BY ORDER OF THE COMMANDER AIR FORCE...

BY ORDER OF THE COMMANDER

HOLLOMAN AIR FORCE BASE

AIR FORCE INSTRUCTION 21-101

HOLLOMAN AIR FORCE BASE

Supplement

18 NOVEMBER 2013

Maintenance

AIRCRAFT AND EQUIPMENT

MAINTENANCE MANAGEMENT

COMPLIANCE WITH THIS PUBLICATION IS MANDATORY

ACCESSIBILITY: Publications and forms are available for downloading or ordering on the e-

Publishing website at www.e-Publishing.af.mil.

RELEASABILITY: There are no releasability restrictions on this publication.

OPR: 49 MXG/MXQ

Supersedes: AFI21-

101_HOLLOMANAFBSUP,

9 January 2012

Certified by: 49 MXG/CC

(Colonel André L. Kennedy)

Pages: 48

This instruction implements the information and requirements set forth in AFI 21-101,

Aircraft and Equipment Maintenance Management, 26 July 2010, AFI 21-101 AFGM3, 24

September 2012, and AFI 21-101 Combat Air Forces (CAF) Supplement dated 11 July

2012. This instruction applies to all unit personnel assigned, attached, and tenant to the 49th

Maintenance Group (49 MXG). Ensure that all records created as a result of processes

prescribed in this publication are maintained in accordance with Air Force Manual 33-363,

Management of Records, and disposed of in accordance with Air Force Records Information

Management System (AFRIMS) Records Disposition Schedule (RDS) located at

https://www.my.af.mil/afrims/afrims/afrims/rims.cfm. Contact supporting records managers

as required. Refer recommended changes and questions to the Office of Primary Responsibility

(OPR) using AF Form 847, Recommendation for Change of Publication, to 49th Maintenance

Group Quality Assurance Office (49 MXG/MXQ), 1210 Forty Niner Ave, Holloman AFB, NM

88330.

SUMMARY OF CHANGES

This document is substantially revised and must be completely reviewed. Major changes

include: This supplement was drafted using Guidance Memorandum 3 (GM3) dated 24

September 2012. We assessed our publication for non-value added language, areas that

previously limited the ability for maintenance leaders to make field level decisions, and for

http://www.e-publishing.af.mil./

https://www.my.af.mil/afrims/afrims/afrims/rims.cfm

2 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013

irrelevant and unrealistic expectations with limited resources. Many deletions stem from

duplication between the parent AFI and other governing directives. These deletions may not

have changed previous requirements but only removed the duplication between directives. All

references to Air Force Global Strike Command aircraft and resources removed. Changed

verbiage as required to clarify responsibilities and renumbered paragraphs to better flow with the

parent publication. The supplement has significant changes from the previous version.

Table 6.1. (Added) Priorities in Effect. ................................................................................... 7

Table 7.1. (Added) Numbers assigned to controlling agencies. ............................................. 10

Table 14.1. Mandatory Special Certification Roster (SCR) and Prerequisites. ........................ 28

Attachment 1—GLOSSARY OF REFERENCES AND SUPPORTING INFORMATION 33

Attachment 15—(Added) IMIS WORK CENTER MNEMONIC CREATION REQUEST

LETTER 36

Attachment 16—(Added) IMDS WORKCENTER MNEMONIC DELETION REQUEST

LETTER 37

Attachment 17—(Added) MEMORANDUM FOR IMDS DATABASE MANAGER 38

Attachment 18—(Added) DATA INTEGRITY APPOINTMENT LETTER 39

Attachment 19—(Added) FLIGHT WWID 40

Attachment 20—(Added) M1 SUPPORT SERVICES 42

Attachment 21—(Added) LOCAL RADIO CALL SIGNS 43

Attachment 22—(Added) PRIVACY ACT STATEMENT 48

AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 3

1.4.1. All requests for maintenance assistance will be coordinated through and be

approved by the 49th Maintenance Group Commander (49 MXG/CC) or designatee prior

to being submitted.

2.8.1. (Added) Double hearing protection is defined as a combination of ear plugs and

ear muffs.‖ Single hearing protection will be worn when; within 100 feet of an MQ-1 with

the engine operating, within 150 feet of an MQ-9 with the engine operating, within 25

feet of AGE being operated outside of a hangar or inside hangars 301 or 500, and inside a

closed hangar adjacent to a hangar with a F-22 operating at idle. Double hearing

protection will be worn when; within 200 feet of any taxiing or operating jet engine

aircraft, within 100 feet of any operating APU, PAO cart, or A/M 32A-60 or -95 turbine

generator/compressor, and AGE is being operated inside a hangar. Hearing protection is

not required for Magnum MLC 4064 Light Carts (i.e.: LC##).

2.8.2. (Added) Personnel are authorized to have food and drink in the flightline area as

long as they are; contained in a closable container, not brought into or consumed in a

hangar conducting LO, paint and/or corrosion control operations, and not brought into or

consumed in areas exposed to toxic materials, chemicals or industrial shop contaminants.

