. Flanges: ASME B16.5, Class 150.

E. Unions: ASME B16.39, Class 150. Provide electrwhere indicated.

2.3 GASKETS, BOLTS, NUTS, AND WASHERS

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Nuts: ASTM A 194/A 194M, Grade 7, with Teflon coa

D. Washers: Provide steel flat circular washers under b

E. Electrical Insulating Gaskets for Flanges: Provide material of 1000 ohms minimum resistance. Materiaaviation hydrocarbon fuels. Provide full face, one pibetween flanges. Provide full surface 0.03 inch t

mylar insulating sleeves between bolts and holes inshanks of a diameter not less than the diameter at tinch thick high strength phenolic insulating washerssteel washers over insulating washers and under bo0.5 inch longer than standard length to compensateand the washers under bolt heads and nuts.

2.4 VALVES

 A. General

1. Steel body for working pressure of ASME ClasProvide with stems in the horizontal positionabove the horizontal position. Valves shall havvalves smaller than 2.5 inches shall have unend connections with a union on all but one sTeflon seals with metal backup. Provide g

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housing designed to exclude driving rain. Profactory-installed limit switches that are actuated

B. Ball Valves

1. API Spec 6D, steel body, ASME Class 150seated type capable of handling two-way operators, except valves 4 inches and smallepositions or infinitely adjustable positions beMinimum bore size shall be equal to of the inteof the same nominal diameter. Provide chroballs. Valves shall have stainless steel stemseats, body seals, and stem seals.

C. Check Valves

1. ASME B16.34, Class 150, steel body. Valve

globe type with fully guided (top and bottom) dis

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

F. Butterfly Valves

1. API Std 609, Class 150, steel body, bubbletig275 psig. Disc shall be Type 304L or Type 3Type 416 or Type 630, stainless steel. Seabackup. Stem seals shall be capable of withtemperature of the valve seat. Valves 6 inchedischarge shall have weatherproof gear opera

shall have 10-position throttling handles. Ins150 flanges. Do not install valves on other flaand valve flanges. Provide spool pieces. Provindicated. Provide fusible link and springautomatically when the link material melts at 1the closed position.

G. Wafer Type Check Valves

1. API Spec 6D and API Std 594, ASME Class 1be provided in lieu of swing-check valves in pValves shall have Grade CF8M stainless steeshall have Type 316 stainless steel spring, hinbearing materials. Install valves between ASM

H. Pump Pressure Relief Valves

1 ASME Cl 150 ith fl d d

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1. ASME Class 150, with flanged end connHydraulically operated, diaphragm type, modpipe line pressure through a pilot control smaintain a constant line pressure but close adjustable, direct acting, spring-loaded, diaphrwhen the controlled pressure is greater than aluminum alloy 6061-T6 or 356-T6, stainless pilot system; and rubber parts of Viton or Buvalve shall close. Provide valve with position pressure gage quick-disconnect fittings located

I. Solenoid Control Valves

1. ASME Class 150, with flanged end connHydraulically operated, pilot controlled, diaphrashutoff down to 200 psig operating pressurecontrols shall cause the main valve to ope

deenergized the solenoid controls shall cause

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. General

1. Pressure components of equipment shall be fo150, 275 psig at 100 degrees F.

B. Fuel Pumps

1. Provide pumps designed for use with aviatio

pressure of 275 psig at 100 degrees F. Desigcharacteristics throughout entire head capacityPump motors shall conform to NEMA MG 1Division 1, Group D, explosion- and weather-prated for continuous duty based on 99 degreeinsulation. Motors shall have built-in, nonsmechanism to prevent reversal of pump shashall be base mounted. Turbine pumps sh

permits pump removal without entering the tank

2.6 ELECTRICAL COMPONENTS

 A. Provide explosion proof motors, controllers, contactoNFPA 70, Class I, Division 1, Group D, except wheGroup D is indicated. Furnish motors, controllers, respective pieces of equipment. Motors, controllers,conform to and shall have electrical connection

"El t i l " C t ll d t t h ll h

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"Electrical." Controllers and contactors shall havecircuits, and shall have auxiliary contacts for use wmotors and equipment furnished are larger than sizeadditional electrical service and related work shall be

2.7 PIPING SYSTEM COMPONENTS AND ACCESSOR

 A. General

1. Design pressure and temperature ratings shaClass 150, 275 psig at 100 degrees F.

B. Pipe Hangers and Supports

1. MSS SP-58 and MSS SP-69, adjustable typindicated otherwise. Provide steel pipe hangenuts, bolts, washers, hangers, and supports s

iron rollers and bases may be painted with twoh t di l i d

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

c. Low-Friction Supports: Provide seelements composed of 100 percent virgireinforcing aggregates, prebonded to apCoefficient of static friction between the installation for both vertical and horizontathan 0.002 inch under allowable static losteel shall be heat cured, high temperatusupport elements for the loads applied

minimum of 0.09 inch thick. Steel supUnits shall be factory designed and manu

d. Miscellaneous Metal: ASTM A 36/A 36Msteel shapes, hot-dip galvanized.

e. Anchors, Bolts, Nuts, Washers, and Scexcept provide Type 316 stainless steel u

C. Strainers

1. ASME Class 150, steel body, with flanged endpattern , duplex type. Strainers shall have rem316 stainless steel wire screen unless other meclean strainer shall not exceed 3 psig at desigair eliminator.

D. Gages

1 Provide single style pressure gage for fuel wit

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1. Provide single style pressure gage for fuel witcase, bronze tube, stainless steel ball valve, scale range suitable for intended service.

E. Pipe Sleeves

1. Provide where piping passes entirely through of sufficient length to pass through entire thickone inch minimum clearance between exterior core-drilled hole. Seal space at both ends oplastic waterproof cement which will dry to a fmechanically adjustable segmented elastomeriseal both ends of sleeves or core-drilled holesmaterial.

a. Sleeves in Masonry and Concrete Wagalvanized steel, ductile-iron, or cast-iro

masonry and concrete may be provide

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

G. Flexible Pipe Connectors

1. Stainless steel, single braided, close helical typconnections. Connectors shall have sufficient movement. Hose shall have working pressure

H. Temporary Conical Strainers

1. Provide steel pipe spool piece 12 inches long each end of the spool piece, and of the same flanges on the connecting piping. Strainers between flanges, with strainer body within thconstructed of stainless steel with 0.25 inch dmesh stainless steel wire screen.

2.8 PROTECTIVE COATINGS FOR BURIED PIPING

 A. Provide protective coatings for buried piping. Padhesive undercoat and continuously extruded plastthickness of plastic resin shall be 23 mils for pipe sizmils for pipe sizes 6 inches and larger. Tape shapolyethylene or plasticized polyvinyl chloride coatepressure sensitive waterproof adhesive. Surfacesexisting piping affected by the Contractor's operationand primed before application of tape. Tape shall ov

inches Waterproof shrink sleeves may be provided

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inches. Waterproof shrink sleeves may be provided by electric heating. Sleeves shall overlap pipe Extruded coating and adhesive undercoat surfaces primed with a compatible primer prior to applicatirecommended by tape manufacturer and approved b

1. Damaged Areas of Extruded Coating: Providover damaged areas. Residual material frombreak or trimmed off. Tape shall be applied sptape is applied. A double wrap of one full widangles to the axis to seal each end of the spiral

2. Fittings, Couplings, and Regular Surfaces: Ptape overlapped not less than one inch over daapply first layer of tape to conform to componsecond layer of tape over first layer of tape.

3. Flanges, Valves, and Irregular Uncoated Surfamastic painting system to a minimum dry film th

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Zinc, zinc coated steel, zinc coated cast iron, brass, contacting the fuel shall not be permitted, except und

1. Brass contacting the fuel shall be permitted uthe total fuel wetted surface area in each system

2. Aluminum casting containing up to a maximumthe fuel shall be permitted.

3. Carbon steel containing up to a maximum of o

fuel shall be permitted in carbon steel piping sy4. Brass hose fittings and couplings will be permit

2.11 BONDING

 A. NFPA 70 for materials and workmanship. All parts bonded in metallic contact to provide electrical components for grounding the entire system. Provid

effects of gaskets, paints, and nonmetallic componenless than No. 6 size, single covered, flexible, strandUSE.

2.12 BURIED WARNING AND IDENTIFICATION TAPE

 A. Provide detectable aluminum foil plastic backed taptape manufactured specifically for warning and ideshall be detectable by an electronic detection inst

inches minimum width color coded for the uti

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inches minimum width, color coded for the utiidentification imprinted in bold black letters continutape length. Warning and identification shall read CBELOW OR similar wording. Use permanent codemoisture and other substances contained in trench ba

2.13 NAMEPLATES

 A. Provide laminated plastic nameplates for equipment, Nameplates shall be melamine plastic, 0.125 inch thSurface shall be matte finish. Corners shall be squaengrave into the white core. Minimum size of nameLettering shall be minimum of 0.25 inch high normalchart and schedule for each system. Frame chartslocate near each system as directed by Contractineach chart and schedule.

PART 3 - EXECUTION

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

above. Provide flanges or unions at valves, straineas indicated.

1. Fire Protection: Conform to safety and fireDepartment when work is in progress. Obtabefore performing welding or burning. Piping inspected for explosive vapors prior to work anthe work. If in the opinion of the Contracting Off

work shall cease until such condition has been 2. Safety: NFPA 30; safety rules shall be strictly o3. Cutting Existing Pipe: Perform initial cutting

pipe cutter, using a nonflammable lubricant. piping with a gas barrier plug in accordance piping shall be purged with carbon dioxideprocess. Complete method of cutting, sealing,advance of the actual work.

4. Cleaning of Piping: Keep interior and ends oaffected by the Contractor's operations thoroumatter during installation by means of plugs owork is not in progress, securely close open eentry of water and foreign matter. Inspect pipin

5. Demolition: Remove materials to avoid damagexisting work damaged by the Contractor's opeconstruction.

3.2 PIPING

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3.2 PIPING

 A. Test, inspect, and approve piping before burying, fittings for changes in direction of piping and forconnections in steel piping may be made with forgedbranches two or more pipe sizes smaller than mainforged, flared for improved flow where attached to thstrains, and designed to withstand full pipe burstingwill not be permitted. Jointing compound for pipe thpaste. Pipe nipples 6 inches long and shorter shall changes in piping sizes through tapered reducing pip

1. Fittings and End Connections: For sizes lessfittings and end connections. For sizes onesocket-welding or buttwelding fittings and enconnections for threaded valves, strainers,equipment. For sizes 2.5 inches and larger, p

connections; provide flanged connections for fla

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

Size (Inches) Under 1.5 2 3 4 6

  Maximum PipeSpacing (Feet) 7 9 10 12 14 1

4. Buried Piping System: Installation includingbackfill shall be in accordance with ASME B31.

3.3 FIELD QUALITY CONTROL

 A. Inspections

1. Prior to initial operation, inspect piping systespecifications, and manufacturer's submittals.

B. Tests

1. Piping Tests: Before final acceptance of the woto demonstrate compliance with contract requirpiping system at not less than 415 psig in accoRP 1110, with no leakage or reduction in gage and dry piping before placing in operation. Flu8 fps. Correct defects in work and repeat teswith contract requirements. Furnish potablconnecting devices, and personnel for tests. R

may be damaged by water used for testing.

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y g y g

2. Protective Coatings of Buried Piping System Tcoatings with a silicone rubber electric wire brtester of an approved type. Tester shall be buzzer, or other audible signal which will souminimum testing voltage equal to 1000 timescoating thickness in mils. Tester shall be a tcannot be made. Calibration by tester manufaintervals. Maintain the battery at ample chaduring tests. Areas where arcing occurs shidentical to that being used for field joints. surfaces, including field joints, for holidays. Pro

3. Cathodic Protection Tests: Perform test connections prior to backfill.

4 Equipment Acceptance Tests: [ ]

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Notify the Contracting Officer in writing at least connections are required. Obtain approval befomaterials required to make connections into existingbackfilling, compacting, and other incidental labor as

END OF SECTION 02555

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 13080 - SEISMIC PROTECTION FOR MISCELLA

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope,

mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this speThe publications are referred to within the text by the

1. ASTM INTERNATIONAL (ASTM)

a. ASTM A 36/A 36M (2001) Carbon Structb. ASTM A 53/A 53M (2002) Pipe, Steel,

Coated, Welded and Seamlessc ASTM A 153/A 153M (2001a) Zinc Coa

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c. ASTM A 153/A 153M (2001a) Zinc CoaHardware

d. ASTM A 307 (2002) Carbon Steel BolStrength

e. ASTM A 325 (2002) Structural Bolts, Minimum Tensile Strength

f. ASTM A 325M (2000) High-Strength B(Metric)

g. ASTM A 500 (2001a) Cold-Formed WStructural Tubing in Rounds and Shapes

h. ASTM A 563 (2000) Carbon and Alloy i. ASTM A 563M (2001) Carbon and Alloy  j. ASTM A 572/A 572M (2001) High-St

Vanadium Structural Steelk. ASTM A 603 (1998) Zinc-Coated Steel. Iron Alloy-Coated (Galvannealed) by the

m ASTM E 488 (1996) Strength of Anc

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

a. TI 809-04 (1998) Seismic Design for B

1.2 SYSTEM DESCRIPTION

 A. General Requirements

1. The requirements for seismic protection measu

be applied to the mechanical equipment and sySEISMIC PROTECTION FOR MECHANICAequipment and systems outlined in Section FOR ELECTRICAL EQUIPMENT, and thesystems listed below. Seismic protection reqwith TI 809-04 and additional data furnished bybe provided in addition to any other requiremethese specifications. The design for seismicSeismic Use Group [I] [II] [IIIH] [IIIE] building coefficients for S<SBS>MS</SBS>  = [_____]Resistance to lateral forces induced by earwithout consideration of friction resulting fromformulas, for Ground Motions A and B in Chapspectral response acceleration parameters forbuilding, not for equipment in the building; theto the formulas shall be required.

B. Miscellaneous Equipment and Systems

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1. The bracing for the following miscellaneous developed by the Contractor in accordancespecification:

a. Storage cabinetsb. Ornamentationsc. Storage Racksd. Signs and Billboardse. Shelvingf. Furnishingsg. Partitions

1.3 SUBMITTALS

 A. Government approval is required for submittals with

having a "G" designation are for information only or

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

c. Equipment Requirements; G,

B. Detail drawings along with catalog cuts, templatedetails, as appropriate, for the items listed. Submittaindicate thickness, type, grade, class of metal, aconstruction details, reinforcement, anchorage, andbuilding construction. For equipment and systperformance objective higher than life-safety, the d

registered engineer who stamps the calculations requ

1. SD-03 Product Data

a. Bracing; G,b. Equipment Requirements; G,

C. Copies of the design calculations with the detail stamped by a registered engineer and shall verify thto which bracing is attached for carrying the load from

1.4 EQUIPMENT REQUIREMENTS

 A. Rigidly Mounted Equipment

1. The following specific items of equipment: [_contract shall be constructed and assembled

specified in TI 809-04, Chapter 10. For anyattached on both sides of a building expansi

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attached on both sides of a building expansielectrical conduit, etc., that are capable of accto the full width of the joint in both orthogonal d

B. Nonrigid or Flexibly-Mounted Equipment

1. The following specific items of equipment toconstructed and assembled to resist a horizo

the operating weight of the equipment at theequipment.

PART 2 - PRODUCTS

2.1 BOLTS AND NUTS

 A. Squarehead and hexhead bolts, and heavy hexag

B18 2 2 or [ASTM A 307 for bolts and ASTM A 56

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1. Plates, rods, and rolled shapes, [ASTM A 36Grade 503]. If the Contractor does the des ASTM A 572/A 572M, grade 503 will be allowed

2. Wire rope, ASTM A 603.3. Tubes, ASTM A 500, Grade [B] [_____].4. Pipes, ASTM A 53/A 53M, Type [E] or [S], Grad5. Light gauge angles, less than 1/4 inch thicknes

PART 3 - EXECUTION

3.1 BRACING

 A. Bracing shall conform to the arrangements shownsecured with not less than two 1/2 inch bolts.

3.2 BUILDING DRIFT

 A. Sway braces for a piping run shall not be attached toof a building that may respond differentially during anis provided.

3.3 ANCHOR BOLTS

 A. Floor or pad mounted equipment shall use cast-

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specified below. Two nuts shall be provided on eacto ASTM A 307. Anchor bolts shall have an embedd12 times nominal diameter of the bolt. Anchor boltsequipment foundation piers or pads shall either efoundation shall be increased in depth to accommoda

B. Expansion or chemically bonded anchors shall n

accordance with ASTM E 488 has been provided to anchor and application. Expansion or chemically boresist pull-out in overhead and wall installations if thtemperature sensitive epoxies and the location Expansion and chemically bonded anchors shall bemanufacturer's recommendations. The allowable spacing between anchor bolts and the distance bnearest edge, as specified by the manufacturer.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

wrenches shall be calibrated at the beginning performed. Torque wrenches shall be recwhenever tests are run on bolts of various diabe between 20 and 100 percent of wrench careached within one half turn of the nut, except shall reach their torque by one quarter turn of tsimilar anchors not previously tested shall be tepass. Failed anchors shall be retightened and

the anchor still fails the test it shall be replaced3. Expansion and chemically bonded anchors sh

load using a hydraulic ram attached to the ancanchors, but not less than 3 per day shall be tethe anchor without removing the nut; when tharemoved and a threaded coupler shall be instaoriginal nut. The test setup shall be checkerestrained from withdrawing by the baseplatfixtures. The support for the testing apparatuembedment length away from the bolt being teloaded to 1 times the design tension value for tno observable movement at the test load. Ifanchors not previously tested shall be tested uFailed anchors shall be retightened and reteanchor still fails the test it shall be replaced.

3.4 RESILIENT VIBRATION ISOLATION DEVICES

 A. Where the need for these devices is determined, bas

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,seismic forces, selection of anchor bolts for vibration for equipment base and foundations shall follow the  ANCHOR BOLTS, except that an equipment weigequipment weight shall be used.

B. Vibration isolation devices shall be selected so tequipment from the static deflection point shall be 0.5

3.5 SWAY BRACES FOR PIPING

 A. Transverse sway bracing for steel and copper pipe sexceed those shown on the drawings. Transverse sother than steel and copper shall be provided at inspacing as specified in Section 15400A PLUMBINGshall consist of at least one vertical angle 2 x 2 inch

angle of the same size

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

D. Maximum Length for Anchor Braces

MaType Size (Inches) (Fe

 Angles 1-1/2 x 1-1/2 x 1/4 2 x 2 x 1/4 2-1/2 x 1-1/2 x 1/4

3 x 2-1/2 x 1/4 3 x 3 x 1/4

Rods 3/4 7/8

Flat Bars 1-1/2 x 1/4 2 x 1/4 2 x 3/8

Pipes (40S) 1 1-1/4 1-1/2 2

E. Bolts used for attachment of anchors to pipe and stinch diameter.

3.6 EQUIPMENT SWAY BRACING

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 A. Equipment sway bracing shall be provided for itemsroof structural systems, including light fixtures. Brawire rope, bars, or pipes arranged as shown and sethan 1/2 inch bolts. Sufficient braces shall be prhorizontal force as specified in Chapter 10 of TI 809-0stress of bracing components. The Contractor shforce calculations in accordance with Chapter 10 of Tproject. Details of equipment bracing shall be subbracing with vertical supports, these items may be s45 degrees directed up and radially away from equiin 90-degree intervals on the horizontal plane, bisecthe equipment, provided that supporting memberoperating weight of equipment when hangers are incl

B Floor mounted equipment shall be bolted to the floo

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 15491H - FUEL-OIL SYSTEM

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope,

environmental conditions and seismic requirements.

Include references to all applicable related sections, sudivisions 2 through 14 sections, mechanical division 15sections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this speThe publications are referred to in the text by the bas

1. AMERICAN NATIONAL STANDARDS INSTITU

a. ANSI A13.1 (1996; R 2002) ScheSystems

b. ANSI B16.24 (2001) Cast Copper A

Fittings Class 150, 300, 400, 600, 900, 15c. ANSI B18.2.1 (1996; A 1999) Square

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S 8 ( 996; 999) SqSeries

2. AMERICAN PETROLEUM INSTITUTE (API)

a. API Std 599 (2002) Metal Plug VaWelding Ends

b. API 600 (2001) Bolted Bonnet SteeNatural Gas Industriesc. API RP 1110 (1997) Pressure Testing d. API RP 1615 (1996) Installation of U

Systems

3. ASME INTERNATIONAL (ASME)

a. ASME B1.1 (1989) Unified Inch Screw

F )

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

i. ASME B18.2.2 (1987; R 1999) Square a j. ASME B31.1 (2001) Power Pipingk. ASME B31.3 (2002) Process Pipingl. ASME B31.4 (2002) Piping Transp

Hydrocarbons and Other Liquidm. ASME B40.1 (1991; Special Notice 19

Dial Type - Elastic Elementn. ASME BPVC SEC VIII D1 (1998; Adden

Vessel Code: Section VIII Pressure Vesso. ASME BPVC SEC IX (1998; Addenda

Code: Section IX Qualification StandProcedures, Welders, Brazers, and Weld

4. ASTM INTERNATIONAL (ASTM)

a. ASTM A 36/A 36M (2002) Carbon Stb. ASTM A 53/A 53M (2002) Pipe, Ste

Coated, Welded and Seamlessc. ASTM A 194/A 194M (2003) Carbon a

High-Pressure and High-Temperature Sed. ASTM A 307 (2002) Carbon Steel Bol

Strengthe. ASTM B 88 (2002) Seamless Copperf. ASTM B 88M (1999) Seamless Copper

5. NATIONAL FIRE PROTECTION ASSOCIATIO

a NFPA 30 (2000) Flammable and Comb

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a. NFPA 30 (2000) Flammable and Combb. NFPA 31 (2001) Installation of Oil Burnc. NFPA 37 (2002) Standard for the In

Combustion Engines and Gas Turbines.d. NFPA 70 (2002) National Electrical Coe. NFPA 780 (2000) Installation of Lightnin

6. THE SOCIETY FOR PROTECTIVE COATINGS

a. SSPC SP 10 (2000) Near-White Blast b. SSPC Paint 20 (1991) Zinc-Rich Primers

"Organic")

7. SHEET METAL & AIR CONDITIONING ASSOCIATION (SMACNA)

SMACNA S i i R t i t M l (1998

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. This Section includes storage tanks, fuel oil, tank specialties for fuel-oil distribution.

1.3 DEFINITIONS

 A. The following are industry abbreviations for fuel tanks

1. AST: Aboveground, fuel-oil storage tank(s).

2. UST: Underground, fuel-oil storage tank(s).

B. The following are industry abbreviations for plastic ma

1. PE: Polyethylene plastic.2. PTFE: Polytetrafluoroethylene plastic.3. RTRP: Reinforced thermosetting-resin pipe.4. TFE: Tetrafluoroethylene plastic.

