AIRCRAFT MANUAL SUPPLEMENT
To support Instructions for Continued Airworthiness in accordance with Regulations EASA CS-25.1529/FAR 14 CFR-25.1529, Appendix H.
365 Aerospace Modification MOD-0228 – ‘EFIS pin programming to TNT standard Document No: AMS-0228-001
Intro Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
HIGHLIGHTS Highlights of future amendments will be listed below
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
RECORD OF REVISION
Issue Date Issue Date
Initial (1) Jan 09/2017
The Aircraft Manual Supplement (AMS) is to be used in conjunction with the related aircraft’s manuals. The information contained within this manual relates to various alterations/changes/modifications that have been carried out on the associated aircraft. A list of effective alterations/changes/modifications can be found in the Introduction pages to this manual. These alterations/changes/modifications are in addition to the initial design of the aircraft and are therefore detailed within this manual using appropriate and related convention. This manual complies with EASA Regulations CS-25.1529 and CS-25 Appendix H, which in turn mirror the FAA regulation 14 CFR 25.1529.
RRA-00 Page 1
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
1. General A. This publication was prepared on behalf of 365 Aerospace Ltd and is in accordance with Air Transport Association of America
Specification No. 100, Specification for Manufacturers Technical Data. The data contained within is related to certain changes/modifications/alterations that are in addition to the associated airplane’s type design.
NOTE: THIS MANUAL IS PREPARED SPECIFICALLY TO COVER THE AIRPLANE(S) LISTED IN THE "INTRODUCTION"
SECTION, FOR THE OWNER/OPERATOR NAMED ON THE TITLE PAGE.
THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.
B. The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM and
WDM. Therefore, this publication is a SUPPLEMENT to the associated AMM and WDM, and instructions on how to use this manual are equivalent to the instructions on how to use the manufacturers AMM and WDM.
C. This Manual Supplement has been raised to give historic design information pertaining to the following related aircraft
manuals:
WDM – Wiring Diagram Manual AMM – Aircraft Maintenance Manual
D. For information on the approval of the technical content of this document, please refer to the Change/Mod/Alteration listing E. Aircraft Effectivity Information:
MODEL/ TYPE
CUST EFFECT CODE
CUST EFFECT CODE
(IPC ONLY)
VARIABLE ENGR
NUMBER
ENGINE SET
NUMBER LINE
NUMBER
MFG SERIAL
NUMBER REGISTRY NUMBER
CUST ASSIGNED AIRPLANE
IDENT
737-4Z9 PW701 PB899 2043 25147 OE-IAB PW701
INTRO-00 Page 1 Jan 09/17
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
2. Change/Modification/Alteration Listing
A. DOA Mod/STC information – Table 2.1
Mod/STC Ref: Title:
MOD-0228 EFIS pin programming change to TNT standard
B. Owner/Operator/Supplier Mod/STC Information – Table 2.2
Mod/STC Ref: Title: Supplier:
3. Approval
A. With reference to any Mod/STC indicated in Table 2.1 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of DOA No. EASA.21J.575. B. With reference to any Mod/STC indicated in Table 2.2 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of the named Owner/Operator/Supplier of the document. The Owner/Operator/Supplier of the document has given the compiler of this supplement rights to use their information in order to produce this manual supplement.
C. The Checking process will include a verification of technical consistency with the associated Mod/STC and Compliance
documentation which may relate to effectivity, description, effects on airworthiness and environmental protection especially when limitations are changed or affected.
Checked: Print Name: Olivier Poelmans
Approved: Print Name:
INTRO-00 Page 2 Jan 09/17
neilcTypewritten TextNeil Chettleburgh
WIRING
DIAGRAM
MANUAL
Contents
WDM-CONTENTS Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
34-22-11 –EFIS POWER/PROGRAM PINS – LEFT
34-22-21 –EFIS POWER/PROGRAM PINS – RIGHT
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
WDM-CONTENTS Page 2
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
WDM-LEP Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
WDM Front Page WDM Contents 1 WDM Contents 2 WDM-List of Effective Pages 1 Chapter 34 Front Page 34-22-11 1 Jan 09/17 34-22-21 1 Jan 09/17
CHAPTER
34 NAVIGATION
B737-300/400/500 WIRING DIAGRAM MANUAL SUPPLEMENT
MSN25147/PW701
EFIS POWER/PROGRAM PINS - LEFT
34-22-11 INCORPORATES:
34-22-11 365 AEROSPACE MOD 0228 Page 1 Page 1
JAN 09/17 JAN 09/17
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B737-300/400/500 WIRING DIAGRAM MANUAL SUPPLEMENT
MSN25147/PW701
EFIS POWER/PROGRAM PINS - RIGHT
34-22-21 INCORPORATES:
34-22-21 365 AEROSPACE MOD 0228 Page 1 Page 1
JAN 09/17 JAN 09/17
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
AIRCRAFT
MAINTENANCE
MANUAL
Contents
AMM-CONTENTS Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
34-22-00 – Electronic Flight Instrument System
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
AMM-CONTENTS Page 2
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
AMM-LEP Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
AMM Front Page AMM Contents 1 AMM Contents 2 AMM-List of Effective Pages 1 Chapter 34 Front Page 34-22-00 501 JAN 09/17
CHAPTER
34 NAVIGATION
B737-300/400/500 AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT
EFFECTIVITY
34-42-03 PW701 post MOD-0228
Page 501
Jan 09/17
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
GROUND PROXIMITY WARNING SYSTEM – ADJUSTMENT TEST
1. General
A. The 365 Aerospace modification MOD-0228 changes the EFIS pin programming to the TNT standard. It installs wiring at the Captain's and First Officer's EFIS control Panels to change the display setting from 'Track UP' to 'Heading Up' and it changes the pin programming of the Left and Right EFIS Symbol Generators in order to set below options: - Improve the airspeed trend indication - Display '1 CH' on the EADI to indicate single channel autopilot operation - Display a white 'ALT' height alert on the EADI at 2500 ft upon descent to selected altitude - Display analog 'RUNWAY' tied to localizer bar at 200 ft and below - Display full 360° compass rose - Display blinking 'PITCH' and 'ROLL' attitude comparator message - Display a range ring if the range is less than 160 NM and TCAS is activated
B. The operational test must be carried out in accordance with Boeing AMM 34-22-00.
Below tables provide the correct test results after incorporation of MOD-0228. 2. EFIS – Operational Test
G. EFIS Display Modes Test
Table 501 EFIS hex code lines
OE-IAB/PW701/25147 FA351B0 86BE008 E180000
Front PackageWiring Diagram Manual (WDM)Chapter 34 - NavigationWDM 34-22-11WDM 34-22-21Aircraft Maintenance Manual (AMM)Chapter 34 - NavigationAMM 34-22-00 pageblock 501
2017-01-16T10:52:15+0100Olivier Poelmans
2017-01-16T16:32:22+0000Neil Chettleburgh