To protect containers from contamination, they will not be allowed on or under aircraft,

on test equipment, near hazardous chemicals, etc. In the West Canyon aircraft hangars,

containers will be stored on the work table at the hangar entrance. If food and/or drink

will be consumed in the hangar, it will be consumed in the immediate vicinity of the

work table. "Camelback" type wearable fluid containers are authorized provided the tube

mouthpiece has a cover.

3.2.2. Refer to Holloman Air Force Base Instruction (HAFBI) 21-38, Tool/Equipment

Control and Accountability Program, for specific guidance on tool control for wing

agencies.

3.2.6. Refer to HAFBI 21-119, Crashed, Damaged or Disabled Aircraft Recovery

(CDDAR) Program, for specific CDDAR responsibilities.

3.4.1.6. Refer to LJG 49MXG-007, Emergency Action Checklist Procedures, for

specific guidance on adverse weather procedures.

3.4.1.25. Refer to ACCI 21-105_HOLLOMANAFBSUP, Fabrication Program, for

specific guidance on corrosion prevention and control.

3.4.1.29. HAFBI 21-119 outlines specific responsibilities and details resource and

training requirements for the CDDAR team.

3.4.1.31. The Maintenance Operations Center (MOC) has been designated as the

OPR for the 49 MXG LMR program.

3.4.1.66. Refer to HAFBI 21-38 for guidance on tool/equipment control for other

than 49 MXG agencies.

3.4.1.69. Transient Alert responsibilities are contracted by M1 Support Services for

Holloman AFB. All roles and responsibilities are outlined in the Contractor’s

operating instructions.


3.4.1.73. Emergency actions for the 49 MXG are outlined in LJG 49MXG-007.

3.4.1.76. External Fuel Tank Procedures:

3.4.1.76.1. (Added) The owning Aircraft Maintenance Unit is responsible for

storage, general care, scheduling for inspection or repair and shipment for

operational use or turn-in. External fuel tanks are accounted for with the AMU

SPRAM account.

3.4.1.76.2. (Added) The MXS Fuel Systems Repair Section performs

maintenance actions as described in section 5.5.4. of AFI 21-101 CAFSUP.

3.4.1.76.3. (Added) Required fuel tank inspections or TCTOs will be scheduled

through the PS&D weekly scheduling meeting.

3.4.1.76.4. (Added) The owning AMU will remove and replace fuel disconnect

and recheck external tank prior to contacting the MXS Production Supervisor. If

external tank anomaly is still present contact PRO SUPER to dispatch Fuel

Systems personnel for inspection and troubleshooting prior to downloading tank.

3.4.1.76.5. (Added) The owning AMU will defuel, drain and ensure fuel and air

standpipes are capped prior to delivering the tank to the fuel barn for repair or

scheduled inspection. The AMU will attach a completed AFTO Form 350,

Reparable Item Processing Tag, and an IMDS screen 122 (snapshot) to the tank.

AMU personnel will coordinate with Fuel Systems personnel or MXS Production

Supervisor to ensure the tank is accepted upon delivery to prevent any delays in

maintenance.

3.4.1.76.6. (Added) Fuel Systems personnel will notify MXS Production

Supervisor when tank maintenance is complete to coordinate pick-up of tank by

owning AMU.

3.4.1.76.7. (Added) The designated tank storage area is the tank farm on the

west side of the south canyon between buildings 816 and 818. The tank farm is

maintained by AMU personnel.

3.4.1.77. Emergency power outage procedures are outlined in LJG 49MXG-007.

3.9.42. (Added) Appoint Dash 21 equipment custodians (primary and alternate) in

writing.

3.10.27. Dash 21 program.

3.10.27.1. (Added) AMUs will:

3.10.27.1.1. (Added) Ensure all equipment identified as Dash 21 is marked

legibly with aircraft tail number or Composite Tool Kit (CTK) EID number to

which they are installed, bags used to contain smaller items will be marked in the

same manner. All Dash 21 will have “Remove Before Flight” streamers attached

(only one streamer is required for items connected by lanyard). If Dash 21 is

transferred from another aircraft, completely remove previous marking.

3.10.27.1.2. (Added) Enforce maintenance and control of all aircraft Dash 21

equipment.


3.10.27.1.3. (Added) Inspect Dash 21 for serviceability, and inventory every 30

days. The inspection may be documented in TAS or on a locally approved form.

Missing Dash 21 will be treated as a lost object and lost tool/object procedures

will be followed. All removed/broken items will be documented on Dash 21

inventory sheet.

3.10.27.1.4. (Added) Support Sections will:

3.10.27.1.4.1. (Added) Use AF Form 2691, Aircraft/Missile Equipment

Property Record, and/or AF Form 2692, Aircraft/Missile Equipment

Transfer/Shipping Listing, to account for and inventory all Dash 21

equipment.

3.10.27.1.4.2. (Added) Spare Dash 21 equipment maintained by support will

be inspected for serviceability and inventoried bi-annually.

3.10.27.1.5. (Added-AMS Section) Crew Chiefs are responsible for Dash 21

inventory upon aircraft movement.

3.10.27.2. (Added) All items listed on Dash 21 equipment inventory sheets will be

held to all Dash 21 accountability and inspection rules.