1.4 SYSTEM PERFORMANCE REQUIREMENTS

 A. Aboveground, Fuel-Oil Distribution Piping Minimumpsig.

B. Double-Contained-Piping, Carrier-Pipe Minimum Wor

C. Double-Contained-Piping, Secondary-ContainmentPressure Rating: 5 psig.

D. Vent, Gage and Fill Piping Minimum Working-Pressu

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g g g

E. Minimum Test-Pressure Rating for Inner Tank, Small

F. Minimum Test-Pressure Rating for Containment She5 psig.

1.5 SUBMITTALS

 A. General: Submit each item in this Article accordingand Division 1 Specification Sections.

B. Product Data: Include identification materials andcapacities, pressure ratings, settings and operating c

1. Each type and size of fuel-oil storage tanks.

2 F l il t t k i d i lt

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1. Wiring Diagrams: For each item of equipmInclude ladder-type wiring diagrams for interlofinal installation. Differentiate between factory-

D. Welding Certificates: Copies of certificates for weldin

E. Test Reports: As specified in "Field Quality Control"

F. Maintenance Data: For accessories and specialties tspecified in Division 1.

1.6 QUALITY ASSURANCE

 A. Product Options: Drawings indicate size, profiles, fuel-oil distribution components and are based on spOther manufacturers' products with equal perfoconsidered. Refer to Division 1 Section "Substitution

B. Distribution Components: Listing/approval stamp, lagency acceptable to authorities having jurisdiction.

C. Electrical Devices, Components and Equipment: NFPA 70, Article 100, by a testing agency acceptable

D. Comply with ASME B31.1, "Power Piping," for fuerequirements.

E. Comply with NFPA 30, "Flammable and Combustib

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"Stationary Combustion and Gas Turbines" for desinspection and testing of fuel-oil distribution sycomponents.

F. Comply with NFPA 70, "National Electrical Code," fwiring and electrically operated devices.

G. Comply with requirements of the EPA and state aauthorities having jurisdiction. Include recordingmonitoring of tanks and piping.

H. Comply with requirements of the State and local b jurisdiction.

I. Welding: Qualify processes and operators accordi

V l C d S ti IX "W ldi d B i Q

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

K. The Contractor shall also be certified for the installaState in which installation occurs.

L. The Contractor’s workers involved in the actual remoof new tanks shall have current OSHA “HAZWOPER1910.120 (latest edition). Copies of current certifrequest of the Owner.

1.7 DELIVERY, STORAGE AND HANDLING

 A. Lift and support fuel oil storage tanks only at designashown on Shop Drawings. Do not move or lift tanks u

B. Preparation for Transport: Prepare storage tanks, afor shipping as follows:

1. Ensure that units are dry and internally protecte2. Protect against damage to threaded ends, flang3. Set valves and specialties in position for hand

and operating parts.

C. Deliver piping with factory-applied end caps. Maistorage and handling to prevent damage and entranc

D. Store valves and specialties with end protectors inspection; then reinstall for storage.

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E. Store valves and specialties indoors and maintain dew-point temperature. Support off ground or pavoutdoor storage is necessary.

F. Protect stored piping from moisture and dirt. Eleva

structural capacity of floor if stored inside. Suppobending.

G. Protect flanges, fittings and piping specialties from m

1.8 PROJECT CONDITIONS

 A. Perform site survey, research public utility records aContact utility-locating service for area where Project

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Coordinate pipe materials, sizes, entry locations andpiping systems.

B. Coordinate installation and set sleeves in poured-in-pcomponents as they are constructed.

C. Coordinate sizes and locations of concrete-anchorsInclude manholes, fill and sounding boxes and vent p

D. Work Interruptions: Leave fuel-oil distribution piping work occur while alterations or repairs are being mad

1.10 WARRANTY

 A. General Warranty: Special warranty specified in thisother rights Owner may have under other provisionshall be in addition to, and run concurrent with, othe

under requirements of the Contract Documents.

B. Special Warranty: Written warranty, executed by fagreeing to repair or replace tanks that fail in materiawarranty period, provided tanks are installed accinstructions. Failures include structural failures of taand collapse; and failure due to external and internfuel oils at temperatures not exceeding 150 degrees F

C. Warranty Period: 30 years from date of Substantial C

PART 2 PRODUCTS

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PART 2 - PRODUCTS

2.1 PIPING MATERIALS

 A. Refer to Part 3 "Piping Applications" Article for adouble-contained piping, and joining materials.

2.2 PIPES AND TUBES

 A. Steel Pipe: ASTM A 106, seamless, Schedule 40, Gr

2.3 PIPE AND TUBE FITTINGS

 A. Steel, Welding Fittings: ASTM A 234/A 234M, seamlwelding type or ASME B16.11, socket-welding type.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2.4 NON-METALLIC PIPING

 A. General:

1. The underground fuel piping shall be non-metabe secondarily contained.

B. Primary Pipe:

1. The primary pipe shall be suitable for use witpressurized submersible pumping system.

2. The piping system shall be UL/ULC listed fgasoline and most petroleum products, as wellpercent.

3. The primary pipe shall be a composite construcNylon 12, an intermediate layer of braided Nypolyethylene.

4. A permeation barrier layer shall inhibit permewalls.

C. Secondary Containment Jacket:

1. The secondary containment jacket shall be extr2. The jacket shall be air testable.3. The jacket shall be separated from the primary 4. Longitudinal stand-off spokes shall separate th

 jacket.5. The jacket shall have a polyethylene liner, a p

l th l ff d t l

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polyethylene scuff guard outer layer.

D. Connection Fittings:

1. The connection fittings shall be located at individual length of pipe and shall terminate w

building. They shall be accessible for testing o2. They shall be fabricated of U.N.C. 360 Brass.3. Fittings shall be two piece construction, swive

viton “O” rings which provide the seal between 4. Connection to pipe shall be by means of a ba

chrome nickel plated high pressure clamp and f

2.5 JOINING MATERIALS

A G k f Fl d J i F ll f d f i

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Tank, Pipe Connectors: Comply with UL 567, connection to equipment.

B. Piping, Flexible Connectors: Fabricated from mateincluding 150 psig minimum working-pressure ratinginch NPS and smaller and flanged ends for 2½ inch N

1. Stainless Steel Hose, Flexible Connectors:

tubing covered with stainless-steel wire braid.welded to hose.

C. Strainers: Duplex, full size of connecting piping. In3/64-inch perforations, except where other screens a

1. Pressure Rating: 200 psig WOG working pindicated.

2. Cast-iron body, with flanged ends.

D. Sight Flow Indicators:

1. Sight flow indicators shall be carbon steel bwheel. End fittings shall be 150 pounds flanindicated on the Drawings.

E. Pressure Gages:

1. Pressure and vacuum gages shall be suitableGages shall be liquid filled type, with twmovements set in brass cases with stop valv

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movements, set in brass cases, with stop valvPressure gages shall have 0-100 psi total diainches total dial graduation.

F. Y-Strainer for Connection Ahead of all Solenoid Valve

1. Provide 300 pounds WOG, bronze body withfittings shall be screwed (female NPT) or flange

2.7 VALVES

 A. General

1. The Contractor shall furnish and install valvesvalves that are necessary for proper operation

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

5. The Contractor shall supply the end user’s manufacturer’s maintenance instructions includinstructions.

B. Ball Valves:

1. Ball valves shall be of full-port design with threefittings. Valve body shall have encapsulated b

shall be of stainless steel construction. Seatsforced PTFE.2. End fittings to be either 150 lb. flanged or s

Drawings.3. Ball valve seating shall be of pre-compresse

adjustable with standard hand tools without rDesign shall allow for repetitive adjustmentsreplacement is necessary. Floating ball type de

4. Stem shall be of positive sealing, mechanicall

Belleville spring washers and double TeUnloaded stem packing designs are not accept

5. Stem shall be of internal entry, anti-blowout dremoval and possible personal injury while the v

6. Manual operator unless otherwise indicated on

C. Multi-port Ball Valves: True four and five seated 3, 4and gasketed valve to allow removal of the body Carbon steel body and end fittings. End fittings shaweld as indicated on the Drawings. Reinforced Tfiguration as shown on the Drawings. Stainless steeless otherwise indicated on the Drawings

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less otherwise indicated on the Drawings.

D. Swing Check: Valve 2½ inches and smaller, 400 pouable bronze disk and integral seats. Valve shall bevertical or horizontal position. End fittings shall be scindicated on the Drawings.

E. Lift Check Valve 2½ Inches and Smaller: 400 pound bronze disk and integral seats. End fittings shall beas indicated on the Drawings.

F. Relief Valve 2½ Inches and Smaller: 300 psig bronspring. End fittings shall be screwed (female NPTDrawings.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

B. Foot Valve 1½ Inches and 2-Inches: Double poppet mesh screen. Replaceable seats, plated cast iron boand monel screen.

C. Anti-Siphon Valve: Zinc plated cast iron body, precisseals. Valve spring setting shall be field adjustable.

D. Fusible Link Valve (½ inch through 2-inch): Full port

stainless steel trim and TFE seat. End fittings sha(female NPT) as indicated on the Drawings. Fusible 165 degrees F with torque handle set for spring-to-clo

E. Overfill Prevention Valve:

1. Valve shall restrict the flow rate when tank is 9when the tank is filled to 95% capacity.

2. Provide longer tube unit for tank diameters grea

2.9 SUBMERSIBLE/CENTRIFUAL PUMPS

 A. Pump shall be of submersible centrifugal type whichthreaded tank opening. Size shall be from  througDrawings.

B. Pump shall be two-stage, self-lubricating and easilywithout disconnecting discharge piping. The pum

readily separable from the pump column pipe to allothe pump and motor.

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C. Impellers shall be either splined or keyed to the pumprotation. Diffusers shall be tightly secured to theprevent rotation.

D. Pump intake inlet shall be horizontal to prevent drawi

E. Manifold assembly shall be completely sealed againsand exterior water leakage into the storage tank.standard 3 inch NPT. The head shall have a built-pressure relief valve which relieves to 8-14 psi, aprimer when required.

F. The motor shall be 208/230 volt, 60 cycle, 34capacitance type, continuous duty, rated explosi

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1. Drive: Direct drive, close coupled.

B. motor: Split phase for single-phase motors; capaenclosed for 3-phase motors.

2.11 DOUBLE WALL UNDERGROUND STORAGE TANK

 A. General:

1. The double wall storage tanks shall be T

fabricated, true double walled (360) secondarUL standards and so labeled and listed for undtank construction shall be compatible with all  jacket shall cover all straight and girth seams. any kind through the jacket to the tank exceptmonitoring the interstitial space. The primary ashall conform to UL l58 standards. The piping

tank primary wall. Double wall steel tanks shpotentially corrosive water vapor from the intshall have the capacities, maximum overall dshown on the Drawings. Tank shall be built in and ACT-100-U standards.

B. Interior Corrosion Protection:

1. It is the responsibility of the tank manufactucompatible with the product being stored in thtests to insure coating integrity.

2 Primary and secondary welds shall be made i

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2. Primary and secondary welds shall be made i1746 for corrosion resistant composite systemsteel wear (striker) plates shall be centered aEach striker plate shall be at least 12” x 12” inplates shall be sandblasted to insure that they a

C. Electrical Isolation:

1. Each tank shall be equipped by the tank manuinsulate the tank from piping and other attachm

D. Exterior Coating:

1. The entire exposed exterior surface of each taapplied fiber-thane shell bonded firmly to the s

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4. Any defects shall be repaired and the coating re5. The coating shall be factory checked with a ba

to assure compliance with the manufacturestandard for cured resin. Tank manufacturer sholiday and hardness testing. Any coating datransit or installation activities shall be repaireContractor in strict accordance with the manufa

6. The tank manufacturer shall provide personnel

site spark test of the tank exterior coating; necbe provided by the tank manufacturer.

E. Ancillary Devices:

1. Each tank shall include a 2 inch diameter leak dlugs, all connections for product removal, fill areading liquid level gage system. The tank shmanholes as indicated on the Drawings. Man

with bolts to attach to 48” diameter pipe/contanumber, type and location shall be as shown orequired for an approved installation.

F. Labeling:

1. The tank shall have a label of permanent concover which contains the maker’s name and ametal of which the tank is construction, montcapacity in gallons, serial number and standaralso be permanently marked in a prominent plaimportant handling, safety, manufacturing and

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po ta t a d g, sa ety, a u actu g a dweight shall be labeled near the lifting lugs.

G. Factory Pressure Tests:

1. To assure tightness of all welds, seams and

tested with compressed air at 5 psig, or greatpermanent placement of the secondary jacket. shall be soaped during the pressure test peSubsequent to placement of the secondary jacfactory pressure tested to 3 psig with fittings, wouter jackets soaped and inspected for bubblaccordance with UL 58 standards and promanufacturer to be tight. The manufacturer scertifications of all test results in writing to the O

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

straps. Hold down concrete slab, straps and abuoyant force on empty installed and backfigrade level.

I. Manholes:

1. Storage tank manhole shall be factory installed 2. Number, size and location shall be as shown

Manhole shall be sealed with a gasket matercontents. The gasket shall be not less thanstainless steel. Gaskets, bolts and covers shal

J. Warranty:

1. Primary and secondary containment shall carrycovering materials and workmanship. The manufacturer or have an equivalent third p

failure such as cracking, rupture or collapse covering leakage due to corrosion for 30 yeinstalled in accordance with the manufacturecontainment monitoring system shall carry materials and workmanship.

K. Markings:

1. Adjacent to each threaded tank opening, the f

tank: non-metallic, dielectric fitting, do not remo

L. Compliance Regulations:

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1. Construction and testing of the tanks shall issues of the applicable guidelines, rules and scodes:

a. Underwriters’ Laboratories, Inc. UL 58, Ub. National Fire Protection Association Specc. United States UPA Regulations.d. State Fire Marshall Codes.e. Any other applicable Federal, State or loc

M. Installation:

1. Tanks shall be installed in accordance with the

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2.12 EXTERIOR ABOVEGROUND DOUBLE WALL STOR

 A. General:

1. The aboveground, double walled, storage tankor cylindrical tank.

2. The storage tank shall consist of a fully listed, surrounded by six inches of lightweight concretshell.

3. The tank shall bear the appropriate UL label for4. The tank shall comply with UL2085, UL142/NF

Standards and shall have primary and emergeon the secondary tank.

5. The tank shall have the capacity, dimensions the drawings and specifications.

6. Provide integral spill containment fill box.7. Provide access stairs and platform, hot dip galv

drawings. Stairs and platform shall comply wifurnished by the tank manufacturer.

B. Tank Coating

1. The tank exterior shall be factory coated by the2. Provide one gallon of finish paint at each locatio

C. Concrete Fill

1. Tank shall be enclosed on all sides, top and bconcrete.

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2. Tank shall be filled at the factory under factoimpact and projectile resistant lightweight concr

D. Labeling

1. Each tank shall have a label of permanent conmaker’s name and address, month and year gallons, serial number and standards of conlabeled.

E. Anchoring

1. Saddles and anchoring channels shall be prangles, nuts, bolts and washers, shall be

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

installed in accordance with the manufacturer’s

G. Compliance Regulations

1. Construction and testing of the tanks shall issues of the applicable guidelines, rules and scodes:

a. Underwriters Laboratories, Inc. UL 2085 ab. National Fire Protection Association Specc. Uniform Fire Code A-11-F-1 (also call UFd. U.S. EPA regulations.

2.13 DAY TANKS

 A. General:

1. The aboveground, double walled storage tanktank.

2. The storage tank shall consist of a fully listed, d3. The tank shall bear the appropriate UL label for4. The tank shall comply with UL 142/NFPA

Standards and shall have primary and emergeon the secondary tank.

5. The tank shall have the capacity, dimensions the Drawings and in the Specifications.

B. Tank Coating:

1 Th t k t i h ll b f t t d b th

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1. The tank exterior shall be factory coated by the2. Provide one gallon of finish paint at each locatio

C. Labeling:

1. Each tank shall have a label of permanent conmaker’s name and address, month and year gallons, serial number and standards of conlabeled.

D. Anchoring:

1. Saddles and anchoring channels shall be proangles, nuts, bolts and washers shall be

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

b. National Fire Protection Association Specc. Uniform Fire Code A-11-F-1 (also called Ud. United States EPA Regulations.

F. Warranty

1. Written warranty, executed by the fuel oil darepair or replace day tank and/or components twithin the specified warranty period, prmanufacturer’s written instructions.

2. Warranty Period: One year from date of shipme

2.14 FUEL-OIL STORAGE TANK FITTINGS AND ACCES

 A. Tank Manholes (Piping): 24 inch diameter, bolted, containment sump operation.

B. Threaded pipe connection fittings on top of tanks, forand gauging, in locations and of sizes indicated. shipping.

C. Striker Plates: Inside tank, on bottom below fill, souopenings.

D. Lifting Lugs: For handling and installation.

E. Containment Sumps: Fiber glass or PE, sump barequired, sump top, lid and gasket-seal joints. Ipenetrations through sidewalls.

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F. Bulkhead Fittings: Two-part pipe fitting for field assempipe. Include gaskets shaped to fit sump sidewarequired for liquid-tight pipe penetrations.

G. Filter Mat: Geotextile woven or spun filter fabric, in total weight of 3.0 oz./sq. yd.

2.15 FUEL-OIL STORAGE TANK FITTINGS & ACCESSO

 A. Tank Manholes: 22- to 24-inch diameter; bolted, flangof tank.

B. Threaded pipe connection fittings on top of tanks, for

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2.16 FUEL-OIL TANK SPECIALTY FITTINGS

 A. Spill-Containment Fill Boxes:

1. Provide spill containment fill box,2. Fill box shall equipped with a hinged lockable

drain valve.3. Capacity shall be 15 gallons. (UST) or 5 gallons

B. Supply and Sounding Drop Tubes: Fuel-oil suppterminating 6 inches above bottom of tank, and with e

C. Pipe Adapters and Extensions: Compatible with pipin

D. Weatherproof Vent Cap:

1. Emergency Vent:

a. 8 ounce/square inch, or as approveconstructed with aluminum bodies, cast Sizes shall be as indicated on the Drawin

E. Fill Caps: Locking type cap for standard padlock and

F. Monitoring Well Caps: Locking pipe plugs and manho

2.17 GRADE MANHOLES

 A. Cast Iron Frame and Cover: Heavy-duty, water-regasket and bolted cover; 24-inch-diameter inside ope

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gasket and bolted cover; 24 inch diameter inside opeheight.

2.18 LEAK-DETECTION AND MONITORING SYSTEM

 A. The in-tank monitoring system shall be a combined detection system for use in up to eight tanks.

B. Hardware: The control unit shall be wall mounted an

1. A liquid crystal display for on-site viewing of ainformation.

2. An internal printer with built-in take up sponotification.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

sensors.9. Underwriter's Laboratory (UL) listed.10. Intrinsically safe.11. An RS-232 communications device for data

printing device.

C. Tank Probe: The tank probe shall be magnetostrictivfollows:

1. Capable of utilizing standard gas and oil-res AWG and 18 AWG for field connections.

2. No more than two wires between each probe a3. Leak detection capability of 0.1 gph.4. Third-party certification according to U.S. EPA's

D. Single-cable interstitial sensing elements capable of d

1. Capable of utilizing standard gas and oil resista2. No more than two wires between each sump

control console.3. Furnish and install sensing elements as schedu

E. Operating Capabilities:

1. The system shall have the capability to monitproduce a combination of automatic and m

following information:

a. Gallons of fuelb Inches of fuel

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b. Inches of fuelc. Inches of waterd. Temperaturee. Ullagef. Time and date

g. Tank identificationh. Fuel identificationi. Temperature compensated fuel volume j. Last inventory increase amountk. 90-percent ullage

2. The ability to perform both automatic and manuin compliance with Federal EPA Regulations 4leak analysis report. This leak analysis report

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

10. Store in memory at least 10 delivery reports pe11. Provide alarm history reports on demand, locall12. Provide flexible console profile setup with U.S. 13. The system shall include emergency generator14. Programmable alarm limits to warn of:

a. Leaksb. Overfillsc. High waterd. Low inventorye. Theftsf. External input alarmg. High level

15. System must be capable of the following perfogallon tank:

a. Height of Fuel: Plus or minus 0.1-inch.b. Volume of Fuel: Plus or minus 15 gallonsc. Height of Water: To 5-inches.d. Fuel Temperature: To +/-1.5 degrees F.e. Time: Plus or minus 1 min/week.f. Leak detection rate of 0.1 gph or greater.

16. Automatic inventory increase (delivery) report c

a. Delivery start time and dateb. Beginning inventoryc. Fuel temperatured Delivery end time and date

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d. Delivery end time and datee. Ending inventoryf. Ending fuel temperatureg. Net increase

2.19 OVERFILL ALARM

 A. The overfill alarm shall be manufactured by the leamanufacturer. The unit shall be complete with reacknowledgement switch.

B. The reset switch shall silence and reset the alarm hoautomatically silence and reset the horn.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2. The supplier shall supply the system as a sincomplete and operating system from a single m

B. Submittals:

1. Material lists and manufacturers’ catalog descri

a. Filtration removal in microns for each filteb. Flow capacity.c. Operating temperatures.d. Controller performance.e. Emulsion water removal.

2. Shop drawings with installation details include:

a. Overall width, length and height.b. Mounting hole locations and anchorage d

c. Plumbing connections.d. Electrical connections.e. Total wet and dry weight.f. Complete electrical and piping schematic

C. Spare Parts:

1. Furnish the following spare parts:

a. Six of each type of filter.

D. Scope:

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1. Provide and install the automated fuel monitoeach fuel source complete with multiple stcirculating pump, industrial PLC (programmacentral monitoring communications port, con

gages, connections, leak detection sensors, and appurtenances which will result in a comple2. Provide and install fuel treatment package for t

fuel oil tank. The fuel treatment package shalfungus and prevent organic contamination in th

3. Provide on-site a 55 gallon Xsorb Response Sfor stored fuel oil.

E. Fuel Monitoring and Maintenance System

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

d. 2 micron fine finish emulsion water remocanister.

e. High water alarm.f. Change filter alarm.g. Leak alarm.

2. The electric motor shall be 1½ horsepower, 2motor shall have a starter with thermal overloathe PLC.

3. System control circuit shall be 120 VAC.4. The combination mechanical gage and e

polycarbonate glass case with a stainless polycarbonate lens.

5. Control box enclosure shall be metal. Seapolyurethane gaskets. Cover screws shall be u

F. Fuel Treatment Package:

1. The fuel treatment shall be equivalent to treatment package for organic contamiorganometallic compounds, manganese and otcompletely soluble in fuel oil and can be added

G. Spill Response Kit:

1, The spill response kit shall be equivalent to

containing a 55 gallon drum of absorbents to inglasses and gloves.