4.8.3. Dedicated Crew Chiefs not only consist of aircraft maintainers, but also

communication systems maintainers (AFSCs 3D1X2/3D1X3) dedicated to provide

continuity/accuracy of GCS forms, GCS status, scheduled maintenance, and improve

GCS cosmetics.

5.7.4.7.1. (Added) The Armament shop will have a minimum of 72 hours to

perform 18-month gun inspections and return the same gun to the AMU. The

forward supply point (FSP) gun will be available for issue to the AMU for

scheduled (serviceable) gun removals when the Armament shop cannot meet the

72-hour deadline, or the original gun becomes unserviceable due to AWM/AWP

status. If the FSP gun is not available, then the Special Purpose Recoverable for

Authorized Maintenance (SPRAM) gun may be issued instead. Any FSP or

SPRAM gun transaction will be coordinated through the MXS Production

Supervisor.

5.7.4.7.2. (Added) The SPRAM gun will be available for issue to FTD for

training use. The SPRAM gun will also be available for issue to the AMU for

unscheduled gun removal due to an unserviceable or unknown condition, unless

aircraft downtime will allow the Armament shop to return the original gun. If the

SPRAM gun is unserviceable or is being utilized by FTD, then the FSP gun may

be issued instead. Any FSP or SPRAM gun transaction will be coordinated

through the MXS Production Supervisor.

5.7.5.1.1. (Added) AMU Weapons Sections will account for AME on a locally

developed AF Form 2434, Munitions Configuration and Expenditure Document,

or locally developed line run document when not installed on aircraft.

5.7.5.1.2. (Added) Armament Flight will track assigned AME on a locally-

developed AME tracking log on the Armament Flight SharePoint.

5.7.5.1.3. (Added-HAFB) All equipment items due scheduled maintenance will


be turned in to Armament Flight on Thursday prior to the week the inspection is

due.

5.7.5.1.4. (Added) Hung munitions suspension equipment turn-in procedures:

5.7.5.1.4.1. (Added) Malfunctioning equipment will be turned in to

Armament Flight as soon as the AMU completes initial troubleshooting.

5.7.5.1.4.2. (Added) A properly documented hung munition worksheet and

IMDS screen 122 will accompany item being turned in.

5.7.5.1.5. (Added) The AMU will not perform the End of Firing (EOF) Day

inspection on any item being turned in for a hung munition or no release.

Armament Flight will complete the EOF inspection once troubleshooting is

complete.

5.7.5.4.1. (Added) Issue and receipt of in-use AME to the AMU will be

documented on the AME Tracking Log located on the Armament Flight

SharePoint. In the event of SharePoint being offline, AF Form 1297, Temporary

Issue Receipt, will be used. Equipment will be issued and received by Armament

Flight clean, free of foreign objects, properly tagged, and properly configured

with all safing devices installed.

6.2.2.9.2. (Added) 49 MXG/CC, or designated representative, will approve

engine runs above idle during quiet hours (2230 to 0600 or up to 2 hours after last

land) on a case-by-case basis. Not applicable to hush house runs. EXCEPTION:

(RPA) Engine runs above idle are permitted during quiet hours.

6.2.3.19.2.3. 49th Logistics Readiness Squadron (49 LRS) Surface Freight

section will notify the Base Engine Manager (BEM), 49th Maintenance

Operation Squadron (49 MOS) upon receipt of all engines and shipping

devices marked for FJ4801 account. 49 MOS will coordinate with 49 LRS

prior to delivery of any aircraft engines to Building 311 for off-base

shipments.

6.2.3.19.2.3.1. (Added) Non-Rolling Stock. The 49 LRS will be

responsible for the intra-base transportation of all aircraft engines not

mounted on trailers. The 49 MOS BEM will coordinate with 49 LRS for

transportation of engines, shipping devices, and related equipment marked

for the FJ4801 account.

6.2.3.19.2.3.2. (Added) 49th Maintenance Squadron (49 MXS), 49th

Aircraft Maintenance Squadron (49 AMXS), 849 AMXS, or applicable

contracted unit engine monitors will notify 49 MOS BEM when engines,

engine trailers, and engine shipping devices require shipment documentation

and transportation coordination.

6.2.3.19.2.3.3. (Added) The Consolidated Aircraft Maintenance (CAM)

contractor engine monitors will input current engine status by 1300 daily,

using CEMS direct line reporting.

6.2.3.19.2.3.4. (Added) Status reporting for applicable contractors. The

CAM contractor shall provide a daily engine status report by 0800hrs to 49


MOS/MXOOE via telefax or email. The report shall convey current posture

of all uninstalled engines. This report will contain the following

information: authorized spare engine level; total uninstalled engines by

type, model, series, and modification (TMSM); total sum of serviceable

engines; total engines obligated to aircraft; net on hand; engines in-work;

engines awaiting maintenance; and engines not mission-capable supply

(ENMCS). Engines that are placed into awaiting maintenance, in-work, or

ENMCS status shall be identified by serial number listing their status,

discrepancy, transaction/condition code, location (including off station),

estimated time of completion for in-work status, and specific work stoppage

pacing items for ENMCS status.