H. Fuel Storage Base, Underground Tank

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g , g

1. The automated fuel monitoring and maintenanwired in a NEMA/CSA Type 4, Type 12 and Tycontainment area ensuring environmental prot

stages of decontamination at a minimum:

a. 150 micron cartridge type strainer/water b. Bulk water and large particulate removalc. 10 micron 95% water removal medial spid. Entrained water and particulate removal.e. 2 micron 99% water removal, fine finish m

element.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

and before shipment.

C. Perform factory tests, according to UL 142 and STI shipment.

D. Perform factory tests, according to UL 142 and UL shipment.

2.22 FUEL OIL SYSTEM CONTROLS

 A. System Configuration

1. Each of the day tanks in the fuel distributiondedicated control panel. The control panel shfor the day tank independently of other day tank

2. Main tank selection shall be provided by a selection and pump operation only. This co

control for any day tanks or other devices in the

B. Controls

1. General: The control panels shall be factory asa NEMA 4 enclosure. All control devices shaterminal strip. All panel factory wiring shall labeled wiring diagrams shall be included with t

2. Automatic Commissioning Feature: The day ta

with an automatic commissioning feature that the control system. The automatic commissioall valves, level control devices, level alarms, the panel without manual intervention from the

f f

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automatically drain fuel from the tank by usreturn pumps or automatic control valves. Duall programmed actuation levels shall be tespanel.

3. Shop Drawings: Provide shop drawings inconditions. Shop drawings shall include:

a. Complete ladder diagram depicting all cothe power circuits and control circuits.

b. Scaled drawing of the control panel internc. Full scale color drawing of the control pand. Complete material list of all components

number.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

through the PLC. Fuses are not an acceptable7. Pilot Lights: All indicator lights shall be LED.

illuminate all lights simultaneously for testing.8. Alarm Horn: All alarm conditions shall be accom

horn may be silenced by a “Silence Button”.9. Panel Face Graphics: Each control panel sha

components being controlled. The graphic dispprinted for the specific application, including aThe display shall be permanently attached toindicator lights for all conditions both normal alocated adjacent to the devices they depict oTouch screens are not acceptable for this purpo

10. Internal Modem: Each control panel shall be eqallow remote access to the PLC programming need not be permanently connected to a phonemay be connected to the modem as requireremote interrogation of the PLC for the pur

problems.11. Communication Between System Control Pa

required to be shared between control panelpanel to pump control panel to start fuel communication bus.

12. Control Valves: Day tank control valves shaValves shall have stainless steel bodies. All with diesel fuel and kerosene. Valve actionreturn actuators. Valve position indication sswitch in the valve actuator.

13. Day Tank Level Controls: Level controls shall bIndividual contact type float switches are not ac

14. Day Tank Fuel Level: An LED readout shall d

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ytank. Indication shall read in gallons to the nea

15. Day Tank Control Panel:

a. General: The day tank control panel sha

VAC power sources. Logic control shall with any required expansion modules. PLC status to be viewed remotely andremotely. Dual ultrasonic level transmittfor control of the system. A failure ofsystem operation.

b. Sequence of Operation: Fuel level in the75% and 85% capacity by volume. ThereCV-2, piped into parallel fluid circuits to t

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

are de-energized and the pump svalves close and pumps shut down

c. Alarm Conditions: Alarm conditions shallthe graphic control panel display. The lthe alarm condition clears and the resealarm at the control panel shall remain following alarm conditions shall be provid

1) Day tank high level at 90%.2) Day tank low level at 60%.3) Day tank critical low level at 10%.

to interface with generator to autom4) Leak (fluid in day tank annular spac5) Control valve CV-1 fail.6) Control valve CV-2 fail.7) Control valve CV-1 circuit breaker t

8) Control valve CV-2 circuit breaker t9) Level transmitter ‘A’ fail.10) Level transmitter ‘B’ fail.

d. Remote Annunciation: The day tank cinterfacing with the building automationconditions shall be made available for conditions, alarm conditions, fuel level an

e. Automatic Commissioning Feature: A kecommissioning feature. In the event thcompletion, a manual override shall be return the system to normal operation.

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1) Activate key switch.2) All pilot lights illuminate and horn is3) Drain valve cycles open (or return

begins to lower.4) When fuel level reaches 60%, lowautomatically silences after five sedigital gage.

5) When fuel level reaches 10%, cri Alarm horn is automatically silencelevel in digital gage.

6) System stabilizes for 30 seconds.7) Automatic mode is restored to the

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

11) When the fuel level reaches 5transmitter ‘B’.

12) When the fuel level reaches 60%valves CV-1 and CV-2. Failure li Alarm horn is automatically silenced

13) The system stabilizes for 15 secocontrol valves. The day tank begreaches 85% (normal fill level), coenergize. System is a “Normal Fill

14) The system stabilizes for 15 seenergized. The system begins to 90%, high level alarm is activated. five seconds. Observe fuel level oCV-1 is de-energized.

15) Drain valve cycles open (or returnbegins to lower. Drain valve is reaches 85% (normal fill level).

16) Test complete.

16. Tank Selector and Fuel Pump Control Panel

a. General: A push-button shall be providedstorage tanks. The tank selector and powered by two diverse dedicated 120 Vshall be provided by two PLC’s alonmodules. PLC ‘A’ shall be the primary c

for the system. If PLC ‘A’ fails, logic coPLC ‘B’. A modem module shall alloremotely and program changes made reprovide interface capability to the buildin

d l diti

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and alarm conditions.b. Sequence of Operation: On initial sta

selected via push-button on the graphicfor the selected tank are initialized but do

from a day tank calling for refill. When received via the communications bus, antransfer pump is energized. When the dcomplete, the fill request signal is cancelle

1) Pump Starters: The pump startershoused in a dedicated enclosureequipped with a control transformeto allow any pump to be started ind

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4) Pump Manual Operation: Each of tHAND-OFF-AUTO switch on the poperates to allow the pump to be st

c. Return Valve Operation: A motor actuatefuel oil return and overflow to the selecontrol panel shall automatically cycle tank. End switches in the valve actuator the PLC. If the valve fails to cycle to the

local alarm is activated at the control pand. Alarm Conditions: Alarm conditions shall

the graphic control panel display. The lthe alarm condition clears and the resealarm at the control panel shall remain following alarm conditions shall be provid

1) Power Source ‘A’ Fail

2) Power Source ‘B’ Fail3) Power Source ‘A’ Circuit Breaker T4) Power Source ‘B’ Circuit Breaker T5) PLC ‘A’ Fail6) PLC ‘B’ Fail7) PLC ‘A’ Circuit Breaker Tripped8) PLC ’B’ Circuit Breaker Tripped9) Return Valve Synchronization Error10) Pump FOP-1A, Fail

11) Pump FOP-1B, Fail12) Pump FOP-2A, Fail13) Pump FOP-2B, Fail14) Pump FOP-1A, HOA Not in Auto15) Pump FOP 1B HOA Not in Auto

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15) Pump FOP-1B, HOA Not in Auto16) Pump FOP-2A, HOA Not in Auto17) Pump FOP-2B, HOA Not in Auto

e. Remote Annunciation: The day tank cinterfacing with the building automationconditions shall be made available for conditions, alarm conditions, fuel level an

PART 3 - EXECUTION

3.1 EARTHWORK

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Use flanges, unions, transition and special fittings, same or higher than system's pressure rating in aboapplications, unless otherwise indicated.

B. Aboveground, Fuel Oil Piping and Vent Piping: Use th

1. 2-Inch NPS and Smaller: Steel pipe, steel weld2. 2½ Inch NPS and Larger: Steel pipe, steel weld3. Secondary Containment Piping: Steel pipe, s

 joints.

C. Underground, Fuel Oil Piping: Use the following:

1. ½ to 3 Inch NPS: Flexible, double-contained pip2. 4 Inch NPS: RTRP double-contained piping.

D. Underground, Fuel Oil Tank Fill Piping: Use the follo

1. 4-Inch NPS and Smaller: RTRP and RTRP fitti

E. Underground, Gage and Vent Piping: Use the follow

1. 2 inch NPS and larger flexible pipe and fittingsvent piping, underground only.

3.4 VALVE APPLICATIONS

 A. Drawings indicate valve types to be used. Wheindicated, the following requirements apply:

1. Shutoff Duty: Use ball valves.

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y

3.5 JOINT CONSTRUCTION

 A. Refer to Division 2 Section "Utility Materials" for basic

B. Make bonded joints for RTRP piping with adheswritten instructions.

3.6 FUEL-OIL STORAGE TANK INSTALLATION (AST)

 A. Install fuel-oil storage tanks according to manufastandards specified.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

G. Install fuel-oil storage tanks according to STI R912.

H. Install fuel-oil storage tanks according to STI R912 an

3.7 FUEL-OIL STORAGE TANK INSTALLATION (UST)

 A. Install fuel-oil storage tanks according to manufastandards specified.

B. Excavate to sufficient depth for a minimum of 3 feetfinished grade. Allow for cast-in-place, concrete-balpea gravel between ballast base and tank. Extenaround perimeter of tank.

C. Set tiedown eyelets for hold-down straps in concretesteel.

D. Place 6 inches of clean sand or pea gravel on top of

E. Set tank on fill materials and install hold-down straps

F. Install piping connections.

G. Install tank leak-detection and -monitoring devices.

H. Install containment sumps.

I. Backfill excavation with clean sand or pea gravel in 1consolidate.

J. Install filter mat between top of backfill material and e

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K. Install fuel-oil storage tanks according to STI R821during tank placement and backfilling operations.

L. Install fuel-oil storage tanks according to STI R913 an

M. Install fuel-oil storage tanks according to STI R923 an

N. Install fuel-oil storage tanks with fiberglass-reinmanhole extensions, and manhole risers.

3.8 CONCRETE BASES

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

D. Refer to Division 2 Section "Utility Materials" for grout

3.9 PIPING INSTALLATION

 A. Install piping free of sags and bends.

B. Locate groups of pipes parallel to each other, spaced

C. Install fittings for changes in direction and branch con

D. Install rigid, underground, double-contained, fill and slope of 0.2 percent downward toward fuel-oil storage

E. Install flexible, double-contained, fuel-oil pipe at downward toward fuel-oil storage tank sump.

F. Install flexible, vent pipe at a minimum slope of 2 storage tank sump.

G. Assemble and install bulkhead fittings for pipe penetsidewalls. Follow fitting manufacturer's written inrequired for liquid-tight joints.

H. Install reductions in pipe sizes using eccentric reducside down.

I. Install tank, pipe connectors at piping connections to

J. Install piping, flexible connectors at piping conequipment. Use according to the following applicatio

1 St l Pi i St i l t l h fl ibl

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1. Steel Piping: Stainless-steel-hose, flexible conn2. Copper Tubing: Bronze hose, flexible connecto3. RTRP: Stainless steel hose or bronze hose, fle

K. Install double-contained piping according to manuassembly, joining, trench preparation and installation

L. Install and terminate double-contained piping at fsumps and at building.

3.10 VALVE INSTALLATIONS

A Install valves in accessible locations Protect valves

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Piping Connections: Make piping connections as follo

1. Install unions, in piping 1¼ inch NPS and smafinal connection to each piece of equipment hav

2. Install flanges, in piping ½ inch NPS and largerfinal connection to each piece of equipment hav

3. Install dielectric fittings to connect piping of diss4. Install flexible connectors where indicated.

D. Make connections to fuel oil storage tank leak-detect

E. Make electrical connections to pumps, control pmonitoring devices.

F. Electrical wiring, disconnect switches and motor cont

G. Ground equipment and AST.

1. Tighten electrical connectors and terminapublished torque-tightening values. If manuindicated, use those specified in UL 486A and U

3.12 LEAK-DETECTION AND MONITORING SYSTEM IN

 A. Install leak-detection and -monitoring systems accinstructions. Install alarm panel inside building where

1. Fuel Oil Storage Tanks: Install probes in interst2. Fuel Oil Storage Tanks: Install probes for single3. Fuel Oil Double Contained Piping: Install leak-

storage tank containment sumps.4 F l Oil D bl C t i d Pi i I t ll l

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4. Fuel Oil Double Contained Piping: Install leindicated.

5. Install liquid-level gage systems according to m

3.13 LABELING AND IDENTIFYING

 A. Equipment: Install engraved, plastic-laminate equipmand equipment.

1. Text of Signs: In addition to name of identifiedunits, inform operator of operational reqemergency precautions, and warn of hazards a

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

E. Refer to Division 2 Section "Earthwork" for warning ta

3.14 PAINTING

 A. Refer to Division 9 Section "Painting" for field-painting

B. Use materials and procedures in "Exterior Paint ScParagraph and "Full-Gloss, Alkyd-Enamel Finish" Su"Painting," using color selected by Owner or as requir

C. Paint AST and metal supports, except units with fcoating. Restore damaged finish to original condition

D. Paint aboveground pipe, fittings, valves and supports

3.15 FIELD QUALITY CONTROL

 A. Perform pressure test for tightness, with air, inert gaand NFPA 31 on tanks before installation. Apply soleaks. Do not exceed the following:

1. Tanks Smaller Than 12-Foot Diameter: 5-psig t2. Tanks 12-Foot Diameter and Larger: 3-psig tes

B. Repair or replace defective tanks and retest until ther

C. Test fuel-oil distribution piping according to NFPA 3and defects with new materials and retest until there a

D. Test and adjust leak-detection and -monitoring systedamaged and malfunctioning controls and devices.

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E. Report test results promptly in writing to Engineer and

F. The delivery system shall be flushed with the same ty

the system, until the fuel being delivered is “clean absence of any sediment or emulsion. Bright refersfuel that has no cloud or haze.

3.16 ADJUSTING

 A. Adjust controls and safety devices. Replace damagesafety devices.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

3.18 DEMONSTRATION

 A. Engage a factory-authorized service representative Owner's maintenance personnel to adjust, operate an

1. Train Owner's maintenance personnel on procup and shutting down, troubleshooting, serviciequipment and pumps.

2. Review data in maintenance manuals. Refe

Closeout."3. Review data in maintenance manuals. Refer

and Maintenance Data."4. Schedule training with Owner with at least seve

END OF SECTION 15491H

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16050 - BASIC ELECTRICAL MATERIALS AND M

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this specthe latest version of the reference publication shall apto in the text by the basic designation only.

1. AMERICAN SOCIETY FOR TESTING AND MA

a. ASTM D 709 Laminated Thermosetting

2. U.S. NATIONAL ARCHIVES AND RECORDS A

a. 29 CFR 1910.147 Control of Hazardous

3. INSTITUTE OF ELECTRICAL AND ELECTRON

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a. IEEE Std 100 Dictionary of Electrical anb. IEEE C2 National Electrical Safety

4. NATIONAL ELECTRICAL MANUFACTURERS

a. NEMA C57.12.28 Pad-Mounted Equipmb. NEMA ICS 6 Industrial Control andc. NEMA MG 1 Motors and Generatod. NEMA MG 10 Energy Management

Fixed Frequency Medium AC Squirrel-Cae. NEMA MG 11 Energy Management

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

a. TIA/EIA-606-A Administration Standard Infrastructure (ANSI/TIA/EIA-606-A)

1.2 RELATED REQUIREMENTS

 A. This section applies to certain sections of[ Division 2"Equipment,"][ Division 13, "Special Construction,"Systems"][ and][ Division 15, "Mechanical"]. This

Division 16, "Electrical," of this project specification individual sections.

1.3 DEFINITIONS

 A. Unless otherwise specified or indicated, electrical anspecifications, and on the drawings, shall be as define

B. The technical sections referred to herein are those sproducts, installation procedures, and equipment osection for detailed description of submittal types.

C. The technical paragraphs referred to herein are PRODUCTS and PART 3 - EXECUTION of the products, systems, installation procedures, equipmen

1.4 ELECTRICAL CHARACTERISTICS

 A. Electrical characteristics for this project shall be 208Y120 volt-3phase-4wire 60 HZ.

1.5 SUBMITTALS

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 A. The following shall be submitted in accordance wPROCEDURES:

B. Submittals required in the sections which refer to thisfollowing additional requirements. Submittals shall trade name, place of manufacture, catalog model olayout dimensions, capacity, project specification anSubmittals shall also include applicable federal, militapublication references, and years of satisfactorynecessary to establish contract compliance of each of existing installations are unacceptable and will be r

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

D. Drawings: Submit drawings a minimum of 14 by 20scale of 1/8 inch per foot, except as specified otherwinstallation details of equipment indicating proposed control panels, accessories, piping, ductwork, and oensure a coordinated installation. Wiring diagrams indicate the internal wiring for each item of equipmeneach item of equipment. Drawings shall indicate amaintenance, and replacement of operating equipme

E. Instructions: Where installation procedures or part required to be in accordance with manufacturer's insthose instructions prior to installation. Installation omanufacturer's instructions are received. Failure to shall be cause for rejection of the equipment or mater

F. Certificates: Submit manufacturer's certifications asfinishes, and equipment as specified in the tech

material suppliers are not acceptable. Preprintpreviously submitted documents will not be accertifications shall name the appropriate products, publication specified as controlling the quality of contain statements to imply that the item does not mas "as good as"; "achieve the same end use and accordance with the referenced publications"; or "eperformance of the specified material." Certificationconforms to the requirements specified. Certif

manufacturer's letterhead and shall be signed by theto sign certificates of compliance.

1. Reference Standard Compliance: Where equipconform to industry and technical societorganizations such as American National Stan

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organizations such as American National StanSociety for Testing and Materials (ASTM),  Association (NEMA), Underwriters Laboratorie

Illuminating Companies (AEIC), submit proof olisting by the specified organization will be acce2. Independent Testing Organization Certificate

submit a certificate from an independent teperform testing, and approved by the Contracstate that the item has been tested in organization's test methods and that the itorganization's reference standard.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Material and Equipment Qualifications: Provide mproducts of manufacturers regularly engaged in the are of equal material, design and workmanship.satisfactory commercial or industrial use for 2 yearsperiod shall include applications of equipmentcircumstances and of similar size. The product commercial market through advertisements, manuduring the 2-year period. Where two or more items orequired, these items shall be products of a sin

component parts of the item need not be the productsstated in the technical section.

B. Regulatory Requirements: Equipment, materials, inbe in accordance with the mandatory and advisory pr

C. Alternative Qualifications: Products having less thanbe acceptable if a certified record of satisfactory field

hours, exclusive of the manufacturers' factory or labo

D. Service Support: The equipment items shall be suwhich are reasonably convenient to the equipmensatisfactory service to the equipment on a regular warranty period of the contract.

E. Manufacturer's Nameplate: Each item of equipmenthe manufacturer's name, address, model number, a

in a conspicuous place; the nameplate of the distribut

F. Modification of References: In each of the publicatioadvisory provisions to be mandatory, as though the wfor "should" wherever it appears. Interpret referen"authority having jurisdiction " or words of similar m

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authority having jurisdiction, or words of similar mOfficer.

G. Material and Equipment Manufacturing Date: Prodyears prior to date of delivery to site shall not be used

1.7 POSTED OPERATING INSTRUCTIONS

 A. Provide for each system and principal item of equipsections for use by operation and maintenance persshall include the following:

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

B. Print or engrave operating instructions and frame undplastic. Post instructions where directed. For opeweather, provide weather-resistant materials or weainstructions shall not fade when exposed to sunligheasy removal or peeling.

1.8 NAMEPLATES

 A. STM D 709. Provide laminated plastic nameplates

enclosure, relay, switch, and device; as specifiedindicated on the drawings. Each nameplate inscriptwhen applicable, the position. Nameplates shall be white with black center core. Provide red laminated where indicated. Surface shall be matte finish. Coalign lettering and engrave into the core. Minimum s2.5 inches. Lettering shall be a minimum of 0.25 inch

1.9 WARNING SIGNS

 A. Provide warning signs for the enclosures of electricapad-mounted transformers, pad-mounted switches, ga nominal rating exceeding 600 volts.

1. When the enclosure integrity of such equipmenwith NEMA C57.12.28, such as for pad-mounteSF6 switches], provide self-adhesive warning

voltage compartment door(s). Sign shall be dimensions of 7 by 10 inches with the legeprinted in two lines of nominal 2 inch high lettein white letters on a red background and the woblack letters on a white background. Decal shor approved equal.

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o app o ed equa2. When such equipment is guarded by a fence, m

metal signs having nominal dimensions of 1"DANGER HIGH VOLTAGE KEEP OUT" printehigh white letters on a red and black field.

1.10 ELECTRICAL REQUIREMENTS

 A. Electrical installations shall conform to IEEE C2, NFPherein.

B. Wiring and Conduit: Provide internal wiring for comp

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16070 - SEISMIC PROTECTION FOR ELECTRICA

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this specthe latest version of the reference publication shall ato in the text by basic designation only.

1. AMERICAN SOCIETY FOR TESTING AND MA

a. ASTM E 580 Application of Ceiling SuTile and Lay-in Panels in Areas Requiring

2. U.S. ARMY CORPS OF ENGINEERS (USACE

a. TI 809-04 Seismic Design for Buildings

3. UNDERWRITERS LABORATORIES (UL)

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1.2 SUBMITTALS

 A. The following shall be submitted in accordance wPROCEDURES:

1. SD-02 Shop Drawings

a. Equipment Requirements;

2. SD-03 Product Data

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

grade, class of metal, and dimensions; and sreinforcement, anchorage, and installation with relatio

C. Copies of the design calculations with the detail stamped by a registered engineer and shall verify thto which bracing is attached for carrying the load from

1. Contractor Designed Bracing;

D. Copies of the Design Calculations with the Drawingscertified, stamped and signed by a Registered Proshall verify the capability of structural members tcarrying the load from the brace.

1.3 SYSTEM DESCRIPTION

 A. General Requirements: The requirements for seismin this section shall be applied to the electrical equStructural requirements shall be in accordance PROTECTION FOR MISCELLANEOUS EQUIPMEN

B. The entire electrical installation shall be Seismically pthe drawings or in other sections of these specificatio

1. Control Panels2. Air Handling Units

3. Pumps with Motors4. Switchgear5. Light Fixtures6. Unit Substations7. Motor Control Centers8. Transformers9 S it hb d (Fl M t d)

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9. Switchboards (Floor Mounted)10. Storage Racks11. Engine Generators

12. UPS equipment13. Batteries14. Battery Racks15. Raceways16. Automatic transfer switches17. Static transfer switches

C. Electrical Systems: The following electrical systems

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friction resulting from gravity loads. TI 809-04 uses pthe equipment in the building; therefore, corresponshall be required. Loadings determined using TI 809therefore, the AISC LRFP specifications shall be usethe following electrical equipment and systems shall b

a. The entire electrical installation shall be s

1.4 EQUIPMENT REQUIREMENTS

 A. Rigidly Mounted Equipment: The following specequipment, Engine-Generator, Substations, Transfofurnished under this contract shall be constructed seismic forces specified in TI 809-04, Chapter 1equipment shall be entirely located and rigidly attachexpansion joint. Piping, electrical conduit, etc., whichprovided with flexible joints that are capable of accomthe full width of the joint in both orthogonal directions.

B. Nonrigid or Flexibly-Mounted Equipment: The followbe furnished: [_____] shall be constructed and asseforce of [_____] times the operating weight of the egravity of the equipment.

PART 2 - PRODUCTS

2.1 SWAY BRACING MATERIALS

 A. Sway bracing materials (e.g. rods, plates, rope, angSection 13080 SEISMIC PROTECTION FOR MISCE

PART 3 - EXECUTION

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3.1 SWAY BRACES FOR CONDUIT

 A. Conduit shall be braced as for an equivalent weigh13080 SEISMIC PROTECTION FOR MISCELLANEO

1. Assembly Mounted on Outlet Box

a. A supporting assembly, that is intended shall be designed to accommodate moplaster rings, and fixture studs.

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SECTION 16075 - ELECTRICAL IDENTIFICATION

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 RELATED DOCUMENTS

 A. Drawings and general provisions of the CoSupplementary Conditions and Division 1 Specificatio

1.2 SUMMARY

 A. This Section includes the following:

1. Identification for raceway.2. Identification for conductors and communication3. Underground-line warning tape.4. Warning labels and signs.5. Instruction signs.6. Equipment identification labels.7. Miscellaneous identification products.

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B. Identification labeling for switchboards, panel boprovided by Government.

1.3 SUBMITTALS

 A. Product Data: For each electrical identification produ

B. Identification Schedule: An index of nomenclature ocomponents used in identification signs and labels.

C Samples: For each type of label and sign to illus

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Comply with 29 CFR 1910.145.

1.5 COORDINATION

 A. Coordinate identification names, abbreviations, crequirements in the Contract Documents, Shop diagrams, and the Operation and Maintenance Macodes, standards, and 29 CFR 1910.145. Use co

Project.

B. Coordinate installation of identifying devices with coof surfaces where devices are to be applied.

C. Coordinate installation of identifying devices with loca

D. Install identifying devices before installing acoustical

PART 2 - PRODUCTS

2.1 RACEWAY IDENTIFICATION MATERIALS

 A. Comply with ANSI A13.1 for minimum size of letters fof color field for each raceway.

B. Color for Printed Legend:

1. Power Circuits: Black letters on an orange field2. EPMS Raceways: White letters on blue field.3. Legend: Indicate system or service and voltage

C. Self-Adhesive Vinyl Labels: Preprinted, flexible labeand chemical-resistant coating and matching wrapa

d f l d l b l

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ends of legend label.

2.2 CONDUCTOR AND COMMUNICATION- AND CONMATERIALS

 A. Color-Coding Conductor Tape: Colored, self-adhesthick by 1 to 2 inches wide.

2.3 UNDERGROUND-LINE WARNING TAPE

 A. Description: Permanent, bright-colored, continuous-p

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2.4 WARNING LABELS AND SIGNS

 A. Comply with NFPA 70 and 29 CFR 1910.145.

B. Self-Adhesive Warning Labels: Factory printeadhesive labels, configured for display on front equipment, unless otherwise indicated.

C. Metal-Backed, Butyrate Warning Signs: Weather-cellulose-acetate butyrate signs with 0.0396-inch gcolors, legend, and size required for application. mounting. Nominal size, 10 by 14 inches.

D. Warning label and sign shall include, but are not limit

1. Multiple Power Source Warning: "DANGER - EQUIPMENT HAS MULTIPLE POWER SOURC

2. Workspace Clearance Warning: "WARNING -FRONT OF ELECTRICAL EQUIPMENT MUINCHES."

2.5 INSTRUCTION SIGNS

 A. Engraved, laminated acrylic or melamine plastic, minto 20 sq. in. and 1/8 inch thick for larger sizes.

1. Engraved legend with black letters on white fac2. Punched or drilled for mechanical fasteners.3. Framed with mitered acrylic molding and arra

equipment.

2.6 EQUIPMENT IDENTIFICATION LABELS

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 A. Adhesive Film Label: Machine printed, in black,

process. Minimum letter height shall be 3/8 inch.

B. Adhesive Film Label with Clear Protective Overlaythermal transfer or equivalent process. MinimumOverlay shall provide a weatherproof and ultraviolet-r

2.7 MISCELLANEOUS IDENTIFICATION PRODUCTS

A. Cable Ties: Fungus-inert, self-extinguishing, 1-pi

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a. Power transfer switches.b. Controls with external control power conn

2. Equipment Requiring Workspace Clearance otherwise indicated, apply to door or coverpanelboards and similar equipment in finished s

I. Instruction Signs:

1. Operating Instructions: Install instruction signsmaintenance of electrical systems and itemsinstruction signs with approved legend where ior equipment operation.

2. Emergency Operating Instructions: Install insta red background with minimum 3/8-inch- highat equipment used for power transfer.

J. Equipment Identification Labels: On each unit of equlabel that is consistent with wiring diagrams, Maintenance Manual. Apply labels to disconnect swcentral or master units, control panels, control stationeach system. Systems include power, control, commalarm systems unless equipment is provided with its o

1. Labeling Instructions:

a. Indoor Equipment: Adhesive film label protective overlay. Unless otherwise indwith 1/2-inch- high letters on 1-1/2-inch- hrequired, use labels 2 inches high.

b. Outdoor Equipment: Engraved label.c. Elevated Components: Increase sizes

appropriate for ie ing from the floor

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appropriate for viewing from the floor.

2. Equipment to Be Labeled:

a. Panelboards, electrical cabinets, and enspecification.

b. Electrical switchboards.c. Transformers.d. Disconnect switches.e. Enclosed circuit breakers.f Power transfer equipment

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

3.2 INSTALLATION

 A. Verify identity of each item before installing identificat

B. Location: Install identification materials and devicesviewing without interference with operation and maint

C. Apply identification devices to surfaces that require fi

D. Self-Adhesive Identification Products: Clean sumaterials and methods recommended by manufactur

E. Attach non-adhesive signs and plastic labels withappropriate to the location and substrate.

F. System Identification Color Banding for Raceways acompletely encircle cable or conduit. Place adjace

contact, side by side. Locate bands at changes in and floors, at 50-foot maximum intervals in straighintervals in congested areas.

G. Color-Coding for Phase and Voltage Level Identificcolors listed below for ungrounded feeder and branch

1. Color shall be factory applied or, for sizes larghaving jurisdiction permit, field applied.

2. Colors for 208/120-V Circuits:

a. Phase A: Black.b. Phase B: Red.c. Phase C: Blue.

3 Colors for 480/277-V Circuits:

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3. Colors for 480/277 V Circuits:

a. Phase A: Brown.b. Phase B: Orange.c. Phase C: Yellow.

4. Field-Applied, Color-Coding Conductor Tape: minimum distance of 6 inches from terminal potaps are made. Apply last two turns of tape wunwinding. Locate bands to avoid obscuring fa

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16081 - APPARATUS INSPECTION AND TESTIN

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this specthe latest version of the reference publication shall ato in the text by the basic designation only.

1. INTERNATIONAL ELECTRICAL TESTING ASS

a. NETA ATS Electrical Power Distribut

1.2 RELATED REQUIREMENTS

 A. Section 16050 "Basic Electrical Materials and Methadditions and modifications specified herein.

1.3 SUBMITTALS

A The following shall be submitted:

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 A. The following shall be submitted:

1. SD-06 Test Reports

a. Acceptance tests and inspections;

2. SD-07 Certificates

a. Qualifications of organization, and lead eb. Acceptance test and inspections procedu

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

work required by this section of the specification shsubcontractor.

1. Submit name and qualifications of organizatioregularly engaged in the testing of electrical msystems for a minimum of 5 years. The orgprogram, and test instruments used shall be ca ATS.

2. Submit name and qualifications of the lead eng

required testing services. Include a list of thrthe technician with specific names and teTesting, inspection, calibration, and adjustmengineering technician, certified by NETA or thein Engineering Technologies (NICET) with a inspecting, testing, and calibrating electricequipment, systems, and devices.

B. Acceptance Tests and Inspections Reports: Subreports and test reports. Reports shall include certificrequirements, identify deficiencies, and recomappropriate. Type and neatly bind test reports toSubmit test reports documenting the results of eachtest is completed.

C. Acceptance Test and Inspections Procedure: Submitem of equipment to be field tested at least 45 days

not perform testing until after test procedure has been

PART 2 - PRODUCTS

NOT USED

PART 3 - EXECUTION

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3.1 ACCEPTANCE TESTS AND INSPECTIONS

 A. Testing organization shall perform acceptance testsprocedures, and test values shall be performed aNETA ATS, the manufacturer's recommendationsQuality Control" of each applicable specification sectNETA ATS are not required unless otherwise specifservice only after completion of required tests and ebeen completed. Contractor shall supply to the test

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

performed by the testing organization. Thesestart-up engineer.

2. Section 16610, "Installation of Uninterruptible P3. Section 16410, "Automatic Transfer Switches"4. Section 16442, "Switchboards"5. Section 16435, “Installation of Paralleling Switc6. Section 16461, “Installation of Dry Type Transfo

3.2 SYSTEM ACCEPTANCE

 A. Final acceptance of the system is contingent acceptance tests and inspections.

3.3 PLACING EQUIPMENT IN SERVICE

 A. A representative of the approved testing organizationtested by the organization is initially energized and pl

END OF SECTION 16081

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SECTION 16231 – INSTALLATION OF PACKAGED ENGINE

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, mental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 SUMMARY

 A. This Section describes the requirements for testingGenerator equipment as specified herein. Refer to PGovernment Furnished Equipment (GFE).

B. The Installing Contractor shall be required to provide

1. Unloading, rigging and installation.2. Concrete pads and superstructure reinforceme3. Interconnecting wiring external to the enclosure4. Conduit external to the equipment specified her5. Load banks and cabling for site tests.

C. Related Sections include the following:

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1. Division 16 Section "Transfer Switches" for tran

and relays to initiate automatic-starting and -stogenerator sets.2. Refer to electrical power monitoring system (EP

alarms information reporting and interface requ3. Division 15 Section “Fuel Oil System” for day ta

pumping and controls.

1.2 SUBMITTALS

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1.3 QUALITY ASSURANCE

 A. Testing Agency Qualifications: An independent acapability to conduct the testing indicated, that International Electrical Testing Association or is laboratory (NRTL), and that is acceptable to authoritie

1. Testing Agency's Field Supervisor: Person curElectrical Testing Association or the National In

Engineering Technologies to supervise on-site

B. Electrical Components, Devices, and Accessories: NFPA 70, Article 100, by a testing agency acceptabland marked for intended use.

C. Comply with ASME B15.1.

D. Comply with NFPA 37.

E. Comply with NFPA 70.

F. Comply with NFPA 99.

G. Comply with NFPA 110 requirements for Level 2 em

1.4 PROJECT CONDITIONS

 A. Interruption of Existing Electrical Service: Do not inteoccupied by The Government or others unless permiand then only after arranging to provide temporarrequirements indicated:

1. Notify Owner no fewer than five days in advancelectrical service. Time and date of interruption

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electrical service. Time and date of interruption 2. Do not proceed with interruption of electrical se

permission.

1.5 COORDINATION

 A. Coordinate size and location of concrete bases for panchor-bolt inserts into bases. Concrete, reinforceare specified in Division 3.

1 6 DELIVERY STORAGE AND HANDLING

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

Officer to determine damage or missing parts. Codamage sustained by the materials and equipment aheavy and easily damaged. Do not bump or bounclifting, do not tip beyond 5 degrees.

PART 2 - PRODUCTS

2.1 CONTRACTOR FURNISHED MATERIAL AND EQU

 A. Packaged Engine Generator shall be GFE. Product information purposes only. Such equipment requoperable Packaged Engine Generator installation limited to, conduit, conduit fittings, insulated conductfasteners, and other such items.

2.2 ENGINE-GENERATOR SET - GFE

 A. Factory-assembled and -tested, engine-generator set

1. KW rating indicated shall be at 0.80-power factodeducting cooling fan horsepower and engine e

B. Capacities and Characteristics:

1. Power Output Ratings: Nominal ratings as indioperate as a unit as evidenced by records of pr

2. Output Connections: Three-phase, four wire.

2.3 ENGINE - GFE

 A. Fuel: Fuel oil, Grade DF-2 .

B. Engine Fuel System

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1. The fuel system shall be integral with the engi

with non-fouling fuel injectors, dual fuel filter, finjection pumps, lines, nozzles and fuel pressudeliver fuel under low pressure to individual cylinder.

C. Fuel/Water Separator

D. Exhaust Noise Control

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2.4 EXHAUST SYSTEM

 A. The engine exhaust system shall be installed combustion gases quickly and silently with minimusilencer shall be designed for minimum restriction, aexceed the maximum specified by the manufacturer f

1. Piping shall be supported and braced to prevetransferred to the engine and flexible

accommodate thermal growth. Support dampwhere necessary to isolate vibration.

2.5 FUEL OIL STORAGE

 A. Refer to specifications Section 15491H.

2.6 CONTROL AND MONITORING - GFE

 A. Remote Emergency-Stop Switch: Contractor shamounted, unless otherwise indicated; and labeled. Paccidental operation.

2.7 GENERATOR OVERCURRENT AND FAULT PROTE

2.8 LOAD BANK – GFE

2.9 REMOTE EMERGENCY-STOP SWITCH

 A. Contractor shall furnish and install Flush; wall mountelabeled. Push button shall be protected from accident

2.10 REFERENCES

 A. This specification includes applicable considerations

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1. American Society of Mechanical Engineers (AS2. Association of British Generating Set Manufactu3. British Standards Institution (BS)4. EEC 89/392 Safety and Health5. Electrical Generating Systems Association (EG6. Institute of Electrical and Electronics Engineers7. International Electrotechnical Commission (IEC8. International Standards Organization (ISO) 900

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2.11

PART 3 - EXECUTION

3.1 EXAMINATION

 A. Examine areas, equipment bases, and conditiocompliance with requirements for installation and otengine-generator performance.

B. Examine roughing-in of piping systems and electlocations of connections before packaged engine-gen

C. Proceed with installation only after unsatisfactory con

3.2 INSTALLATION

 A. Conform to the requirements for electrical equipment

in strict accordance with NFPA 70, and manufacturerDuring and after installation, until the system is accContractor shall protect equipment, from moisture,completion of the Engine Generator installation, Generator manufacturer's technical representative contract compliance. Contractor shall correct installa

B. Contractor shall notify Contracting Officer in writing

completion of the Engine Generator system installaOfficer, will schedule the manufacturer's technicacompleted installation. The technical representativeincluding days of instruction for activity personnel.

C. Installation Inspection: Engine Generator technical rOfficer, in the presence of the Contractor, will inspeContractor shall correct construction or installation de

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D. Comply with packaged engine-generator manufaalignment instructions and with NFPA 110.

E. Install packaged engine generator to provide accessaccessories, for periodic maintenance.

F. Install packaged engine generator with [elastomspring isolators] having a minimum deflection of [1

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2. Under supervision of the factory authorized serContractor shall test all system functions, operaContractor shall provide all instruments and equ

B. Tests and Inspections:

1. Perform tests recommended by manufacturer aand mechanical inspection for "AC Generators specified in NETA Acceptance Testing Specific

parameters.2. NFPA 110 Acceptance Tests: Perform tests re

additional to those specified here including, butpickup test.

3. Battery Tests: Equalize charging of battery celwritten instructions. Record individual cell volta

a. Measure charging voltage and voltages bterminals for full-charging and float-charg

level and specific gravity under both condb. Test for contact integrity of all connectors

and a capacity load test for the battery.c. Verify acceptance of charge for each elem

discharge.d. Verify that measurements are within man

4. Battery-Charger Tests: Verify specified rates o

float-charging conditions.5. System Integrity Tests: Methodically verify prointegrity of each element of engine-generator syoperation. Check for air, exhaust, and fluid lea

6. Exhaust-System Back-Pressure Test: Use a m40-inch wg. Connect to exhaust line close to ethat back pressure at full-rated load is within malimits for the engine.

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7. Exhaust Emissions Test: Comply with applicab

8. Voltage and Frequency Transient Stability Testmeasure voltage and frequency transients for 5increases and decreases, and verify that perfor

9. Harmonic-Content Tests: Measure harmonic cthan 25 percent and at 100 percent of rated linecontent is within specified limits.

10. Noise Level Tests: Measure A-weighted level ogenerator-set installation, including engine exha

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

D. Test instruments shall have been calibrated within standards of NIST, and adequate for making positivecalibration records available for examination on reque

E. Leak Test: After installation, charge system and test until no leaks exist.

F. Operational Test: After electrical circuitry has beenproper motor rotation and unit operation.

G. Test and adjust controls and safeties. Replace damand equipment.

H. Remove and replace malfunctioning units and retest

I. Retest: Correct deficiencies identified by tests aspecified requirements are met.

J. Report results of tests and inspections in writing. Remeasured insulation resistances, time delays, and Attach a label or tag to each tested component indtests.

K. Infrared Scanning: After Substantial Completion, but Acceptance, perform an infrared scan of each poweconnection. Remove all access panels so terminatio

to portable scanner.

1. Follow-up Infrared Scanning: Perform an additmonths after date of Substantial Completion.

2. Instrument: Use an infrared scanning device deor to detect significant deviations from normal vfor device.

3. Record of Infrared Scanning: Prepare a certifieterminations and connections checked and that

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terminations and connections checked and that

Include notation of deficiencies detected, remedobservations after remedial action.

3.6 DEMONSTRATION

 A. Engage a factory-authorized service representativpersonnel to adjust, operate, and maintain packagDivision 1 Section "Demonstration and Training."

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16402 — INTERIOR DISTRIBUTION SYSTEM

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NECESFOLLOWING:

Modify specifications to suit project conditions, scope, all aptions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this speThe publications are referred to in the text by the bas

1. AMERICAN NATIONAL STANDARDS INSTITU

a. ANSI C80.5 (1994) Aluminum Rigid Cond

2. ASTM INTERNATIONAL (ASTM)

a. ASTM B 1 (2001) Hard-Drawn Copper Wb. ASTM B 8 (1999) Concentric-Lay-Stra

Medium-Hard, or Soft

3. INSTITUTE OF ELECTRICAL AND ELECTRON

4. INTERNATIONAL ELECTRICAL TESTING ASS

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a. NETA ATS (1999) Electrical Power Distr

5. NATIONAL ELECTRICAL MANUFACTURERS

a. NEMA BU 1 (1999) Buswaysb. NEMA FU 1 (2002) Low Voltage Cartridgc. NEMA ICS 1 (2000) Industrial Co

Requirements

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

i. NEMA MG 1 (1998; R 2002) Motors a j. NEMA MG 10 (2001) Energy Managem

of Fixed Medium AC Squirrel Cage Polypk. NEMA MG 11 (1977; R 2001) Energy

and Use of Single Phase Motorsl. NEMA RN 1 (1998) Polyvinyl-Chloride (PV

Rigid Steel Conduit and Intermediate Metm. NEMA ST 20 (1992; R 1997) Dry-T

 Applicationsn. NEMA TP 1 (2002) Guide for Determining

Transformers

6. NATIONAL FIRE PROTECTION ASSOCIATIO

a. NFPA 70 (2002) National Electrical Cob. NFPA 780 (2000) Installation of Lightnin

7. UNDERWRITERS LABORATORIES (UL)

a. UL 1561 (1999; R 2001) Dry-Type Transformers

b. UL 198E (1988; R 1988) Class R Fusesc. UL 198H (1988; R 1993) Class T Fused. UL 467 (1993; R 2001) Grounding and Be. UL 486A (1997; R 2001, Bul. 2002, 2003

Lugs for Use with Copper Conductorsf. UL 486B (1997; R 2001, Bul. 2002, 200

 Aluminum Conductorsg. UL 486C (2000; R 2002) Splicing Wireh. UL 489 (2002; R 2002, Bul. 2003) Molde

Case Switches, and Circuit-Breaker Encloi. UL 50 (1995; R 1999, Bul. 2001) Enclo j. UL 506 (2000; Bul. 2002, 2003) Specialtk UL 508 (1999; R 2002 Bul 2003) Indus

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k. UL 508 (1999; R 2002, Bul. 2003) Indus

l. UL 510 (1994; R 1998) Polyvinyl ChloInsulating Tape

m. UL 67 (1993; R 2002) Panelboardsn. UL 83 (1998; R 2001, Bul. 2002) Th

Cableso. UL 845 (1995; R 2002, Bul. 2003) Motorp. UL 869A (1998; Bul. 2002) Reference Sta

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

used, a designation following the "G" designation idthe submittal for the Government. The following shaSection 01330 SUBMITTAL PROCEDURES:1. SD-02 Shop Drawings

a. Panelboards; Gb. Transformers; Gc. Motor control centers; Gd. Wireways; G

2. SD-03 Product Data

a. Receptacles; Gb. Circuit breakers; Gc. Switches; Gd. Transformers; Ge. Enclosed circuit breakers; G

f. Motor controllers; G

3. SD-06 Test Reports

a. 600-volt wiring test; Gb. Grounding system test; Gc. Transformer tests; Gd. Ground-fault receptacle test; G

4. SD-07 Certificatesa. Fuses; G

5. SD-09 Manufacturer's Field Reportsa. Transformer factory tests

6. SD-10 Operation and Maintenance Data

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B. Submit operation and maintenance data in aOPERATION AND MAINTENANCE DATA and as sp

1.4 QUALITY ASSURANCE

 A. Submit coordination data as specified in article entitle

1.5 MAINTENANCE

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

PART 2 - PRODUCTS

2.1 MATERIALS AND EQUIPMENT

 A. Materials, equipment, and devices shall, as a minwhere UL standards are established for those items,

B. PANELBOARDS: UL 67 and UL 50 having a short-cfor use as service disconnecting means shall ad

Panelboards shall be circuit breaker-equipped. Debreakers can be removed without disturbing adjacremoving supplemental insulation supplied as merequired by UL. "Specific breaker placement" is reqbreaker placement indicated in the panelboard sch"Subfeed Breakers" is not acceptable unless specibreaker shall be "separately" mounted ["above"] [or] "space only" is indicated, make provisions for

Panelboard locks shall be keyed same. Directories circuit in panelboard. Directories shall also indicate(e.g., Panel PA served from Panel MDP). Type directransparent protective covering. [Panelboards shaintended use.]

C. Panelboard Buses: Support bus bars on bases indebuses and back pans shall be designed so that bmachining, drilling, or tapping. Provide isolated

connection of circuit neutral conductors. Provide sequipment grounding bus per UL 67 for connectinsteel cabinet.