6.2.6.10. All requests for the addition or deletion of work center mnemonic codes

must be accomplished on an IMDS work center Mnemonic Creation/Deletion

Request Letter (Attachment 15, IMDS Work Center Mnemonic Creation Request

Letter, Attachment 16, IMDS Work Center Mnemonic Deletion Request Letter).

Letter will be sent to the Maintenance Management Analysis (MMA) Database

Management function that will coordinate with Programs and Resources Flight and

update IMDS database.

6.2.6.16.2. 49 MOS/MXOOA (Maintenance Analysis) will coordinate all long

recovery actions with mainframe personnel, as required. In this process, all

transactions since the last system saved to the moment of system failure are

recovered from the Audit Trail Tape (ATT). Should the automated recovery fail,

the following priorities are in effect when IMDS comes back on-line:

Table 6.1. (Added) Priorities in Effect.

Priority 1 Aircraft Status (IAW AFI 21-103, Equipment

Inventory, Status and Utilization Reporting) and

input of open discrepancies

MOC

Priority 2 Aircraft sorties and flying hours Debrief

Priority 3 All scheduled maintenance actions PS&D

Priority 4 All input and deferred discrepancies that are

awaiting parts (AWP)

Support section

Priority 5 All remaining closed discrepancies. Workcenters are responsible

for their shop inputs.

6.2.6.16.3. All users will complete a DD Form 2875, System Authorization

Access Request (SAAR), and submit it to the MMA DBM section in order to be

issued an IMDS password. Completed DD Form 2875 will be maintained on file

in the MMA DBM section. In order to get a Reliability and Maintainability

Information System (REMIS) password, each user will be required to complete a

REMIS user access request letter. MMA DBM section will forward the

completed REMIS access letter to the appropriate MAJCOM. Prior to separation,

retirement, PCS, or PCA, users will be required to out process through the DBM

section in order to have access to IMDS/REMIS deleted.

6.2.6.16.6. Each Squadron within the MXG and each Flight/Section as deemed


appropriate by Flight Chiefs within the MXG will appoint a primary and alternate

Data Integrity Team (DIT) monitor as part of the MXG DIT. Appointed monitors

will receive training from the 49 MOS/MXOOA DIT Section.

6.2.6.16.6.4. Appointed DIT monitors will utilize AutoDIT, a Microsoft

Access application, to review and verify IMDS documentation accuracy.

6.2.6.16.6.5. Error corrections will be made by the appropriate maintenance

workcenter, validated by the Squadron’s DIT monitor, and forwarded to 49

MOS/MXOOA DIT Section within 3 calendar days.

7.1.4.1. (Added) PS&D will host and schedule Pre-dock and Post-dock meetings.

7.1.4.2. (Added) As a minimum, the following will attend the Pre-dock and Post-

dock meeting: MOF PS&D, Dedicated/Assistant Crew Chief (with the aircraft

forms), Phase Inspection Dock Chief, AMU Production Super, MXS Production

Super, LO ASM, NDI, and EME. Additionally, QA will attend all Post-dock

meetings to assist with configuration management.

7.1.4.3. (Added) Pre-dock meetings will be held for all all Programmed

Maintenance Packages (PMP) and Contract Field Teams (CFT) NLT 10 duty days

prior to the scheduled induction date. Post-docks will be held after completion of the

PMP/CFT. At this time, MQ-1 and MQ-9 aircraft do not have a Phase Inspection

requirement.

7.1.4.4. (Added) MOF PS&D will prepare an AF Form 2410, Inspection/TCTO

Planning Checklist, listing all items to be accomplished during the inspection. Items

to be accomplished will be discussed and agreed upon. For configuration

management, MOF PS&D will request IMDS screen 942, Actual Configuration Set-

up from DBM. Once accomplished, the scheduler must run an IMDS screen 990.

This must be given to the PMP Dock Chief for verification/correction of all items out

of configuration. The Dock Chief will ensure items out of configuration are verified,

corrected in IMIS/IMDS using appropriate JDD screens, and annotated on the 990.

After agreeing to the items in the work package, attendees will sign the AF Form

2410 in the appropriate block. A copy of the AF Form 2410 is given to the PMP

Dock Chief and the original is maintained by MOF PS&D.

7.1.4.5. (Added) MOF PS&D will ensure the following:

7.1.4.5.1. (Added) Coordinate with the EM scheduler on any engine related time

changes, inspections and TO's required and ensure they are annotated on the AF

Form 2410.

7.1.4.5.2. (Added) Perform a complete document review on the aircraft.

7.1.4.5.3. (Added) Prior to the Post-dock records review, the dock chief defers

all discrepancies in IMDS that were identified but not corrected, verifies

completion of all inspection requirements and transcribes open discrepancies to

the appropriate AFTO Form 781's. Verified configuration data is updated and

corrected in IMDS.

7.1.4.5.4. (Added) At the Post-dock meeting, a representative from the AMU

PS&D, the dedicated crew chief or assistant, the Dock Chief, and the AMU


Production Superintendent review the completed PMP or CFT package and check

for proper documentation. This review will ensure all work cards are signed off

and all items annotated on the AF Form 2410 are complete. AMU PS&D will

print the PMP/CFT package and all added maintenance work orders showing the

jobs completed.