1. Panelboard Neutrals for Non-Linear Loads: ULhave been specifically UL heat rise testedPanelboard shall be heat rise tested in accordneutral assembly installed and carrying 200

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during testing. Verification of the testing prrequest. Two neutral assemblies paralleacceptable. Nameplates for panelboard ratedbe marked "SUITABLE FOR NON-LINEAR LOAinstructions for wiring the neutral of panelboloads.

D. Circuit Breakers: UL 489, [thermal magnetic-type]t ti l t th h t i it t ti

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2. Circuit Breaker With [GFCI] [GFI]: UL 943 andtest" button, visible indication of tripped conditiocurrent imbalance of [6 milliamperes or greateClass A [GFCI] [GFI] devices, for personnel progreater per requirements of UL 943 for Clasprotection.]

3. Circuit Breakers for HVAC Equipment: Circuhaving motors (group or individual) shall be maUL listed as HACR type.

4. Arc-Fault Circuit-Interrupters: UL 489, UL 16circuit breaker shall be rated as indicated. [Twshall be rated 120/240 volts. The provision of shared neutral circuits in lieu of (one) two polProvide with "push-to-test" button.

5. Fusible Switches for Panelboards: NEMA KSserving as motor disconnect means shall be ho

6. 400 Hz Panelboard and Breakers: Panelboard

systems shall be "400 Hz" rated and labeled.

2.2 TRANSFORMERS

 A. NEMA ST 20, general purpose, dry-type, self-cooledin NEMA 1 enclosure. Transformer shall have 220transformers 15 kVA and greater, and shall havtransformers rated 10 kVA and less, with temperaturC under full-rated load in maximum ambient of 40

degrees C temperature rise shall be capable of carnameplate kVA without exceeding insulation rating. with maximum sound level at least 3 decibels lestransformer ratings indicated.

B. Specified Transformer Efficiency: Transformers, indprimary, 80 degrees C or 115 degrees C temperaturfor single phase or 30 to 500 for three phase, shall b

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efficiency, based on factory test results, shall not be as defined by NEMA TP 1.

C. Transformers With Non-Linear Loads: Transformer i220 degrees C system. Neither the primary nor exceed 220 degrees C at any point in the coils whisinusoidal load. Transformers are to be UL listedindicated, defined as the sum of fundamental and h

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. UL 845, NEMA ICS 2, NEMA ICS 3. Wiring shall beenclosure. Provide control centers suitable for opera60 Hz system and shall have minimum short-circuit w65,000 amperes rms symmetrical. Incoming powerthe top or bottom of enclosure and terminating ondevice shall be molded case circuit breaker rateinterrupting capacity. Arrange busing so that control cends. Interconnecting wires shall be copper. Terminthat controllers may be removed without disconnectin

B. Provide the following bus systems. Power bus scurrent of 65,000 amperes rms symmetrical. Wirinhorizontal and vertical bus bars.

1. Horizontal bus shall have continuous current Main bus shall be copper, silver-plated enclosof each vertical section. Main bus shall be is

and other areas.2. Vertical bus shall have continuous current rat

copper, tin-plated. Vertical bus shall be encloglass "sandwich."

3. Copper ground bus shall be provided full widthbe equipped with necessary lugs.

C. Motor Disconnecting Devices and Controllers: Sha"Combination Motor Controllers."

D. Combination Motor Controllers: UL 508 and other re"Motor Controllers." Controller shall employ moldebreakers for combination controllers shall be thermal

2.4 SOURCE QUALITY CONTROL

 A. Transformer Factory Tests: Submittal shall include

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test results on each transformer and also contain t"prototype" tests that were made on transformers elethose specified.

PART 3 - EXECUTION

3.1 FIELD QUALITY CONTROL

A Furnish test equipment and personnel and submit w

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

D. Transformer Tests Perform the standard, not optioInspection and Test Procedures for transformers, dbelow; as specified in NETA ATS. Measure primary tap settings. Tests need not be performed by a recoindependent electrical consulting firm.

END OF SECTION

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16410 — INSTALLATION OF AUTOMATIC TRAN

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NECESFOLLOWING:

Modify specifications to suit project conditions, scope, all aptions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 SUMMARY

 A. This Section describes the requirements for testing Switches. Refer to Part 2 – Products for listing of G(GFE)

1.2 REFERENCES

 A. The publications listed below form a part of this specthe latest version of the reference publication shall a

to in the text by the basic designation only.

1. INTERNATIONAL ELECTRICAL TESTING ASS

a. NETA ATS Electrical Power Distribution

2. NATIONAL FIRE PROTECTION ASSOCIATIO

a. NFPA 70 National Electrical Code

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1.3 RELATED REQUIREMENTS

 A. Section 16050, "Basic Electrical Materials and M"Apparatus Inspection and Testing," apply to thismodifications specified herein.

1.4 SUBMITTALS

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Government-Furnished Equipment (GFE): The G

components and equipment listed in PART 2- PRContractor.

B. Delivery: Contractor shall receive, the GFE at the unpack, and install GFE. Notify Contracting Officewhen delivery on the site is required. GFE shall Contracting Officer to determine damage or missresponsible for damage sustained by the materials aEquipment is heavy and easily damaged. Do not btime. When lifting, do not tip beyond 5 degrees.

PART 2 - PRODUCTS

2.1 CONTRACTOR FURNISHED MATERIAL AND EQU

 A. Automatic Transfer Switches shall be GFE. Product information purposes only. Such equipment requ

operable Automatic Transfer Switches installation limited to, conduit, conduit fittings, insulated conductosupports, fasteners, and other such items.

2.2 AUTOMATIC TRANSFER SWITCHES - GFE

 A. Provide three-pole, automatic transfer switches foaccordance with UL 1008. Each automatic transfsystem transfer and have the current and voltage rati

B. Automatic Transfer Switch Controls: Controls for UtSwitch: Provide all necessary controls to start thenormal (utility) source, transfer the load to the gevoltage and frequency, re-transfer the load when tand stop the generator set.

PART 3 - EXECUTION

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3.1 INSTALLATION

 A. Conform to the requirements for electrical equipmenspecified herein, and in strict accordance with NFPA drawings and wiring. During and after installation, uContracting Officer, Contractor shall protect equipcontamination. Upon completion of the AutomaC t ti Offi d A t ti T f S

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

inspect the completed installation. The _____tec

 _____ days of service including _____days of instruc

C. Installation Inspection: The Automatic Transfer Switthe Contracting Officer, in the presence of the Continstallation. The Contractor shall correct constructdirected.

3.2 PREREQUISITES FOR FUNCTIONAL ACCEPTANC

 A. Completion of the following requirements is mandaacceptance tests for the automatic transfer switch.

1. Performance of Acceptance Checks and tparagraph entitled "Acceptance Checks and and Tests shall be accomplished by the TesSection 16081, "Apparatus Inspection and Test

B. All test equipment and instruments shall be on handsubject to Contracting Officer's approval, evidencearrangements have been made to have the necessasite prior to field testing.

3.3 FIELD QUALITY CONTROL

 A. Give Contracting Officer 15 days notice of dates anrequire the presence of the Contracting Officer. The

with the using activity and schedule a time that will eand interference with the activity operations. The ccosts associated with conducting tests outside of incorporating special arrangements and proceduconditions. The contractor shall provide labor, equload, and consumables required for the specified tedevices and indicating devices shall be certified. Tproduct in accordance with Section 16050, "Basic E

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Perform the following field tests in accordarecommendations and include the following visual electrical tests, performed in accordance with NETA A

B. Automatic Transfer Switch Acceptance Checks and T

1. Visual and Mechanical Inspection

C i t l t d t

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

g. Perform manual transfer operation.

h. Verify positive mechanical interlockingsources.

2. Electrical Tests

a. Measure contact-resistance.b. Perform insulation-resistance on each po

ground with switch closed, and across Perform tests in both source positions.

c. Verify settings and operations of control dd. Calibrate and set all relays and timers.

C. Functional Acceptance Tests: Functional AcceptancSection “Packaged Engine Generator Tests” and shaand demonstrating the following operations for Contractor shall show by demonstration in service thare in good operating condition, and function not less

D. Perform automatic transfer tests:

a. Simulate loss of normal/preferred power.b. Return to normal/preferred power.c. Simulate loss of emergency power.d. Simulate all forms of single-phase conditi

2. Verify correct operation and timing of the follow

a. Normal source voltage-sensing relays.b. Engine start sequence.c. Time delay upon transfer.d. Alternate source voltage-sensing relays.e. Automatic transfer operation.f. Interlocks and limit switch function.g. Time delay and retransfer upon normal po

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END OF SECTION

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16412 — INSTALLATION OF STATIC TRANSFER

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NECESFOLLOWING:

Modify specifications to suit project conditions, scope, all aptions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

The publications listed below form a part of this specification

est version of the reference publication shall apply. The pubby basic designation only.

1. NATIONAL FIRE PROTECTION ASSOCIATIO

a. NFPA 70 National Electrical Codeb. NFPA 110 Emergency and Standby Pow

1.2 SUBMITTALS

 A. The following shall be submitted in accordance wPROCEDURES:

B. Dimensioned plans, sections and elevations showiand conduit entry provisions for each STS.

1 3 DELIVERY STORAGE AND HANDLING

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1.3 DELIVERY, STORAGE, AND HANDLING

 A. Government-Furnished Equipment (GFE): The Gcomponents and equipment listed in PART 2- PRContractor.

B. Delivery: Contractor shall receive GFE at the jobsite.and install GFE. Notify Contracting Officer [

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Static Transfer Switches shall be GFE. Product s

information purposes only. Such equipment requoperable Static Transfer Switches installation includeconduit, conduit fittings, insulated conductors, comprfasteners, and other such items.

2.2 STATIC TRANSFER SWITCH (STS) - GFE

 A. The Static transfer Switch is a Solid State Three Phaswitch with characteristics as indicated on the drawin

PART 3 - EXECUTION

3.1 INSTALLATION

 A. Conform to the requirements for electrical equipmenspecified herein, and in strict accordance with NFPA drawings and wiring. During and after installation, u

Contracting Officer, Contractor shall protect equipcontamination. Upon completion of the Static TransOfficer and Static Transfer Switch manufacturer's tethe installation for contract compliance. Contdeficiencies as directed.

B. Contractor shall notify Contracting Officer in writing completion of the Static Transfer Switch systemContracting Officer, will schedule the manufacturer's

the completed installation. The technical represenservice including _____days of instruction for activity

C. Installation Inspection: The Static Transfer Switch Contracting Officer, in the presence of the Contrainstallation. The Contractor shall correct constructdirected.

3.2 INSTRUCTIONS

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 A. Manufacturer's approved operating instructions shcabinet where operator can see them. One-line andshall be permanently secured to inside of front enclos

B. Training: The manufacturer shall provide one day offive (5) owner personnel in the operation of the STS u

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1. Insulation resistance shall be tested, both phas

2. Power failure of normal source shall be protective device. This test shall be performed

3. Power failure of emergency source with nsimulated by opening upstream protective detest shall be performed a minimum of five times

4. Low phase-to-ground voltage shall be simusource.

5. Operation and settings shall be verified for override time delay, transfer time delay, retu

features.6. Manual and automatic STS and BP/IS functions

END OF SECTION 16412

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16442 — INSTALLATION OF SWITCHBOARDS

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NECESFOLLOWING:

Modify specifications to suit project conditions, scope, all aptions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 REFERENCES

 A. The publications listed below form a part of this spec

the latest version of the reference publication shall ato in the text by the basic designation only.

1. INTERNATIONAL ELECTRICAL TESTING ASS

a. NETA ATS Electrical Power Distribution

2. NATIONAL FIRE PROTECTION ASSOCIATIO

a. NFPA 70 National Electrical Code

1.2 RELATED REQUIREMENTS

 A. Section 16050, "Basic Electrical Materials and "Apparatus Inspection and Testing" apply to this modifications specified herein.

1 3 SUMMARY

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1.3 SUMMARY

 A. The Contractor shall furnish and install the equipmenshall be as shown in the Drawings and outlined below

1.4 SUBMITTALS

 A. The following shall be submitted in accordance w

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

b. Switchboard production tests;

c. Acceptance checks and tests;

3. SD-11 Closeout Submittals

a. Equipment Test Schedule;b. Request for Settings;

1.5 DELIVERY, STORAGE, AND HANDLING

 A. Government-Furnished Equipment (GFE): The Gcomponents and equipment listed in PART 2- PRContractor.

B. Delivery: Contractor shall receive the GFE at the unpack, and install GFE. Notify Contracting Officewhen delivery on the site is required. GFE shall Contracting Officer to determine damage or missresponsible for damage sustained by the materials aEquipment is heavy and easily damaged. Do not btime. When lifting, do not tip beyond 30 degrees.

PART 2 - PRODUCTS

2.1 CONTRACTOR FURNISHED MATERIAL AND EQU

 A. Switchboards shall be GFE. Product specification

purposes only. Such equipment required to prSwitchboards installation includes, but is not necesfittings, insulated conductors, compression lugs, cabother such items.

2.2 PRODUCT COORDINATION

 A. Products and materials not considered to be switchbspecified in Section 16402, "Interior Distribution Syste

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2.3 SWITCHBOARD - GFE

1. NEMA PB 2 and UL 891.

B. The voltage and ampere rating of the switchboacontinuous current rating of the main bus shall be as

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

PART 3 - EXECUTION

3.1 INSTALLATION

 A. Conform to the requirements for electrical equipmentin strict accordance with IEEE C2 and NFPA 70drawings and wiring. During and after installation, uContracting Officer, Contractor shall protect equipcontamination. Upon completion of the Switchboardand Switchboards manufacturer's technical represen

for contract compliance. Contractor shall correct inst

B. Contractor shall notify Contracting Officer in writing completion of the Switchboards system installatioOfficer, will schedule the _____manufacturer's techncompleted installation. The _____technical represeservice including _____days of instruction for activity

C. Installation Inspection: The Switchboards technical rOfficer, in the presence of the Contractor, will inspeContractor shall correct construction or installation de

3.2 GROUNDING

 A. NFPA 70 and IEEE C2, except that grounds and resistance to solid earth ground not exceeding 5 ohm

B. Grounding Electrodes: Connect ground conductorsrods by exothermic weld or compression connector. at equipment end of ground conductors.

C. Equipment Grounding: Provide bare copper cable nless than 24 inches below grade connecting to the inin addition to that indicated or specified is directeresistance, the provision of the contract covering "Cha

D. Connections: Make joints in grounding conductors

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D. Connections: Make joints in grounding conductorsBonding resistance of all interconnections shall be (when measured with a 4-terminal milliohm meconnection for all underground and limited accessconnections for all other locations.

E. Grounding and Bonding Equipment: UL 467, eth i

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Meters and Instrument Transformers: NEMA C12.1.

D. Galvanizing Repair: Repair damage to galvanized crich paint, for galvanizing damaged by handling, bolting. Do not heat surfaces that repair paint has be

3.4 FOUNDATION FOR EQUIPMENT AND ASSEMBLIE

 A. Interior Location: Mount switchboard on concrete sthe slab shall be at least 4 inches thick. The to

approximately 4 inches above finished floor. Edgechamfer. The slab shall be of adequate size to proequipment. Provide conduit turnups and cable equipment to be mounted. Seal voids around conduoil-resistant caulking or sealant. Cut off and bussurface. Concrete work shall be as specified in Concrete".

3.5 FIELD QUALITY CONTROL

 A. Contractor shall submit request for settings of breakeapproval of switchboard and at least 30 days inContractor shall set all settings.

B. Performance of Acceptance Checks and Tests: manufacturer's recommendations and include the inspections and electrical tests, performed in accorda

1. Switchboard Assemblies

a. Visual and Mechanical Inspection

1) Compare equipment nameplate approved shop drawings.

2) Inspect physical, electrical, and me3) Confirm correct application of

lubricants.

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4) Verify appropriate anchorage, requalignment.

5) Inspect all doors, panels, and sectiand missing hardware.

6) Verify that [fuse and] circuit breakapproved shop drawings.

7) V if th t t t f t

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

10) Clean switchboard.

11) Inspect insulators for evidence of surfaces.12) Verify correct barrier [and shutter] in13) Exercise all active components.14) Inspect all mechanical indicating de15) Verify that vents are clear.16) Test operation, alignment, and pen

withdrawal disconnects.17) Inspect control power transformers.

b. Electrical Tests

1) Perform insulation-resistance tests 2) Perform overpotential tests.3) Perform insulation-resistance test

this test on wiring connected to soli4) Perform control wiring performance

5) Perform primary current injection teeach section of assembly.6) Perform phasing check on doub

correct bus phasing from each sour7) Verify operation of switchboard hea

2. Circuit Breakers - Low Voltage - Power

a. Visual and Mechanical Inspection

1) Compare nameplate data with sdrawings.

2) Inspect physical and mechanical co3) Confirm correct application of

lubricants.4) Inspect anchorage, alignment, and

Inspect moving and stationary coalignment.

5) Verify that all maintenance device

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) yoperating the breaker.

6) Verify that primary and secondary cvital to satisfactory operation of the

7) Perform all mechanical operator anthe breaker and its operating mech

8) Inspect all bolted electrical connect

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1) Perform contact-resistance tests on

2) Perform insulation-resistance tests.3) Adjust Breaker(s) for final settingsprovided settings.

4) Determine long-time minimum piinjection.

5) Determine long-time delay by prima6) Determine short-time pickup and de7) Determine ground-fault pickup and 8) Determine instantaneous pickup va

9) Activate auxiliary protective devundervoltage relays, to ensure opethe operation of electrically-operate

10) Verify correct operation of any aupickup indicators, zone interlocoperation, trip-free, and antipump fu

11) Verify operation of charging mecha

3. Circuit Breakers: [Low Voltage - Insulated-CCase with Solid State Trips]

a. Visual and Mechanical Inspection

1) Compare nameplate data with sdrawings.

2) Inspect circuit breaker for correct m3) Operate circuit breaker to ensure sm

4) Inspect case for cracks or other def5) Inspect all bolted electrical connect

resistance ohmmeter, verifying connections and/or cable connectmethod, or performing thermograph

6) Inspect mechanism contacts and ar

b. Electrical Tests

1) Perform contact-resistance tests.

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)2) Perform insulation-resistance tests.3) Perform Breaker adjustments for

Government provided settings.4) Perform long-time delay time-curren5) Determine short-time pickup and de6) Determine ground-fault pickup an

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

a. Visual and Mechanical Inspection

1) Compare equipment nameplate approved shop drawings.

2) Inspect physical and mechanical co3) Verify correct connection.4) Verify that adequate clearance

secondary circuit.5) Inspect all bolted electrical connect

resistance ohmmeter, verifying

electrical connections by calibraperforming thermographic survey.

6) Verify that all required grounding good contact.

b. Electrical Tests

1) Perform resistance measurementswith low-resistance ohmmeter, if ap

2) Perform insulation-resistance tests.3) Perform polarity tests.4) Perform ratio-verification tests.

5. Metering and Instrumentation

a. Visual and Mechanical Inspection

1) Compare equipment nameplate approved shop drawings.

2) Inspect physical and mechanical co3) Verify tightness of electrical connec

b. Electrical Tests

1) Determine accuracy of meters at 2scale.

2) Calibrate watthour meters accordd t

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data.3) Verify all instrument multipliers.4) Electrically confirm that current tra

secondary circuits are intact.

6. Grounding System

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1) Perform ground-impedance mea

potential method. On systems corods, perform tests after interconneconsisting of a single ground rod connected. Take measurements than 48 hours after rainfall. Use a accordance with manufacturer's ingroup of grounds. The instrumenreading directly in ohms or fractiovalue of the ground rod or groundin

2) Submit the measured ground resgrounding system, indicating the lsystem. Include the test method used to determine ground resistanthe measurements were made.

C. Follow-Up Verification

Upon completion of acceptance checks, settings, and tests,demonstration in service that circuits and devices are in gooerly performing the intended function. Circuit breakers shall protective device. Test shall require each item to perform itstimes. As an exception to requirements stated elsewhere in cer shall be given 5 working days advance notice of the dateand tests.

END OF SECTION

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16461 – INSTALLATION OF DRY TYPE TRANSFO

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, environmental conditions and seismic requirements.

Include references to all applicable related sections, sudivisions 2 through 14 sections, mechanical division 15sections and division 1 section.

PART 1 - GENERAL

1.1 RELATED DOCUMENTS

 A. Drawings and general provisions of the Contract, Division 1 Specification Sections, apply to this and ot

1.2 SUMMARY

 A. This Section describes the requirements for teTransformers. Refer to Part 2-PRODUCTS , for Equipment (GFE).

1.3 SUBMITTALS

 A. Qualification data for firms and persons specified in demonstrate their capabilities and experience. Incprojects with project names and addresses, andrespective Owner’s Representatives and Owners.

B. Field test reports of tests and inspections condu

Section.

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1.4 DELIVERY, STORAGE, AND HANDLING

 A. Government-Furnished Equipment (GFE): The Gcomponents and equipment listed in PART 2- PRContractor.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Temporary Heating: Apply temporary heat

recommendations within the enclosure of each ventiduring which equipment is not energized and is nounder normal control of temperature and humidity.

1.5 QUALITY ASSURANCE

 A. Field-Testing Agency Qualifications: To qualify for acagency must demonstrate, based on evaluatioconforming to ASTM E 699, that it has the experien

conduct the testing indicated.

B. Comply with NFPA 70 "National Electrical Code."

C. Comply with IEEE C2 "National Electrical Safety Cod

1.6 COORDINATION

 A. Coordinate size and location of concrete bases, caconcrete reinforcements and formwork requirements

PART 2 - PRODUCTS

2.1 GENERAL PUPOSE, DRY-TYPE TRANSFORMERS

PART 3 EXECUTION

3.1 INSTALLATION

 A. Arrange equipment to provide adequate spacing circulation. Examine walls and floors for suitatransformers will be installed.

B. Install floor-mounting transformers level on concrete

not less than four inches larger in both directions thhigh.

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g

C. Identify transformers and install warning signs accordElectrical Identification.

D. Tighten electrical connectors and terminals accordtorque-tightening values Where manufacturer's tor

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G. Do not use expansion bolts to fasten the transformer

H. Locate wiring compartment at bottom to ensure termitemperature level. Conduit entrances shall be the loarea suitably marked.

3.2 GROUNDING

 A. Transformer secondary winding neutral, core and accordance with the latest National Electrical Code re

3.3 FIELD QUALITY CONTROL

 A. Independent Testing Agency: Provide services of agency according to the requirements of Division 1 Sto perform tests on installations made under this Sect

B. Test Objectives: To ensure transformer installation manufacturer's tolerances, install according to Contenergizing.

C. Test Labeling: Upon satisfactory completion of testssigned "Satisfactory Test" label to the tested compon

D. Schedule tests and provide notification at least commencement.

E. Report: Submit a written report of observations andand workmanship.

F. Tests: Include the following minimum inspectiomanufacturer's instructions. Conform to IEEE Standtype units, test method, and data correction factors.