7.1.4.5.5. (Added) The Dock Chief will give the corrected 990 to AMU PS&D.

Items not verified and specific reasons why the verification was not conducted

will be discussed and annotated on the AF Form 2410. AMU PS&D will forward

the Post-dock 990 to MOF PS&D no later than one duty day after the Post-dock

meeting. MOF PS&D will request IMDS screen 942 from DBM for the same tail

number. Completed/verified copies of the output product will be maintained in

MOF PS&D in the aircraft jacket file until the next scheduled PMP inspection for

that aircraft.

7.1.4.5.6. (Added) A Post-dock records review will be completed no later than

the day of the Post-dock meeting.

7.1.8. 49 MOS/MXOOA DBM will follow LJG 49 MXG-002 F-22 IMDS-Emergency

Aircraft Incident Procedures and Checklist and LJG 49 MXG-003 RPA IMDS-

Emergency Aircraft Incident Procedures and Checklist.

7.1.12.1. (Added) Table 7.1. Shows blocks of numbers assigned to controlling

agencies identified.Listed agencies are responsible for controlling, recording, and

tracking manual JCNs as well as input of JDD data when IMDS returns on-line.


Table 7.1. (Added) Numbers assigned to controlling agencies.

Non-Assignable JCNs for Integrated

Maintenance Data System (IMDS)

0000-1449

F-22

Plans & Scheduling 9400-9499 Engine Management 9800-9819

Avionics 9500-9519 NDI 9820-9839

Crew Chiefs 9520-9539 Structural Maintenance 9840-9859

Weapons 9540-9559 Propulsion 9860-9879

AGE 9560-9579 Fuels 9880-9899

COSO 9580-9599 LO 9900-9919

Production 9600-9719 Egress 9920-9939

Debrief 9720-9739 Wheel & Tire 9940-9959

Corrosion 9740-9759 Crash Recovery 9960-9979

QA 9760-9779 Armament 9980-9999

Life Support / AFE 9780-9799 F-22 IMIS 2000-8999

MQ-1 MQ-9

RPA ASM 9000-9029 RPA ASM 1800-1819

Avionics 9030-9059 Avionics 1820-1839

Crew Chiefs 9060-9089 Crew Chiefs 1840-1859

Weapons 9090-9119 Weapons 1860-1879

AGE 9120-9149 AGE 1880-1899

COSO 9150-9179 COSO 1900-1919

Production 9180-9209 Production 1920-1939

Debrief 9210-9239 Debrief 1940-1959

COMM 9240-9269 COMM 1960-1979

QA 9270-9299 QA 1980-1999

P&S 9300-9399 P&S 1450-1499

7.2.1.3.1. Aircraft Document Reviews (ADR) will be completed utilizing the

developed and published local checklist designed for each MDS. ADRs will be

completed at deployed location using checklist if MOF PS&D is present at

deployed location. CAM Contractor ADRs will be completed IAW the

contractor’s operating instructions.

7.2.11.1.5.1. GCS pulled 781-series forms will be maintained in the 849

ACMU COMM Section Flight Office. A pulled set of 781-series forms are

defined as the forms that were closed out and removed from the binder. These

inactive sets may or may not include an AFTO Form 781J/K and will not be

filed separately.

7.10.7. (Added) Work centers are responsible for creating each Job Standard (JST)

package/IMIS maintenance template, as required. QA/QAE will review each

JST/maintenance template for technical accuracy; decide if it meets criteria for a

QA/QAE managed JST/maintenance template. When approved, Wing Plans, Scheduling,

and Documentation (PS&D) will input JST/maintenance template into Maintenance

Information Systems (MIS). Any changes to a JST/maintenance template will first be


routed through the QA/QAE office; once changes are approved, they will be input into

MIS by MOF PS&D. To prevent duplicate discrepancies in aircraft forms, individuals

may delete only WCEs in JST/maintenance template, which are already open, entered

into MIS, or are not applicable to current maintenance function.

7.10.15. (Added) Reference Holloman AFB Instruction (HAFBI) 11-101, Squadron

Programming/Airspace/Range Scheduling, for guidance on sortie and flying hour

reconciliation.

8.10.14. PEs will be tracked in IMDS by course code 30002 and in the QA database.

8.14.6. TO Change Notification. The following procedures will be used for all F-22

Technical Order Data (TOD) updates/changes:

8.14.6.1. (Added) Typical, Full and Partial TOD updates/changes:

8.14.6.1.1. (Added) Initial Notification of TOD updates/changes.

8.14.6.1.1.1. (Added) Upon initial notification from the IMIS Integrated

Product Team (IPT), IMIS Administrators will notify the 49th Maintenance

Group (49 MXG) TODO via email (49 MXG/MXQ TOD Change Notification

email distribution box) that an IMIS TOD update/change is being released.

8.14.6.1.1.2. (Added) If available, IMIS Administrators will forward a

summary of TOD updates/changes to 49 MXG TODO at this time.