1. Inspect accessible components for cleanlinintegrity, for presence of damage or deterior

temporary shipping bracing. Do not proceedcorrected.

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a. Include internal inspection through accesb. Inspect bolted electrical connection

manufacturer's published torque values UL standards 486A and 486B.

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7. Applied Voltage Test - 4kV

8. Ratio and Polarity Test9. Induced Voltage Test - Two times the normal vo

G. Test Failures: Correct deficiencies identified by testsmeets the specified requirements.

3.4 ADJUSTING

 A. After completing installation, cleaning, and testing,

finish to match original finish.

B. Adjust transformer taps to provide optimum voltage throughout the normal operating cycle of the facility. to submit with test results.

END OF SECTION 16461

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SECTION 16610 – INSTALLATION OF UNINTERRUPTIBLE

SINGLE MODULE

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NTHE FOLLOWING:

Modify specifications to suit project conditions, scope, environmental conditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 SUMMARY

 A. This Section describes the requirements for testing aSupply (UPS) equipment as specified herein. Refer tof Government Furnished Equipment (GFE).

B. The Installing Contractor shall be required to provide

1. Unloading, rigging and installation.2. Concrete pads and superstructure reinforceme3. Interconnecting wiring external to the enclosure4. Conduit external to the equipment specified her5. Cabling for site tests.

1.2 DEFINED TERMS

 A. Refer to the Instructions to Bidders Section for appearing in this Specification.

B. The following special terms appearing in this Spe

following meanings:

1 “Uninterruptible Power Supply System” or “UPS

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1. Uninterruptible Power Supply System or UPSUninterruptible Power Supply System, inclubatteries and associated accessories.

2. The term "Manufacturer" or "Vendor" shall mespecific equipment referred to in these Specific

3. The term "Contractor", “Installing Contractor”

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. Submit scaled drawings for Switchboard installation

dimensions, front view and sectional view.

1.4 APPLICABLE CODES, STANDARDS, AND APPROVA

 A. The design, equipment, installation and testing sapplicable requirements set forth in the following stan

1. National Fire Protection Association: (NFPA)

2. NFPA-70 (National Electrical Code)3. NETA ATS (International Electrical Testing

Specifications)

1.5 DELIVERY, STORAGE, AND HANDLING

 A. Government-Furnished Equipment (GFE): The Gcomponents and equipment listed in PART 2- PRContractor.

B. Delivery: Contractor shall receive GFE at the jobsiteand install GFE. Notify Contracting Officer on-site prequired. GFE shall be unpacked in the presence odamage or missing parts. Contractor shall be respthe materials and equipment after this inspection. damaged. Do not bump or bounce equipment at abeyond 5 degrees.

PART 2 - PRODUCTS

2.1 CONTRACTOR FURNISHED MATERIAL AND EQU

 A. UPS, Batteries, and Battery Packs shall be GFE. Pris for information purposes only. Such equipment roperable UPS, Batteries, and Battery Packs installatlimited to, conduit, conduit fittings, insulated cond

trays, supports, fasteners, and other such items.

S S S G

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2.2 UPS SYSTEM - GFE

 A. The UPS shall be comprised of one UPS module opThere are 6 systems being installed for CR/DR contphase, solid-state, single-module, uninterruptible powbe referred to as the UPS The UPS shall provide co

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

1. One rectifier/battery charger/inverter power contable No. 1 and as shown on drawings, includiinput isolation transformer.

2. One (1) battery circuit breaker disconnect switc3. UPS input and output circuit breaker.4. UPS system control including the static transfer

and all system control and monitoring.5. Module and system metering.6. System interfaces as required for monitoring

System (PMCS).

B. Modules shall convert incoming AC power to DC andstrings, one per module. At the same time they shathe inverters to reconstruct AC power at their outpusystem output bus to provide conditioned power to tutilized to power the critical load during out-of-tolepower, including total power outages for the specified

C. UPS system modules shall be capable of providing ffactor ranging from .8 (lagging) to 1.0 for 15 minuteDuration of less than 15 minutes at this kW rating fonot acceptable.

2.4 BATTERY, BATTERY RACKS, BATTERY SPILL CCIRCUIT BREAKER - GFE

PART 3 - EXECUTION

3.1 INSTALLATION

 A. Conform to the requirements for electrical equipmenspecified herein, and in strict accordance with installation drawings and wiring. During and afteaccepted by the Contracting Officer, Contractormoisture, dust, and contamination. Upon comContracting Officer and UPS manufacturer's technicinstallation for contract compliance. Contractor shalldirected.

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B. Contractor shall notify Contracting Officer in writing completion of the UPS system installation. At thisschedule the manufacturer's technical representinstallation and to perform start up on the equipment.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

and controls. All rigging required for unloadin

responsibility of the Contractor.

E. The UPS system shall be installed following the psystem Vendor. The Vendor shall assist the instinterpreting the installation instructions. The Contracthe Owner that the installation has been performed pand instructions. The Vendor’s field service persobattery installer to assure proper connection to the UP

3.2 START-UP COMMISSIONING

 A. After installation, the Vendor shall provide one representatives to assist and supervise start-up andadvise the Vendor at least 5 days in advance of the drequired. Such supervisors shall meet with the commissioning to establish a mutually agreeacommissioning testing activities. The supervisocontinuously until successful start-up completion.

B. The Contractor shall provide labor as required for The Contractor shall engage qualified electricians assystem.

C. UPS-testing

1. UPS-Module

a. UPS Data

1) Make:________________________2) Serial #: ____________________ k

b. Battery Data_

1) Make:____________________ Mo2) # of Strings: _______ Jars/string: __

Float/Cell: ____

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c. Steady-State Load Tests

1) Connect the RPM recorder to thetested.

2) Record the three phase input volta

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

3) Connect the RPM recorder to the tested.4) Record three phase output voltag

harmonic distortion (voltage and Record, on the attached data sheecurrent readings from the RPM rpanel at the following load levels:

a) 100% load.

b) 50% load.c) No load (0% load).

5) While 100% load is applied to theattached data pages:

a) Three phase current into the b) Three phase current into the

c) Three phase current into the

d. Transient Load Tests

1) Connect the Waveform Recorder tomeasure three phases of output vcurrent.

2) Record the following load step trans

a) 0% - 50% - 0%.b) 50% - 100% - 50%.c) 25% - 75% - 25%.

3) Connect the Waveform recorder tovoltage and one phase current of th

4) Record the following transfer transie

a) Normal transfer to bypass witb) Module failure to bypass withc) Move the waveform recorder

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from bypass to UPS with 100

e. Battery Discharge Test

1) Verify that the UPS Module’s low b

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4) Connect a Fluke multi-meter to me

shunt of the UPS module. Recorddischarge data sheet.5) Connect another Fluke multi-meter 6) Verify that 100% load is applied to t7) Send the UPS module to battery. R

a) The initial transfer to battery wb) DC bus voltage and current frc) DC bus voltage and DC shun

d) Infrared scan the batteries du

8) End the battery discharge test wheend of discharge voltage is reachebattery shutdown voltage is reache

10) Record the utility restoration and recorder.

f. Infrared Scan

1) Infrared scan the entire UPS moapplied for a minimum of 15 minute

2) Infrared scan all UPS batteries battery discharge.

3) Infrared scan all UPS batterieapproximately 5 minutes.

4) Transfer the UPS module to inter

internal bypass path once full loadof 15 minutes.

5) Transfer the UPS module to Maintthe load C side of the MBC cabinefor a minimum of 15 minutes.

3.3 SITE SYSTEM TESTS

 A. In general, the UPS system Vendor shall be responstests on the UPS system, including batteries and disccertify the proper operation of the system as a wproced re shall be pro ided b the UPS s stem Ven

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procedure shall be provided by the UPS system VenThe Vendor shall inspect the installation location of tchoosing locations for load bank installation. This teOwner and may occur during normal working hours, o

B A i i th f ll i it t t i

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4. Voltage regulation. Record L-L voltage for eac

a. Record each system output voltage at nob. Record each system output voltage at hac. Record each system output voltages at fud. Calculate the voltage regulation as follow

1) (L-NL)/NL)x100=%Voltage regulatio2) NL= No load volts3) L = 1/2 or full rated load volts

5. Transient Tests

a. A light beam recorder or equivalent bandwidth to record one cycle of a 1000 Hchannels to monitor three phase voltaoutput, single phase current input and sin

b. Record all system level voltages, currenoutput of steady state load steps prior to

Example: Step load from 25% to 75%. the 75% load setting before performing th

c. Each transient test listed below shall following criteria, except when noted othe

d. Plus 8% or minus 8% with a recovery ominus one percent of the initial steady smet by each individual transient, measure

e. The method of measuring a transient is af. The steady state voltage envelope pri

millimeters is subtracted from the peamillimeters. This absolute difference is denvelope and multiplied by 100 to arrive a

g. An interruption of power under any of considered to be out of spec:

1) Load Step Transients:

a) For each module, perform the

(1) 0% to 50% to 0% of the(2) 25% to 75% to 25% of

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(2) 25% to 75% to 25% of (3) 50% to 100% to 50% o(4) 75% to 110% to 75% o(5) 0% to 100% to 0% of th

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4) Input Fail Transient: This test is to

battery, with module on-line and at voltage shall be monitored by the lig5) Note that the transients do not ex

output modulation of each module dthe formula below:

VM% = (Ep MAX - Ep MIN) x 10Ep MAX + Ep MIN

EpMAX = Maximum phase v

EpMIN = Minimum phase v

a) Remove the input power for ob) Repeat this test a total

consistency in performance.

6) Loss of Bypass Remove the bypasminutes. Reconnect the bypass a

system synchronizes to bypass.

6. Heat Run

a. Operate the entire system continuously load. For the first four hours operate with

b. Record the system output voltage, currenone hour time intervals to verify stability and record the room temperature throug

after 24 hours, perform an infrared scan o

7. System Battery Tests: The objective of this testbatteries with the associated UPS system and each module for the reserve time and to cut off

a. Prior to the start of the test, the batteryvoltage for the time specified by the batthe resistance of all inter-cell and inte

micro-ohmmeter or equivalent.b. Each module shall be tested with full lominimum of 10 minutes, to a cut offdi ti f tilit lt i t t

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disconnection of utility voltage input to moc. After module of each system has been s

batteries of system for minimum of 3 hotime perform system tests as specified.

d. The test shall be conducted with each U

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

minimum of five minutes to demonstrateinput current limit.

e. After successful completion of individufollowing system tests at full load using across system output.

1) Open utility input breaker, record oinput failure when inverter input tran

2) Close utility input breaker, record otime when inverter input transfer from

3) Fail UPS system, critical load transinput, record voltage and current duinverter output and utility.

4) Reestablish UPS system output, critby-pass to UPS output, record volttransfers between static switch and

f. The batteries shall be recharged to 95%discharge time. Record every thirty min

current, kW, pf, frequency and the Drecharge requirement is met.g. Upon successful completion of the bat

have a chance to reach their normal charof cell voltage readings, specific gravity a

h. After completion of discharge testing, more than ±10% of average voltage.

i. After completion of installation and acceVendor shall certify that installation is co

of Vendors requirements and that Vendor

C. An integral power system test designed to demonsystem in conjunction with the emergency generatoContractor with the assistance of the Vendor. The hours and shall prove the following:

1. Compatibility between the UPS system and tnot influence voltage regulation and the UP

generators.2. Ability of the UPS system to synchronize to the3. Ability of the UPS system to transfer the load

bypass and back while on generator power

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bypass and back while on generator power.4. Ability of the UPS to limit battery recharge curre

D. Live Load Test

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

2) Voltage unbalance

3) Modulation

2. Verify that the UPS system is capable of suload.

E. The Vendor shall provide qualified field service persosite tests. The Vendor’s field service technicinstrumentation, including line disturbance analyrecorders, required to perform the tests.

F. Electrical trade labor for all tests shall be provided by

G. The UPS system Vendor shall provide all special eqsite tests. Special equipment shall mean any instrurequired for testing UPS system equipment, and ntrade contractors.

H. Load banks and load bank cables as required for s

operated by the Installing Contractor.

END OF SECTION 16610

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FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

SECTION 16910 –EPMS LAN CABLE PLANT

NOTE TO SPECIFICATION WRITER:SPEC WRITER SHALL MODIFY THIS SPECIFICATION AS NECESFOLLOWING:

Modify specifications to suit project conditions, scope, all apconditions and seismic requirements.

Include references to all applicable related sectiondivisions 2 through 14 sections, mechanical divisiosections and division 1 section.

PART 1 - GENERAL

1.1 RELATED DOCUMENTS

 A. Drawings and general provisions of the Contract, Division 1 Specification Sections, apply to this and oth

1.2 SUMMARY

 A. This section includes the installation of a complete E(EPMS) cabling system as detailed in the DrawSpecifications.

B. The Contractor shall furnish and install the equipmento Government-Furnished EPMS equipment. The wiring diagram for Government Furnished EPMSraceways. All cabling types, enclosures and power EPMS equipment provider prior to submitting produc

C. Refer to the drawings and EPMS points list mamonitoring points and work to be performed.

1.3 SUBMITTALS

 A. Shop drawings shall clearly indicate the requirementfollowing shall be submitted:

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1. Catalog sheets indicating features, specificaticabinets, racks, patch panels, connectors anequipment specified herein).

2. Point-to-point wiring diagrams of all monit

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

5. Provide at least three references associated wGovernment may contact and/or visit. For ework performed; duration; and customer contac

6. Summary of experience installing pathwaycommunications systems as appropriate.

7. Resumes and backgrounds for all key persospecific project including those responsiblassurance, and safety. Resumes shall includetraining, licenses, and any certifications held

these personnel must be agreed upon between8. Provide a list of twisted-pair and fiber optic cab

certification.9. Cable termination and test plans as required.10. Provide all applicable portions of the following

sections listed in paragraph above, in additiowithin 10 days after completion of the tests for e

11. Test reports shall be submitted in the following 12. One copy on eight and one-half inch by eleve

reproducible printing. Also provide one copy diskette or compact disk in Microsoft Excel form

13. Submit test report documentation through the for specification conformance.

14. Twisted-pair field test documentation.

B. Bidders will provide a Compliance Review of the SpThe Compliance Review shall be a paragrap

Specifications with the following information, “C”, “D” original Specifications and any subsequent Addenda.

1. “C”: Comply with no exceptions.2. “D”: Comply with deviations. For each and eve

footnote with reasons for the proposed deviSpecification can be satisfied.

3. “E”: Exception, do not comply. For each numbered footnote with reasons and possible a

C. Unless a deviation or exception is specifically noteassumed that the Bidder is in complete compliance Deviations or exceptions taken in cover letters subs

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Deviations or exceptions taken in cover letters, subsby contradiction do not release the Bidder from beinthe exception or deviation has been specifically noteBidder may submit the latest state-of-the-art compondeviations from the Specifications must be approved

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

C. Provide passive cabling components for copper-pacabling. The installed cabling solution must be aConnectivity Solution 10-Year Extended Product WaProgram.

D. The installer must be certified by manufacturer toConnectivity Solution. The final deliverable for proregistered by manufacturer certifying the communicarepresentatives shall review and approve the part materials described in this Specification before order

E. Communications Cabling: The Contractor shallexperience performing cable placement, splicing, tefor each of the media types and system materSubcontract Documents, e.g., Category 6 UTP, singlIn the case of newer technologies that do not haveshall have documented experience for at least technology.

1. Project Manager, Supervisors, and Principal 5 years’ experience in like work.

2. Category 6 Unshielded Twisted Pair and documented training, licensing, and/or certispecified, as applicable.

1.5 STANDARDS

 A. All equipment, material, work and testing supplied latest edition and amendments of all applicable standlisted below:

1. American National Standards Institute (ANSI)2. National Electrical Code (NEC)3. Underwriters’ Laboratories, Inc. (UL)4. Institute of Electrical and Electronics Engineers5. National Electrical Manufacturers’ Association (

6. Federal, State and local codes and laws.7. International Standards ISO/IEC 11801.8. EIA/TIA-568-A, Commercial Building Telecomm9 EIA/TIA 569 Commercial Building Standard for

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9. EIA/TIA-569, Commercial Building Standard for10. TIA/EIA TSB-67, Transmission Performance

Unshielded Twisted-Pair Cabling Systems.11. International Standard ANSI/IEEE 802.3.12 EIA/TIA 606 C i l B ildi Ad

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

communications cables shall conform to NatiOptical Fiber Cables.

B. All equipment furnished shall be in accordance withrequirements of the Federal Government, State and c

1.6 IDENTIFICATION

 A. All panels, devices and equipment shall be identified

nameplates.

B. Except as otherwise noted, nameplates shall be of lbeveled edges and engraved to display white charact

C. Nameplates shall be attached using self-tapping stain

D. The Vendor shall submit a nameplate inscription Government prior to engraving the nameplates.

1.7 OPERATING AND MAINTENANCE INSTRUCTIONS

 A. The Vendor shall furnish to the Government operatineach piece of equipment, each device and for the coand devices supplied.

B. The instructions shall provide detailed descriptions oof the equipment or device, manufacturer’s literature

internal wiring diagrams, electrical characteristics aincluded. All material should be bound in a hardcovcontents and tabs identifying all major sections.

1.8 WARRANTY

 A. General Warranty: The special warranty specified iOwner of other rights the Owner may have under Documents and shall be in addition to, and run conc

by the manufacturer under requirements of the Contr

B. A ten (10) year extended product warranty and apsystem shall be provided for all new cabling as follow

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system shall be provided for all new cabling as follow

1) The 10-year extended product warranty shall covdefective product(s) and labor for the replacemeproduct(s) for a ten (10) year period

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

 A. All equipment and material shall be shipped to the job

B. All equipment shall be adequately protected, bracedand environmental damage during transit and handinstalled on the major equipment during shipping shawith the associated equipment.

C. Delivery: Contractor shall receive, GFE at the jobsiteand install GFE. Notify Contracting Officer [____delivery on the site is required. GFE shall be unpacOfficer to determine damage or missing parts. Cdamage sustained by the materials and equipmeequipment is heavy and easily damaged. Do not btime. When lifting, do not tip beyond 5 degrees.

1.10 EXTRA MATERIALS

 A. Vendor to supply a recommended spare parts list wit

PART 2 - PRODUCTS

2.1 EPMS LAN CABLE PLANT

 A. General

1. The Contractor shall be responsible for:

a. Providing all materials, and the necessaensure a complete Cat 6 cabling systemintent of the Contract Documents. Subcon

b. Furnishing and installing all incidentaspecified, but which are required by goofunctional system.

c. Coordinating the details of facility equspecification divisions, which affect the w

d. Coordinating all activities with the overall e. Ensuring materials in excess of those re

kept in their original condition and packag

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2. Summary Description Scope of Work

a Furnish and install Category 6 cable cab

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e. Provide and install fire stopping of aContract Documents.

f. Provide and install labeling of the newlythis Section.

g. Exposed cable installed in underfloor cmeet NEC Article 645.

3. Intent of Drawings:

a. EPMS LAN and Cable Plant Drawingsequipment, devices, raceways, cable tradimensioned.

b. The Contractor shall be responsible for thequipment, cable, raceways, cable tray,according to the Contract Documents aGovernment. Raceways are to be Contractor.

c. If found, refer any conflicts within the Conresolution.

2.2 FIELD HARDWARE COMPONENTS

 A. Advanced Web Enabled Revenue Accurate PoweTransient Detection: Installed and wired by swEthernet connection, GPS synch signal, cabling, andto I/O as indicated on the drawings.

B. Sequence of Event Recorders: Installed and wiredconnection, programming and GPS synch signal.

C. Video Display Terminals with Industrial PC: Insmanufacturer. Provide Ethernet connection.

D. Ethernet Gateways: Installed and wired by Contracto

1. Ethernet Gateway shall feature one 10/100 Moptic port.

E. Horizontal Cable

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1. Horizontal Cables: Plenum rated.2. Horizontal cables shall be clearly factory-labele

foot to easily differentiate Category type

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F. Connectors

1. UTP: Category 6, 8-position/8-conductor moduoval or round four-pair UTP.

2. Fiber Optic: Duplex LC or Simplex SC configurtermination type with equipment provided.

G. Backbone Copper Cable

1. Backbone Cables: Plenum rated.2. Backbone cables shall be clearly factory-labele

foot to easily differentiate Category type.

H. Single-Mode Fiber Optic Cable

1. Single-mode optical fibers shall be Class IVa dioptical fibers, which comply with ANSI/EIA/TIA-optic cable cores consist of 8.3/125/250, 8.2/12fibers which meet or exceed the following optic

a. Zero Dispersion Wavelength: between 1,b. Maximum Value of Dispersion Slope at S

nm2.c. Nominal Diameter: 8.7 um to 10 um with

at 1,300 nm.

d. Maximum Attenuation:

1) 0.7 dB per km at 1,310 nm.2) 0.7 dB per km at 1,550 nm.

2. Type 8.3/250: 8.3/125/250 single-mode fiber nonmetallic construction and filled loose tube co

3. Type 8.3/900: 8.3/125/900 single-mode fiber nonmetallic construction, a core of individually tOFNR as shown in the Drawings.

I 62 5 M lti d

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I. 62.5 Multimode

1. Multimode fiber optic cable cores shall be Classwith nominal 62 5/125 core/cladding diameter

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

b. Bandwidth range:

1) 500 to 1000 MHZ per km2) 500 to 1500 MHZ per km

2. Type 62.5/125: 62.5/125 multimode fiber opticconstruction, a core of individually tight bufferedOFNP as shown in the CD.

J. Fiber Optic Connectors

1. Terminate 62.icron multimode fiber optic strandmultimode connectors, as indicated on the pull

2. Terminate single-mode fiber optic strands at bomode connectors, as indicated on the pull sche

3. Terminate fiber optic connectors with the manuterminating procedures.

K. Fiber Patch Panels

1. Install couplers/connectors in adapter panels andistribution shelf. Use separate adapter panels and different fiber optic type. Refer to pull sched

L. Communications Cable Management Accessories

1. Horizontal cable management panels 2 Rack Umanagement panels 3” wide. Cable managers cover panels

M. RS 485 Paired Instrumentation Cable for trip units

1. 2 pair, 4 conductor, unshielded, 22 AWG, 7x30polypropylene insulation with 8 twists per foot.

2. Aluminum Foil-polyester tape inner shield, 100%ohms impedance, 0.17 uH/ft nominal inductancat 1 kHz, 300 V RMS.

N IRIG B/GPS and DCF 77 Paired Instrumentation Cab

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N. IRIG-B/GPS and DCF-77 Paired Instrumentation Cab

1. 1 pair, 2 conductor, shielded, 18 AWG, 16x30 spolypropylene insulation with 8 twists per foot

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

P. Outlets

1. Faceplates

a. All faceplates shall be in a single gang cob. Surface mount boxes shall be available in

2. Outlets for voice and data:

a. Communications outlets shall consist of outlet boxes with plates equipped with 8shall utilize EIA/TIA-T568B wiring. Provshown on the Drawings.

3. Outlet locations

a. Outlets installed within the switchgear wboxes.

b. Outlets installed in walls will be mounted ic. Unless otherwise noted on the floor p

outlets for 24 AWG copper cable shall boutlets.

e. Support universal applications in a mulmodular RJ-45 plugs. Provided with blamodule locations. Jack module arrangem

4. Category 6 outlets

a. All category 6 outlets shall meet or erequirements for connecting hardware, acommercial building telecommunications section. Conform to latest draft at time of

Q. Patch Panels

1. Category 6 RJ45 Modular Patch Panel

a Used in the Mezzanine patch racks to d

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a. Used in the Mezzanine patch racks to dthe wall mounted distribution cabinets ofield.

b Mounted on 19" equipment rack

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

S. Modular Patch Cords

1. Provide modular patch cords for each assigncords shall conform to the requirements of Etelecommunications cabling standard, horizont

the UL LAN certification and follow-up prograan 8 pin modular connector on each end aspecified on the detailed drawing. Cordconfiguration.

2. All Category 6 cordage shall be round, and coconductors, tightly twisted into individual pairs.

T. Grounding

1. Grounding conductors of the size and type sminimum of 6-AWG insulated copper wire.

2. Provide solid copper busbar, predrilled for lthickness of ¼ inch, for racks and cabinets. :

3. Provide solid copper busbar, predrilled for lthickness of ¼ inch, in Building Engineer’s Officto the grounding electrode system and thecabinets.

U. Unspecified Equipment and Material

1. Any item of equipment or material not specifica

in this Specification and required to provide a cinstallation shall be provided in a level of quaitems.

PART 3 - EXECUTION

3.1 IDENTIFICATION

 A. Provide warning signs to conform with OSHA and Sta

3.2 FIELD QUALITY CONTROL

 A. Contractor shall notify Contracting Officer in writing f S

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completion of the EPMS wiring installation. At thisschedule the EPMS manufacturer's technical represinstallation.

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

3.3. DEFINITION OF ACCEPTANCE

 A. System acceptance shall be defined as that porequirements have been fulfilled:

1. All submittals and documentation have been su2. The complete system has successfully complet3. All punch list items have been corrected and ac

3.4 PROJECT RECORD DOCUMENTS

 A. Provide detailed project record documentation for sin addition to the standard requirements, within 30 da

1. Maintain separate sets of red-lined record drawwhich show the exact placement and icomponents.

2. Provide communication pathway record drawinand routing for all components, e.g., manholcable tray, pull boxes, enclosures, telecommun

3. Provide communication room record drawings wall components; e.g., conduit, wireway, cabcabinets, equipment racks, cross-connect equip

4. Provide communication wiring and cabling recoindicate exact placement, routing, and conne

e.g., twisted-pair cables, splices, cable crosenclosures, telecommunications outlets, cross-5. Provide network schematics when appropriate.

3.5. INSTALLATION

 A. Contractor shall obtain EPMS vendor cabling instaOfficer prior to roughing in raceways or purchasing equipment locations, equipment cabinets or boxes, a

reviewed and coordinated with the EPMS vendor.

B. Install cable after interior of building has been physand all mechanical work likely to injure conductors ha

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y j

C. Before installing cabling, ensure all cable pathwaycleaned:

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

4. Install communications cable in accordance was not to exceed the manufacturer’s specified p

5. Provide pigtails of adequate length for neat, tra6. Provide protection for exposed cables where su

a. Provide abrasion protection for any cathrough holes or across edges of sheet m

b. When installing cable, insure that any le

floor are protected from traffic.

7. Cable Management Mountings, Hangerscommunications cable firmly in place using inde

a. Design and install straps, mountings, distribution rings, cable tie mountings, ansupport loads with ample safety factors adeflect cable. Do not use plumbers’ p

support.b. Do not fasten communications cable su

piping, ductwork, mechanical equipmenraceways, or wires used to supporcommunications cables to make contasupport wires, or lighting fixtures.

8. Communications Cable Ties: Cable ties and

shall be no more than hand tightened and scrimp, or otherwise change the physical chardistort the placement of twisted-pair componestresses due to overtightening of cable managtypes of cable ties:

a. Plenum Building Areas: Where cable space, use plenum-rated color-coded and

b. Nonplenum Building Areas: Use conven

velcro ties.c. Exterior and Underground Locations: Us

9. Cabling: Utilize continuous unspliced lengths o

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g p gstrands between splice enclosures and/or term

a Arrange wire and cable neatly cut to p

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

10. The number of twisted-pairs or fiber strands

terminated and working.11. Place unshielded twisted-pair (UTP) cable so

bend radius limits specified by the manufactularger:

a. Horizontal Four-Pair Unshielded Twisted-

1) Termination Points: eight times the

2) Other Locations: four times the cab3) Multipair Unshielded Twisted-Pair Cradius of ten times the cable diame

12. To avoid stretching four-pair horizontal cable not exceed a 25-pound force pulling tension (te

13. Place copper cables transitioning between the in a neat and orderly manner per NEC 318.11transitioning bundles.

14. Directly terminate twisted-pair cable on wiring standard WECO color code order.

15. Use wiring block and/or connector manufactuproper-sized anvils for all copper punchdown, Stuffer caps are not permitted.

16. Unshielded twisted-pair connecting hardwarblocks, patch panels, connectors, TOs, crosspatch cords, and other components used

twisted-pair cable shall meet or exceed the  Additional Transmission Specifications for UnHardware, for the category of use specified in t

17. Cable Jackets: To reduce untwisting of pairs jacket as close as possible to the point of termi

a. Multipair Cable: Strip back only as muterminate on connecting hardware.

b. Horizontal Cable: Strip back no more tha

18. Pair Twist: Observe the EIA/TIA-568-A recowire pair twists as closely as possible to the poamount of untwisting in a pair as a result of te

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shall be no greater than 1 inch for multipairgreater than 1/2 inch for Category 6 cablesmaximum number of twists in the wire to minim

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

c. Conduit with Innerduct Installed: Suitable

and innerduct.d. After Cable Installed: Suitable duct wate

or between innerduct and cable.

20. Seal penetrations in fire-rated walls and floors.apply to the communications contractor:

a. Inspect firestopping installation by others

innerduct and conduit, sleeves, wireway, installation.b. Sleeves and Fire Barrier Sealing Systems

1) Sleeves: After cable installationpenetration sealing materials betwfire barrier sealing systems.

2) Raceways: After cable installatiopenetration sealing materials betwe

or wireway at all exposed penetratio3) Cable Trays: After cable installat

sealing materials to provide require

21. Provide each conduit passing from a nonhazhazardous area and each conduit entering an ewith a sealing fitting which meets applicable Nsealing fitting shall be UL-listed and shall

compound of the same manufacture.22. Protect adjacent surfaces from damage duRepair any damage.

23. Communication Spaces Grounding

a. Building Ground Busbars: Provide grcommunications space, connect to the buat the Main Grounding Block. Verify that and size conductor used for the main bu

busbar is not required if a building grounRefer to Ground Bus Detail shown construction.

b. Telecommunications Ground Busbars

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ground busbar hardware at each telecConnect the telecommunications grounbusbar located in the same room using

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

nearest access to the conduit or sleeve th

system.

3.6 CABLE TERMINATION, TEST PLANS AND TESTIN

 A. General:

1. Provide proof of testing technician(s) certificaunits of test equipment which are proposed for

2. The Contractor shall obtain Government approplan prior to execution of the work.3. This Section covers work necessary to furnis

cable system testing.4. Inspection Requirements:

a. As part of any performance test, inspect physical damage, continuity, and proper c

b. Verify identification and labeling at require

legibility, and accuracy.

5. Test Report Requirements: Each test report sh

a. Scope of testing.b. List of equipment used in the test with

certificate.c. List of technician performing the tests iden

d. Summary of Test Results: The summaryContractor. The summary shall be provifirst uses the available columns providedsecond uses a template to be provided. forms are available to the EPMS Contract

e. Individual Test Data Sheets: The indideveloped and completed by the Contracscanners are typically acceptable providrequired by this Section.

6. Twisted-Pair Cable Tests: The most common are the time domain reflectometer (TDR), thetesters. NEXT testing shall be performed usinman fact rer

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manufacturer.7. Twisted-Pair Test Plans: Provide separate pos

Horizontal Subsystem twisted-pair segment tes

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

3. Testing shall be performed by responsible, qua

in the presence of the Owner or an authorized r

C. Unshielded Twisted-Pair Cable System Testing:

1. Link Test Configuration: Perform metered tesand/or four-pair UTP cable through the wiring the cable section and/or telecommunication oshall be undertaken as described in EIA/TIA TS

2. Channel Test Configuration: Perform meteredpair and/or four-pair UTP cable through the wend of the cable channel and/or telecommunicsections, cross-connection equipment, jumpecords, and station cords, but not including acshall be undertaken as described in TIA/EIA TS

3. Performance Testing:

a. Use field test instruments capable of the f

voltage measurements in accordance wrequired by EIA/TIA 568-A, and EIFrequencies up to 100MHz.

b. Test each horizontal link or channel palength, attenuation, skew, and near-end-EIA/TIA TSB67.

c. Test each T.O. for connectivity to the asand port using a ping test, and link light ve

d. Test Reports: Include field test results length in accordance with EIA/TIA TSBThe test summary shall include:

1) Cable identification as it appears on2) Cable identification as it appears on3) Cable identification as it is l

Specifications.

4) Pass/Fail Status.5) The individual test data sheet sha

produced by the cable scanning eq

D Fiber Optic Cable Reel Testing

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D. Fiber Optic Cable Reel Testing

1 The Contractor shall be responsible for perfor

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

b. Number each reel, list Contractor’s reel n

test data shipped with the cable reel, and Engineer approval.

c. Review factory-produced manufacturer’conformance to product specifications inDocuments.

d. Submit documentation providing the propduration, and scheduled date for the testin

e. Testing procedures shall permit recor

parameters for each fiber, including spacef. Test fiber optic components on the reeContract Documents and manufacturer’slength and attenuation are consistent wand reel identification.

g. Furnish a copy of the OTDR calibration celocation of testing.

h. Test each multimode fiber optic strand fo850 nm and 1,300 nm, using a recording t

i. Test each single-mode fiber optic strand f1,300 nm and 1,550 nm, using a recordcapabilities.

 j. All test results shall be equal to or betteSection 17020, Basic Communications Mstrands that do not meet this criteria shall

k. Submit field test documentation for einstallation, including CM’s signature for

shall include:

1) Cable identification as it appears on th2) Cable identification as it appears on th

from a. orc.3) Cable identification as it is labeled acc4) Pass or fail status for each fiber strand5) Individual test data sheets of the OTD

E. Testing And Inspection of Grounding System

1. Bonding resistance of all interconnections sheach bond when measured with a 4-terminal m

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2. Submit test results for all busbars installed wground of less than 1 ohm

FAA DTFA-AC-03-D-13284 EYP MCF NO. 1503022.00

5. Submit test results for 10 percent of multi-pair s

to telecommunications ground bus bar is less th

F. Final Test And Adjust

1. The Contractor shall be responsible for post-inscabling systems specified.

2. Testing procedures shall permit recording the lbudget, and tested parameters for each pair a

off by CM and A/E.3. Any cable links with pairs or fiber strands whcriteria shall be reterminated, respliced, or recharge.

4. Submit final field test documentation in list formapproval.

END OF SECTION 16910

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

APPENDIX E—DRAWINGS

E 1 DRAWING LIST

Drawing

NumberDrawing Title

E001 General Symbols and Abbreviations

E120LS Floor Plan – Type 2 Limited Space

E200 Typical Generator Room Layout

E201 Typical Generator Switchboard Room Layout

E202 Typical Input Switchboard Room Layout

E203 Typical UPS Room Layout

E204 Typical Battery Layout

E205 Typical STS and Maintenance Bypass Room Layout

E206 Typical Outdoor Equipment

E300 Kohler Generator Fuel Oil Consumption Chart

E320 Fuel Oil Flow Diagram – Type 2

E321Fuel Oil Flow Diagram – Perspective – Type 2

E322 Fuel Oil Connections Diagrams – Type 2

E420LSAElectrical Single Line Diagram – Type 2A – Limited Sp

Tracon & ATCT

E420LSBElectrical Single Line Diagram – Type 2B – Limited Sp

 ATCT CAB

E421 Equipment Description – Type 2

E422 Equipment Description – Type 2

E501 Electrical Details

E502 Electrical Details

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E502 Electrical Details

E503 Electrical Details – Type 2 & 3 STS Wiring Schematic

July 11, 2008 Design Guidel

 Appendix E—Drawings FAA Pow

Drawing

Number

Drawing Title

E721 Panel Schedules – Type 2

E722 Panel Schedules – Type 2

E723 Panel Schedules – Type 2

E801LS EPMS Details – Limited Space

E820LSAEPMS Monitoring Points – Type 2A Limited Space

E820LSB EPMS Monitoring Points – Type 2B Limited Space

E821LSA EPMS Wiring Diagram – Type 2A Limited Space

E821LSB EPMS Wiring Diagram – Type 2B Limited Space

E901 Signage and Labeling Example

E920 Signage and Labeling Standards – Type 2

E921 Signage and Labeling Equipment Naming – Type 2

E922 Signage and Labeling Equipment Naming – Type 2

E923 Signage and Labeling Equipment Naming – Type 2

Only Design Drawings are Part of the Design Guide.

The Reference Drawings shall be reviewed by Desig

design aspects and adapted to each site as applicab

shall be used by the design engineer to develop equ

signage, fuel systems, etc.