8.14.6.1.1.2.1. (Added) 49 MXG TODO will include the summary of TOD

updates/changes in the weekly schedule.

8.14.6.1.1.3. (Added) Once notification is received from Fort Worth Data

Management that TOD updates/changes are available on the Contractor

Support Field Database (CSFDB), IMIS Administrators will notify the 49

MXG TODO that updates/changes are available for download to local servers.

8.14.6.1.1.4. (Added) 49 MXG TODO will contact IMIS Administrators

(IMIS HAFB email distribution box) with approval to download TOD

updates/changes to local servers.

8.14.6.1.2. (Added) TOD Update/Change Implementation.

8.14.6.1.2.1. (Added) IMIS Administrators will download TOD

updates/changes to local servers within 24 hours of 49 MXG TODO approval.

IMIS Administrators will notify 49 MXG TODO once local servers have been

updated.

8.14.6.1.2.2. (Added) 49 MXG TODO will notify 49 MXG personnel and 49

MXG TODA managers that TOD updates/changes are available on local

servers. 49 MXG QA will brief the 49 MXG/CC at the next scheduled

maintenance meeting that TOD updates/changes have been made available.

8.14.6.1.2.3. (Added) TODA managers will update all Portable Maintenance

Aid (PMA) hard drives within 5 work days of notification.

8.14.6.1.2.4. (Added) TODA managers will inform 49 MXG TODO of any

issues encountered during the update process.


8.14.6.1.2.5. (Added) 49 MXG TODO will consult with IMIS

Administrators on all reported issues.

8.14.6.2. (Added) Non-typical Full and Partial TOD updates/changes:

8.14.6.2.1. (Added) These types of TOD updates/changes require the direct

assistance of IMIS Administrators.

8.14.6.2.2. (Added) Initial Notification of TOD updates/changes.

8.14.6.2.2.1. (Added) Upon initial notification from the IMIS IPT, IMIS

Administrators will notify 49 MXG TODO that an IMIS TOD update/change

is being released. NOTE: IMIS Administrators will inform 49 MXG TODO

that upcoming TOD updates/changes will require special processing to

complete.

8.14.6.2.2.2. (Added) If available, IMIS Administrators will forward a

summary of TOD updates/changes to 49 MXG TODO at this time.

8.14.6.2.2.2.1. (Added) 49 MXG TODO will include the summary of TOD

updates/changes in the weekly schedule.

8.14.6.2.2.3. (Added) Once notification is received from Fort Worth Data

Management that TOD updates/changes are available on the CSFDB, IMIS

Administrators will notify the 49 MXG TODO that updates/changes are

available for download to local servers.

8.14.6.2.2.4. (Added) 49 MXG TODO will contact IMIS Administrators via

email with approval to download TOD updates/changes to local servers.

8.14.6.2.3. (Added) TOD Update/Change Implementation:

8.14.6.2.3.1. (Added) IMIS Administrators will download TOD

updates/changes to local servers within 24 hours of 49 MXG TODO approval.

IMIS Administrators will notify 49 MXG TODO once local servers have been

updated.

8.14.6.2.3.2. (Added) 49 MXG TODO will notify 49 MXG personnel and 49

MXG Technical Order Distribution Accounts (TODA) managers that TOD

updates/changes are available on local servers. 49 MXG QA will brief the 49

MXG Commander at the next scheduled maintenance meeting that TOD

updates/changes have been made available.

8.14.6.2.3.3. (Added) Aircraft Maintenance Unit (AMU)/Back shop TODA

managers will coordinate with IMIS Administrators as to when

PMA/Workstation hard drives will be turned in for update.

8.14.6.2.3.3.1. (Added) PMA/Workstation hard drives will be updated

within 5 workdays of notification.

8.14.6.2.3.4. (Added) IMIS Administrators will inform AMUs/Back shop

TODA managers and 49 MXG TODO of estimated completion time and

coordinate return of all PMA hard drives.


8.16.1.1. In addition to established directives, the following responsibilities and

procedures will apply to all Operational Check Flights (OCF):

8.16.1.1.1. (Added) Appropriate AMU will coordinate all OCFs with flying

squadron commander or operations officer. Final approval authority for OCFs

rests with flying squadron commander. 49 MXG/CC/CD and 49 OG/CC/CD will

be notified.

8.16.1.1.1.1. (Added) As soon as it is determined an OCF is required, the

AMU/ squadron will coordinate with QA/QC for the type aircraft. QA/QC or

a squadron FCF pilot will determine required in-flight checks necessary to test

system for which aircraft is being OCF’d.

8.16.1.1.1.2. (Added) The flying squadron will designate a pilot and a

takeoff time. OCFs will be flown either single ship or in conjunction with a

training mission.

8.16.1.1.1.3. (Added) QA/QC will review aircraft forms of any aircraft

designated for an OCF no later than one hour prior to takeoff time.

8.16.1.1.1.4. (Added) Upon approval of mission, pilot, and takeoff time by

49 OG/CC, aircraft forms will be released to aircraft location for final review

prior to flight.