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4  8  9 . 6  0 

 5  0 

 3  6 .2  0 

 8  6  8 . 8  0 

 5  0 

 3  3 . 6  0 

 8  0  6 .4  0 

7  5 

 5 1 .2  0 

1  ,2 2  8 . 8  0 

7  5 

4  6 . 9  0 

1  ,1 2  5 . 6  0 

1  0  0 

 6 7 . 6  0 

1  , 6 2 2 .4  0 

1  0  0 

 6 1 .2  0 

1  ,4  6  8 . 8  0 

2  5 

1  8 . 0  0 

4  3 2 . 0  0 

2  5 

1  0 .7  0 

2  5  6 . 8  0 

 5  0 

 3 1 .7  0 

7  6  0 . 8  0 

 5  0 

2  3 . 8  0 

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7  5 

4  6 . 9  0 

1  ,1 2  5 . 6  0 

7  5 

4  0 . 8  0 

 9 7  9 .2  0 

1  0  0 

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1  , 5 4  8 . 0  0 

1  0  0 

 5 7 . 8  0 

1  , 3  8 7 .2  0 

2  5 

1  9 . 5  0 

4  6  8 . 0  0 

-

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 5  0 

 3  5 . 0  0 

 8 4  0 . 0  0 

-

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7  5 

 5 2 .1  0 

1  ,2  5  0 .4  0 

-

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1  0  0 

7 2 .1  0 

1  ,7  3  0 .4  0 

-

-

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2  5 

2  0 . 0  0 

4  8  0 . 0  0 

2  5 

1  8 . 9  0 

4  5  3 . 6  0 

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1  ,2  8 4 . 0  0 

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1  ,2  0  0 . 0  0 

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1  , 6  9 4 .4  0 

1  0  0 

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1  , 5  6  9 . 6  0 

2  5 

2 1 .7  0 

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2  5 

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 9  3  3 . 6  0 

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1  , 3  3  9 .2  0 

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1  0  0 

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1  , 6 2 2 .4  0 

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1  ,1  6  6 .4  0 

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1  , 0  8  9 . 6  0 

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1  , 6  6  5 . 6  0 

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1  , 5 2  8 . 8  0 

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2  ,2 4  6 .4  0 

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1  ,2  0  0 . 0  0 

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1  , 0  5  3 . 6  0 

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1  ,4  9 2 . 8  0 

1  0  0 

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2  ,2 1  0 .4  0 

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1  , 9  3 2 . 0  0 

2  5 

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7 4 1 . 6  0 

2  5 

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1  , 3 1 2 . 8  0 

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1  ,2  0  0 . 0  0 

7  5 

7  8 . 3  0 

1  , 8 7  9 .2  0 

7  5 

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1  ,7  0  6 .4  0 

1  0  0 

1  0 2 . 9  0 

2  ,4  6  9 . 6  0 

1  0  0 

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2  5 

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7  8 7 .2  0 

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1  ,4 1  8 .4  0 

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1  , 3 2 4 . 8  0 

7  5 

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2  , 0  3 7 . 6  0 

7  5 

7 7 . 9  0 

1  , 8  6  9 . 6  0 

1  0  0 

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2  ,7 2  8 . 8  0 

1  0  0 

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2  ,4  6 7 .2  0 

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 9 1 2 . 0  0 

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 5  0 

 6  6 .4  0 

1  , 5  9  3 . 6  0 

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1  ,4 1 1 .2  0 

7  5 

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7  5 

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1 2  3 . 0  0 

2  , 9  5 2 . 0  0 

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2  , 5  9 2 . 0  0 

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1  , 5 4  0 . 8  0 

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2  , 9 2  5 . 6  0 

1  0  0 

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2  , 6  5 2 . 0  0 

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 8  5  6 . 8  0 

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1  ,7  3 7 . 6  0 

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1  , 5 1 2 . 0  0 

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1  0  0 

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2  , 8  6  3 .2  0 

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1  , 6  5  6 . 0  0 

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 3  ,2 2  8 . 0  0 

1  0  0 

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2  , 9 2  5 . 6  0 

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4  , 5  9  6 . 0  0 

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7  5 

 0 .4  6 

1 1 . 0 4 

7  5 

 0 .4  6 

1 1 . 0 4 

1  0  0 

 0 . 6 1 

1 4 . 6 4 

1  0  0 

 0 . 6 1 

1 4 . 6 4 

2  5 

 0 . 3  0 

7 .2  0 

2  5 

 0 . 3  0 

7 .2  0 

 5  0 

 0 . 6  0 

1 4 .4  0 

 5  0 

 0 . 6  0 

1 4 .4  0 

7  5 

 0 . 8  0 

1  9 .2  0 

7  5 

 0 . 8  0 

1  9 .2  0 

1  0  0 

1 .1  0 

2  6 .4  0 

1  0  0 

1 .1  0 

2  6 .4  0 

2  5 

 0 . 6  0 

1 4 .4  0 

2  5 

 0 . 6  0 

1 4 .4  0 

 5  0 

 0 . 8  0 

1  9 .2  0 

 5  0 

 0 . 8  0 

1  9 .2  0 

7  5 

1 .1  0 

2  6 .4  0 

7  5 

1 .1  0 

2  6 .4  0 

1  0  0 

1 .4  0 

 3  3 . 6  0 

1  0  0 

1 .4  0 

 3  3 . 6  0 

2  5 

 0 . 8  0 

1  9 .2  0 

2  5 

 0 . 9  0 

2 1 . 6  0 

 5  0 

1 . 3  0 

 3 1 .2  0 

 5  0 

1 .2  0 

2  8 . 8  0 

7  5 

1 . 8  0 

4  3 .2  0 

7  5 

1 . 6  0 

 3  8 .4  0 

1  0  0 

2 . 3  0 

 5  5 .2  0 

1  0  0 

2 . 0  0 

4  8 . 0  0 

2  5 

 0 . 8  0 

1  9 .2  0 

2  5 

 0 . 8  0 

1  9 .2  0 

 5  0 

1 . 3  0 

 3 1 .2  0 

 5  0 

1 .2  0 

2  8 . 8  0 

7  5 

1 .7  0 

4  0 . 8  0 

7  5 

1 . 6  0 

 3  8 .4  0 

1  0  0 

2 .2  0 

 5 2 . 8  0 

1  0  0 

1 . 9  0 

4  5 . 6  0 

2  5 

1 . 0  0 

2 4 . 0  0 

2  5 

1 . 0  0 

2 4 . 0  0 

 5  0 

1 . 6  0 

 3  8 .4  0 

 5  0 

1 . 5  0 

 3  6 . 0  0 

7  5 

2 .2  0 

 5 2 . 8  0 

7  5 

2 .1  0 

 5  0 .4  0 

1  0  0 

2 . 9  0 

 6  9 . 6  0 

1  0  0 

2 . 6  0 

 6 2 .4  0 

2  5 

1 .2  0 

2  8 . 8  0 

2  5 

1 .1  0 

2  6 .4  0 

 5  0 

1 . 8  0 

4  3 .2  0 

 5  0 

1 .7  0 

4  0 . 8  0 

7  5 

2 . 5  0 

 6  0 . 0  0 

7  5 

2 . 3  0 

 5  5 .2  0 

1  0  0 

 3 .2  0 

7  6 . 8  0 

1  0  0 

2 . 9  0 

 6  9 . 6  0 

2  5 

1 .7  0 

4  0 . 8  0 

2  5 

1 . 6  0 

 3  8 .4  0 

 5  0 

2 . 5  0 

 6  0 . 0  0 

 5  0 

2 .4  0 

 5 7 . 6  0 

7  5 

 3 .4  0 

 8 1 . 6  0 

7  5 

 3 .1  0 

7 4 .4  0 

1  0  0 

4 .4  0 

1  0  5 . 6  0 

1  0  0 

4 . 0  0 

 9  6 . 0  0 

2  5 

1 . 8  0 

4  3 .2  0 

2  5 

1 .7  0 

4  0 . 8  0 

 5  0 

2 .7  0 

 6 4 . 8  0 

 5  0 

2 . 5  0 

 6  0 . 0  0 

7  5 

 3 .7  0 

 8  8 . 8  0 

7  5 

 3 .4  0 

 8 1 . 6  0 

1  0  0 

4 . 8  0 

1 1  5 .2  0 

1  0  0 

4 .4  0 

1  0  5 . 6  0 

2  5 

2 .2  0 

 5 2 . 8  0 

2  5 

2 .1  0 

 5  0 .4  0 

 5  0 

 3 . 8  0 

 9 1 .2  0 

 5  0 

 3 . 5  0 

 8 4 . 0  0 

7  5 

 5 .2  0 

1 2 4 . 8  0 

7  5 

4 . 8  0 

1 1  5 .2  0 

1  0  0 

 6 .7  0 

1  6  0 . 8  0 

1  0  0 

 6 .1  0 

1 4  6 .4  0 

2  5 

2 .4  0 

 5 7 . 6  0 

2  5 

2 . 3  0 

 5  5 .2  0 

 5  0 

4 .1  0 

 9  8 .4  0 

 5  0 

 3 . 8  0 

 9 1 .2  0 

7  5 

 5 . 9  0 

1 4 1 . 6  0 

7  5 

 5 .4  0 

1 2  9 . 6  0 

1  0  0 

7 . 6  0 

1  8 2 .4  0 

1  0  0 

 6 . 8  0 

1  6  3 .2  0 

2  5 

2 . 6  0 

 6 2 .4  0 

2  5 

2 .4  0 

 5 7 . 6  0 

 5  0 

4 . 3  0 

1  0  3 .2  0 

 5  0 

 3 . 9  0 

 9  3 . 6  0 

7  5 

 6 .4  0 

1  5  3 . 6  0 

7  5 

 5 . 9  0 

1 4 1 . 6  0 

1  0  0 

 8 . 5  0 

2  0 4 . 0  0 

1  0  0 

7 .7  0 

1  8 4 . 8  0 

2  5 

 3 .2  0 

7  6 . 8  0 

2  5 

2 . 5  0 

 6  0 . 0  0 

 5  0 

 5 . 0  0 

1 2  0 . 0  0 

 5  0 

4 .1  0 

 9  8 .4  0 

7  5 

 6 . 3  0 

1  5 1 .2  0 

7  5 

 5 .7  0 

1  3  6 . 8  0 

1  0  0 

 8 .1  0 

1  9 4 .4  0 

1  0  0 

7 .2  0 

1 7 2 . 8  0 

2  5 

2 . 8  0 

 6 7 .2  0 

2  5 

2 . 6  0 

 6 2 .4  0 

 5  0 

4 . 9  0 

1 1 7 . 6  0 

 5  0 

4 .4  0 

1  0  5 . 6  0 

7  5 

7 .2  0 

1 7 2 . 8  0 

7  5 

 6 . 5  0 

1  5  6 . 0  0 

1  0  0 

 9 .4  0 

2 2  5 . 6  0 

1  0  0 

 8 .4  0 

2  0 1 . 6  0 

2  5 

 3 . 3  0 

7  9 .2  0 

2  5 

 3 .2  0 

7  6 . 8  0 

 5  0 

 5 . 5  0 

1  3 2 . 0  0 

 5  0 

 5 .1  0 

1 2 2 .4  0 

7  5 

 8 .1  0 

1  9 4 .4  0 

7  5 

7 .2  0 

1 7 2 . 8  0 

1  0  0 

1  0 . 6  0 

2  5 4 .4  0 

1  0  0 

 9 . 5  0 

2 2  8 . 0  0 

2  5 

 3 . 6  0 

 8  6 .4  0 

2  5 

 3 .4  0 

 8 1 . 6  0 

 5  0 

 6 .4  0 

1  5  3 . 6  0 

 5  0 

 5 . 8  0 

1  3  9 .2  0 

7  5 

 9 . 3  0 

2 2  3 .2  0 

7  5 

 8 . 5  0 

2  0 4 . 0  0 

1  0  0 

1 2 . 0  0 

2  8  8 . 0  0 

1  0  0 

1  0 . 9  0 

2  6 1 . 6  0 

2  5 

 3 . 9  0 

 9  3 . 6  0 

2  5 

 3 . 6  0 

 8  6 .4  0 

 5  0 

 6 . 3  0 

1  5 1 .2  0 

 5  0 

 5 . 9  0 

1 4 1 . 6  0 

7  5 

 8 . 9  0 

2 1  3 . 6  0 

7  5 

 8 . 3  0 

1  9  9 .2  0 

1  0  0 

1 2 . 0  0 

2  8  8 . 0  0 

1  0  0 

1  0 . 8  0 

2  5  9 .2  0 

2  5 

4 .2  0 

1  0  0 . 8  0 

2  5 

 3 . 8  0 

 9 1 .2  0 

 5  0 

 6 . 8  0 

1  6  3 .2  0 

 5  0 

 6 .4  0 

1  5  3 . 6  0 

7  5 

1  0 . 0  0 

2 4  0 . 0  0 

7  5 

 9 .2  0 

2 2  0 . 8  0 

1  0  0 

1  3 .2  0 

 3 1  6 . 8  0 

1  0  0 

1 2 . 0  0 

2  8  8 . 0  0 

2  5 

 3 . 8  0 

 9 1 .2  0 

2  5 

 3 . 5  0 

 8 4 . 0  0 

 5  0 

 6 . 9  0 

1  6  5 . 6  0 

 5  0 

 6 . 3  0 

1  5 1 .2  0 

7  5 

1  0 . 0  0 

2 4  0 . 0  0 

7  5 

 9 .2  0 

2 2  0 . 8  0 

1  0  0 

1  3 .2  0 

 3 1  6 . 8  0 

1  0  0 

1 2 . 0  0 

2  8  8 . 0  0 

2  5 

4 . 9  0 

1 1 7 . 6  0 

2  5 

4 . 5  0 

1  0  8 . 0  0 

 5  0 

7 . 8  0 

1  8 7 .2  0 

 5  0 

7 . 8  0 

1  8 7 .2  0 

7  5 

1 1 . 0  0 

2  6 4 . 0  0 

7  5 

1  0 . 0  0 

2 4  0 . 0  0 

1  0  0 

1 4 . 9  0 

 3  5 7 . 6  0 

1  0  0 

1  3 .2  0 

 3 1  6 . 8  0 

2  5 

4 . 9  0 

1 1 7 . 6  0 

2  5 

4 . 6  0 

1 1  0 .4  0 

 5  0 

 8 . 0  0 

1  9 2 . 0  0 

 5  0 

7 . 5  0 

1  8  0 . 0  0 

7  5 

1 1 . 5  0 

2 7  6 . 0  0 

7  5 

1  0 . 5  0 

2  5 2 . 0  0 

1  0  0 

1  5 . 3  0 

 3  6 7 .2  0 

1  0  0 

1  3 . 8  0 

 3  3 1 .2  0 

2  5 

 5 . 5  0 

1  3 2 . 0  0 

2  5 

 5 .2  0 

1 2 4 . 8  0 

 5  0 

 9 . 3  0 

2 2  3 .2  0 

 5  0 

 8 . 8  0 

2 1 1 .2  0 

7  5 

1  3 . 5  0 

 3 2 4 . 0  0 

7  5 

1 2 .4  0 

2  9 7 . 6  0 

1  0  0 

1  8 . 9  0 

4  5  3 . 6  0 

1  0  0 

1 7 . 0  0 

4  0  8 . 0  0 

2  5 

 5 . 9  0 

1 4 1 . 6  0 

2  5 

 5 . 6  0 

1  3 4 .4  0 

 5  0 

1  0 . 0  0 

2 4  0 . 0  0 

 5  0 

 9 . 3  0 

2 2  3 .2  0 

7  5 

1 4 . 8  0 

 3  5  5 .2  0 

7  5 

1  3 .4  0 

 3 2 1 . 6  0 

1  0  0 

2  0 . 8  0 

4  9  9 .2  0 

1  0  0 

1  8 . 5  0 

4 4 4 . 0  0 

2  5 

 6 . 8  0 

1  6  3 .2  0 

2  5 

 6 . 3  0 

1  5 1 .2  0 

 5  0 

1  0 . 9  0 

2  6 1 . 6  0 

 5  0 

 9 . 8  0 

2  3  5 .2  0 

7  5 

1 4 . 8  0 

 3  5  5 .2  0 

7  5 

1  3 . 5  0 

 3 2 4 . 0  0 

1  0  0 

1  9 . 8  0 

4 7  5 .2  0 

1  0  0 

1 7 . 9  0 

4 2  9 . 6  0 

2  5 

7 . 3  0 

1 7  5 .2  0 

2  5 

 6 . 6  0 

1  5  8 .4  0 

 5  0 

1 1 . 6  0 

2 7  8 .4  0 

 5  0 

1  0 .4  0 

2 4  9 . 6  0 

7  5 

1  5 . 9  0 

 3  8 1 . 6  0 

7  5 

1 4 .4  0 

 3 4  5 . 6  0 

1  0  0 

2 1 . 6  0 

 5 1  8 .4  0 

1  0  0 

1  9 .2  0 

4  6  0 . 8  0 

2  5 

7 . 5  0 

1  8  0 . 0  0 

2  5 

7 .1  0 

1 7  0 .4  0 

 5  0 

1 2 . 8  0 

 3  0 7 .2  0 

 5  0 

1 1 . 8  0 

2  8  3 .2  0 

7  5 

1  8 . 5  0 

4 4 4 . 0  0 

7  5 

1 7 . 0  0 

4  0  8 . 0  0 

1  0  0 

2 4 .7  0 

 5  9 2 . 8  0 

1  0  0 

2 2 . 6  0 

 5 4 2 .4  0 

2  5 

 8 .4  0 

2  0 1 . 6  0 

2  5 

7 .7  0 

1  8 4 . 8  0 

 5  0 

1 4 . 3  0 

 3 4  3 .2  0 

 5  0 

1  3 .1  0 

 3 1 4 .4  0 

7  5 

2  0 . 9  0 

 5  0 1 . 6  0 

7  5 

1  9 . 0  0 

4  5  6 . 0  0 

1  0  0 

2  9 .2  0 

7  0  0 . 8  0 

1  0  0 

2  5 .4  0 

 6  0  9 . 6  0 

1  3 2  0 

7  0 

4  0  5 

 3  6  5 

 6  0  6  0  6  0 

 3  6  0 

 3  0  0 

2 7  0 

 3  3  0 

 6  0  6  0 

2 7  5 

2  6  5 

 6 1  0 

2  0 

2  0 

 3  0 

 3  0 

 3  0 

 3  0 

 6 1  0 

4  3  0 

 6  0 

1  8  0 

1  6  5 

 3  0 

 9  0 

 8  5 

1  8  0 

1  6  5 

1 4  5 

1 4  5 

1  6  0 

1  6  0 

1 1  5 

 9  0 

 6  0 

1  0  0 

1  3  0 

1 1  0 

 6  0 

 5 . 5  9 

 6  0 

4  0 

 6  0 

 6 

 6  0 

1  0 

2 7 

 5  0 

 6  0 

1 1 4  0 

 9  8  0 

4  0 

7  0  0 

 8 7  0 

4  0 

 9  5  0 

 9 1  0 

2 4  0 

2  5  0 

 5  0 

 5  0 

4  0  0 RE  OZ V 

 6  8  0 

4  0 

1  8  0 

2  0  0 

 6  0 

2 1  0 

2  3  0 RE  OZ V 

2  0  0 RE  OZ V 

2 4  0 

 6  0   6  0 

1  9  0 

2 2  0 

 6  0  6  0 

1  5  0 RE  OZ  J B 

1  3  5 RE  OZ  J  C 

1 2  5 RE  OZ  J B 

1 2  5 

 6  0   6  0 

1 4  0 

 3  9  0 

 3  5  0 

 3 1  0 

 5  5  0 

 5  5  0 

4  9  0 

 3 7  0 

2  0 

2  0 

2  0 

7 7 

 8 2 

1  0  0 

 8  0 RE  OZ  J B 

 6  0  6  0  6  0 

2  3  0 

 6  0 

 5  5 

 5  0 

1  0 

2 1  0 

 6  0 

 6 2 

 5 7 

1  5  0 

 3  3 

2 4 

4  0 RE  OZ  J B 

 3  0 RE  OZ  J B 

2  0 R OZ  J B 

1  0 

1  0 

 3  6 

1  0 

1 1  0 

1  0  0 

1 4  0 

 6  0  6  0 

2 7 

 3  5 

1  0 

2 4 

 6  0 

7  0 

1  5 

 6  0 

1  3 . 5 

1  0 

 3  0 

 6  0 

1  0 

1  0 

2  0 

 6  0 RE  OZ  J B 

 5  0 RE  OZ  J B 

1  0  0 RE  OZ  J  C 

1  0  0 RE  OZ  J B 

 8  0 RE  OZ  J  C 

1  5  0 RE  OZ  J  C 

 3  5  0 RE  OZ V 

 3  0  0 RE  OZ V 

2 7  5 RE  OZ V 

2  5  0 RE  OZ V 

M o d  el  

2  0 RE  OZ  J B 

1  5 R OY  /  R OZ 

1  0 R OY  /  R OZ 

 6 R OY  /  R OZ 

2  0  0 RE  OZ  J  C 

1  8  0 RE  OZ  J  C 

1  8  0 RE  OZ  J B 

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Design Guidelines—Type 2A & 2B Limited Space CPDS

FAA Power Services Group, CPDS Program Office

APPENDIX F—TIMETABLE FOR SCHEDULING

Sample timetable below:

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T Y P E 1 L i  mi   t   e d  S  p a c

 e G ov er nm en t  F  ur ni   sh  e d P 

 ow er E  q ui   pm en t  T i  m e t   a b l   e

f   or  S  ch  e d  ul  i  n g

E  Q UI  P ME NT 

T  a sk N a

m e

D ur  a t  i   oni  n

 C  al   en

 d  ar 

D a y s

N o t   e s /   S  c o p e

N-A T  C T  C  on s  t  r  u c  t  i   on

  d  a

 y  s 

B  OD

  d  a y 

P l   an t   s A  c  t  i  v i   t  i   e s P r i   or  t   oB  OD

  d  a

 y ? 

 S WI  T  C HB  OA RD S  , S  Q UA RE 

DF A A P  ur  c h  a s  eR e q u e s  t   /  P  ur  c h  a s  e Or  d  er P r  o c  e s  s 

 3  0  d 

 a y  s 

D ev  el   o p S h  o pDr  awi  n g s  , af   t   er  e q ui   pm en t   or  d  er i   s r  e c  ei  v  e d 

 3  0  d 

 a y  s 

 S h  o pDr  awi  n gR ev i   ew ,F A A  an d A  & 

1  5  d 

 a y  s 

E  q ui   pm en t  A  s  s  em b l   y 

1 2  0  d  a y  s 

E  q ui   pm en t  D el  i  v  er  y 

4  d  a y  s 

E P M S *   C  onn e c  t  i  v i   t   y I  n s  p e c  t  i   onN o t  i   c 

 e t   o S  q u ar  eD

1 4  d 

 a y  s 

B  ef   or  e e q ui   pm en t  i   s  en er  gi  z  e d  , c 

 al  l  f   or E P M S  c  onn e c  t  i  v i   t   y i  n s  p e c  t  i   on.

E P M S  C  onn e c  t  i  v i   t   y I  n s  p e c  t  i   on

4  d  a y  s 

I  n s  p e c  t  i   oni   s  s  e p ar  a t   ef  r  om s wi   t   c h  b  o ar  d  an d  c i  r  c  ui   t   b r  e ak  er i  n s  p e c  t  i   on ;  e q

 ui   pm en t  n o t  

 en er  gi  z  e d .T h i   s  t   a s k i   s  t  h  e S  q u a

r  eDE P M S  t   e c h ni   c i   ani  n s  p e c  t  i  n g t  h  e s i   t   e

 t   o en s  ur  e al  l   C  a t   5 

 or  6  an d  /   or f  i   b  er  c  a b l   e s  , an d  al  l   t  wi   s  t   e d  p ai  r  c  omm uni   c  a t  i   on an d  GP  S wi  r  e

 s h  av  e b  e en

 pr  o p er l   y i  n s  t   al  l   e d  b  y  t  h  e b  ui  l   d i  n g

 c  on t  r  a c  t   or  , an d  c  onn e c  t   e d  t   o t  h  e e q ui   pm

 en t  .T h i   s i   s  d  on e

 b  ef   or  e e q ui   pm en t  i   s  en er  gi  z  e d  an d  s wi   t   c h  b  o ar  d  s  t   ar  t   u p.

 S wi   t   c h  b  o ar  d  an d  C i  r  c  ui   t  B r  e ak  er  S  t   a

r  t   u pN o t  i   c  e t   o S  q u ar  eD

1 4  d 

 a y  s 

 C  al  l   S  q u ar  eDf   or  s wi   t   c h  b  o ar  d  s  t   ar  t   u p

 S wi   t   c h  b  o ar  d  an d  C i  r  c  ui   t  B r  e ak  er  S  t   a

r  t   u p

4  d  a y  s 

 S  q u ar  eD t   e c h ni   c i   an s i  n s  p e c  t   s  an d  s  e t   s  c i  r  c  ui   t   b r  e ak  er  s  , s  t   ar  t   s 2 - y  e ar  e q ui   pm en t  w ar r  an t   y .

E P M S  S  t   ar  t   u pN o t  i   c  e t   o S  q u ar  eD

1 4  d 

 a y  s 

 C  al  l   S  q u ar  eDf   or E P M S  s  t   ar  t   u p an d  t   e s  t  i  n g.

E P M S  S  t   ar  t   u p an d T  e s  t  i  n g

1 4  d 

 a y  s 

A l  l  E  G , S T  S  , UP  S  an d  S WB D s  t   a

r  t   u p s  ar  e c  om pl   e t   e d  b  ef   or  e t  h i   s  t   a s k i   s i  ni   t  i   a t   e d . S  q u ar  eD

i  n s  t   al  l   s  t  h  eE P M S  s  er v  er i  n a g gr  e

 g a t   e e q ui   pm en t  r  a c k .A l  l   e q ui   pm en t  i   s  e

n er  gi  z  e d  an d 

m oni   t   or i  n g p oi  n t   s  onE  G , UP  S  , S 

WB D /  P  an el   b  o ar  d  s  /   C i  r  c  ui   t  B r  e ak  er  s  , an d 

 S T  S  ar  e t   e s  t   e d .

T h i   s  s  t   ar  t   s  t  h  eE P M S  3 - y  e ar w ar r  an t   y .

 *  E l   e c  t  r i   c  al  P  ow er M oni   t   or i  n g S  y  s  t   em

 (  E P M S  )   b  y  S  q u ar  eD

I  n s  t   al  l   a t  i   on of   el   e c  t  r i   c  al   s  y  s  t   em: A l  l   c  on d  ui   t   p ow er  an d  s i   gn al   ,E  G , S WB D s  , U

P  S  , S T  S  an d  s  u b  p an el   s .

E n er  gi  z  eP  ow er  S  y  s  t   em

P  ow er  S  y  s  t   emF  un c  t  i   oni  n g.N o t  n e c 

 e s  s  ar i  l   y  t   e s  t   e d  , b  u t   al  l   p ow er  s  y  s  t   em c  om

 p on en t   s  d  own t   o c r i   t  i   c  al   p an el   s  an d  e s  s 

 en t  i   al   p an el   s  , a s  s h  own on g en er i   c T  y  p e

1  s i  n gl   el  i  n e

 d i   a gr  am , ar  e en er  gi  z  e d .

P  a g e1  of  

 3 

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T Y P E 1 L i  mi   t   e d  S  p a c e G ov er nm en t  F  ur ni   sh  e d P 

 ow er E  q ui   pm en t  T i  m e t   a b l   e

f   or  S  ch  e d  ul  i  n g

 S T A T I   C T RA N S F E R S WI  T  C H

 (   S T  S  )   ,

L - 3  C  OMM UNI   C A T I   ON S 

F A A P  ur  c h  a s  eR e q u e s  t   /  P  ur  c h  a s  e Or  d  er P r  o c  e s  s 

 3  0  d 

 a y  s 

E  q ui   pm en t   a s  s  em b l   y  b  e gi  n s  af   t   er  e q

 ui   pm en t   or  d  er i   s r  e c  ei  v  e d 

1  5  0  d  a y  s 

E  q ui   pm en t  D el  i  v  er  y 

4  d  a y  s 

 S T  S  S  t   ar  t   u pN o t  i   c  e t   oL - 3  C  omm uni   c  a t  i   on s 

1 4  d 

 a y  s 

 S T  S  S  t   ar  t   u p

1  d 

 a y 

L - 3  t   e c h ni   c i   an s  t   ar  t   u p of   S T  S  an d 

 b  e gi  n2 - y  e ar w ar r  an t   y .

 UNI  NT E RR UP T I  B L E P  OWE R

 S  UP P L Y  (   UP  S  )  

F A A P  ur  c h  a s  eR e q u e s  t   /  P  ur  c h  a s  e Or  d  er P r  o c  e s  s 

 3  0  d 

 a y  s 

E  q ui   pm en t   a s  s  em b l   y  b  e gi  n s  af   t   er  e q

 ui   pm en t   or  d  er i   s r  e c  ei  v  e d 

 6  0  d 

 a y  s 

E  q ui   pm en t  D el  i  v  er  y 

2  d  a y  s 

 UP  S  S  t   ar  t   u pN o t  i   c  e t   oV  en d  er 

1 4  d 

 a y  s 

 UP  S  S  t   ar  t   u p

1  d 

 a y 

V  en d  er '   s  t   e c h ni   c i   an s  t   ar  t   u p of   UP 

 S  an d  b  e gi  n2 - y  e ar w ar r  an t   y .

E N GI  NE  GE NE RA T  OR (  E  G )   ,

K  OHL E R

F A A P  ur  c h  a s  eR e q u e s  t   /  P  ur  c h  a s  e Or  d  er P r  o c  e s  s 

 3  0  d 

 a y  s 

E  q ui   pm en t   a s  s  em b l   y  b  e gi  n s  af   t   er  e q

 ui   pm en t   or  d  er i   s r  e c  ei  v  e d 

1  8  0  d  a y  s 

E  q ui   pm en t   d  el  i  v  er  y 

2  d  a y  s 

E  G S  t   ar  t   u pN o t  i   c  e t   oK  oh l   er Di   s  t  r i   b  u t   or 

1 4  d 

 a y  s 

E  G S  t   ar  t   u p

1  d 

 a y 

P  OWE R S Y  S T E MT E  S T I  N G

N o t  i   c  e t   oP  ow er  S  y  s  t   em s  Of  f  i   c  e (  P  S  O )  

 3  0  d 

 a y  s 

N o t  i  f   y P  S  Owh  en e q ui   pm en t  i   s  en er  gi  z  e d  an d  af   t   er  s  t   ar  t   u p of   al  l   p ow er  s  y 

 s  t   em e q ui   pm en t   ,

i  n c l   u d i  n gE P M S .

P  ow er  s  y  s  t   em t   e s  t  i  n g

1 4  d 

 a y  s 

 C  an b  e c  o or  d i  n a t   e d wi   t  h  J A I   /   C A I  .

P  ow er  S  y  s  t   em e q ui   pm en t  i  n s  t   al  l   e d  a

n d f   un c  t  i   oni  n g.N o t  n e c  e s  s  ar i  l   y  t   e s  t   e d  , b 

 u t  E  Gi   s  c  onn e c  t   e d  an d r  e a d  y f   or  s  t   ar  t   u p.

P  ow er  S  y  s  t   em e q ui   pm en t  i  n s  t   al  l   e d  a

n d f   un c  t  i   oni  n g.N o t  n e c  e s  s  ar i  l   y  t   e s  t   e d  , b 

 u t   S T  S  s  ar  e en er  gi  z  e d  an d r  e a d  y f   or  s  t   a

r  t   u p.

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wi  r  e s  ar  e c  on t  r  a c  t   or f   ur ni   s h  e d .

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