8.16.1.1.1.5. (Added) QA/QC or squadron FCF pilot will provide preflight

assistance upon request of OCF pilot on reason for OCF and the system

checks required. In cases of ground aborts, QA/QC will be notified of all

discrepancies by maintenance debrief section.

8.16.1.1.1.6. (Added) Aircraft operations will be accomplished IAW

applicable aircraft -1 T.O. procedures.

8.16.1.1.1.7. (Added) Upon completion of OCF, pilot will debrief with

appropriate AMU debrief section. QA/QC will be present to document all

discrepancies in OCF logbook.

8.16.3.5. Holloman FCF pilots may be made available to FCF transient aircraft.

Before this can occur, the owning organization’s OG/CC, 49 OG/CC and 49

MXG/CC must mutually agree on the flight. 49 OG/CC is the final authority for all

FCF flights of transient aircraft. The FCF pilot/crew must be current and qualified in

the transient aircraft.

8.16.3.5.1. (Added) If a transient FCF pilot is used for a FCF of a transient

aircraft, FCF personnel will be made available to brief transient FCF pilot on local

area procedures, restrictions, and intended route of flight. 49 OG/CC must

approve all FCF flights of transient aircraft by transient aircrew. Local FCF pilot

will assist in booking airspace and filing local flight plan. Local FCF pilot will

notify mission control (CHEROKEE) and Command Post. Command Post will,

in turn, notify 49 MXG/CC and 49 OG/CC.

8.16.5. 49 OG/CC has final approval authority regarding any modifications to FCF

profiles recommended by 49 MXG/CC.


8.16.5.1.1. All FCFs profiles will be flown in daylight, Visual Meteorological

Conditions (VMC). Pilot will begin profile in VMC and ensure that aircraft is

operating properly before penetrating overcast or undercast to Visual Flight Rules

(VFR) on Top. Overcast or undercast conditions may be penetrated to ―VFR on

Top conditions only if all primary and standby attitude references and

flight/navigation instruments are operational. Instrument Meteorological

Conditions (IMC) will not be entered unless aircraft is fully capable of flight

under Instrument Flight Rules (IFR) and pilot has determined sufficient VMC in

airspace, to include a clearly discernable horizon, is available to perform required

checks. Minimum weather for takeoff and landing will be 3,000 foot ceiling with

5 miles visibility.

8.16.6. If aircraft is released from FCF, document the aircraft forms IAW TO 00-20-1 by

entering FCF Released at (time aircraft released from FCF) in the corrective action block

and sign inspected by block.

8.16.6.2. Ground aborts of FCF aircraft results in automatic cancellation of 49

OG/CC approval of FCF flight.

8.16.8. (Added) Local Home Station Procedures.

8.16.8.1. (Added) FCF pilot will ensure that an entry is made on HAFB Form 36,

Local Flight Clearance – Flight Orders, or squadron equivalent Local Flight

Clearance Order for each scheduled FCF. In addition, FCF crew must certify that

their Bold Face and Flight Crew Information File (BF/FCIF) are current and on file at

their respective squadron.

8.16.8.2. (Added) Prior to each FCF, the FCF pilot will ensure Command Post is

notified. Command Post, will in turn, notify 49 MXG/CC and confirm 49 OG/CC

approval to the requester.

8.16.8.3. (Added) Prior coordination with mission control (CHEROKEE) or Radar

Approach Control (RAPCON) will be made for all FCFs prior to pilot departing for

the aircraft. This coordination will include, but not be limited to, airspace availability

or restrictions and altitude or airspeed restrictions.

8.16.8.4. (Added) Notify Life Support of any special requirements.

8.16.8.4.1. (Added) T-38s will have Life Support configure aircraft for dual or

solo. Off-station jets require use of dummy seat kits and detachable Personal

Survival Kit (PSK).

8.16.8.5. (Added) 49 WG FCF call sign will be ―BREAK XX.

8.16.8.6. (Added) Procedures to enter test areas will be IAW HAFBI 11-250,

Airfield Operations Instruction, and the Albuquerque Air Route Traffic Control

Center (ARTCC) Letters of Agreement.

8.16.8.7. (Added) Upon completion of an FCF or a ground abort, the FCF pilot will

debrief at appropriate AMU debrief section. QA/QC will be present at the respective

debrief to annotate discrepancies from FCF.


8.16.8.8. (Added) T-38 FCFs will be scheduled IAW the CAM contractor operating

instructions, FCF Scheduling, Coordination, and Documentation.

8.16.8.9. (Added) For F-22s the 49 OG/CC must specifically approve shutdown of

an engine in-flight. For any such F-22 flight, FCF pilot will have practiced ENGINE

AIRSTART procedures in simulator within preceding 30 days.

8.18. High Speed Taxi Checks. Coordinate all High Speed Taxi Checks with the QA FCF

monitor. The QA FCF monitor will initiate the High Speed Taxi Aircrew Briefing Checklist

prior to aircraft engine start to ensure that all requirements are met.

8.19.1.5. In the event an aircraft is deployed and a weight and moment verification is

required, adhere to following procedures. TDY QA inspector or OIC/NCOIC will

telephonically relay weight and moment verification requirements to the home station

W&B manager. After verification has been completed, and center of gravity is

determined to be within limits, the discrepancy may be cleared.

9.2. Specific Guidance. Aircraft Impoundments. The impound authority for the CAM

contractor has been delegated IAW the CAM contract, the contractor’s operating

instructions, and Impoundment Program. Impoundment authority, in conjunction with QA,

will determine need to freeze aircraft MIS records in event of an aircraft impoundment.

10.2.1.1. Support sections/tool rooms will strictly control engine blade blending blue

dye. Blue dye is to be used only for blade blending and marking exhaust nozzle

erosion. Authorized individuals must be appropriately trained and remain current.

10.2.1.1.1. (Added) To mark damaged lines and structural components,

qualified personnel will use green dye to identify damage within limits.

10.2.1.5. AMU/MXS Supervision will approve all on-site turnovers. Use the CAF

Form 140, CTK Inventory and Control Log, for CTKs and/or AF Form 1297, for

equipment items to record on-site turnovers. The CAM contractor turnover

procedures are located in contractor operating instructions, Composite Tool Kit and

Lost Object Programs. Test equipment and Warning Tags connected to aircraft may

be transferred at job site using these procedures.

10.2.1.9. Maintain positive control of clean, dirty, and total rag count at the

beginning and end of each shift by documenting accountability on an inventory sheet.

10.2.1.9.1. Maintain strict accountability of absorbent pads, canopy cloth, or

equivalent when technicians require any of these items for maintenance. When

needed, these items will be signed out by quantity to technicians using TAS.

10.2.1.9.3. (Added) Hangar Spill Kits.

10.2.1.9.3.1. (Added) Spill Kits will have an inventory of contents attached

to the exterior of kit.

10.2.1.9.3.2. (Added) When Spill Kits contain a full inventory; the kit will

be sealed with a tamper-evident seal.

10.2.1.9.3.3. (Added) If a Spill Kit is opened, but contents are not removed,

an inventory will be performed and the kit resealed with a tamper-evident

seal.


10.2.1.9.3.4. (Added) If a Spill Kit is opened and contents are used, a one-

for-one swap will be done at the respective support section to return the kit to

a full inventory and the kit will be resealed with a tamper-evident seal.

10.2.1.10. Only personnel authorized a Government Purchase Card (GPC) will be

allowed to procure tools. Requests for the purchase of large quantities of

tools/equipment will be approved by the flight/section chiefs and the request will be

routed to the squadron Resource Advisor for coordination.

10.2.1.10.1. (Added) All requests to procure new tools will be routed through

the Support Section/Tool Room NCOIC and approved by applicable flight

supervision.

10.2.1.12. Depot teams, factory representatives, and contract field teams performing

maintenance at HAFB will meet intent of HQ ACC and unit-established tool control

outlined in AFI 21-101, CAF Supplement and this supplement when working on

aircraft, GCS or equipment within the MXG. Tools will be signed out from

applicable support section in TAS or on an AF Form 1297. If the contractor or team

does not have any provisions for tool control or accountability, the team

leader/supervisor will coordinate with MXG/QA to develop a program. The

guidelines developed will be put on memorandum of agreement that is signed by

MXG/CC and the team leader/supervisor. QA and the team will maintain a copy of

this letter for the duration of the stay. Lost tool procedures will be followed if an item

is lost. QA may also periodically monitor compliance.

10.2.1.12.1. (Added) Depot teams, contract field teams (CFT), and factory

representatives, who work on equipment within a unit, will provide a copy of their

CTK equipment contents listing to the unit’s support section. These depot teams,

or contract field teams, and factory representatives will inventory toolboxes at the

beginning and end of each shift.

10.2.1.13. If two or more workcenters elect to operate a single tool room/support

section, they will designate one person from either work center as the NCOIC. The

NCOIC will assume overall responsibility for proper management of all tools,

equipment, and CTKs assigned to the tool room. If tools/equipment are distributed

from any support section/tool room (consolidated or not) to a decentralized location,

the NCOIC of the support section/tool room remains accountable for the proper

management of those tools/equipment. At least quarterly, the NCOIC or designated

support section personnel will visit the decentralized location to inventory/inspect the

tools/equipment and compare the master documentation, maintained in the support

section, to that with the tools/equipment.

10.2.1.14. CDDAR equipment is treated as a CTK.

10.2.1.15. Sign-in/out in TAS or on CAF Form 140 will not be signed by same

individual. Individuals working weekend duty will have an on-duty supervisor in-

check the CTK. If needed, have a supervisor from another section or squadron

annotate the sign-in block.

10.2.1.16. Access to a tool room will be governed by the unescorted entry letter.


10.3.6. A MIL will be complete and accurate by listing items in the CTK, the location of

the items, and total number of all items in each drawer, section, and within the CTK.

10.3.6.3. Consumable hand tools, HAZMATs, and other items contained in

Composite Tool Kits (CTKs) will be identified on MIL and be replaced by means of a

one for one swap. Only support section personnel are authorized to replace

consumables and only when the empty container or roll is returned. Consumables

that are not feasible to mark (petrolatum, grease, and all other items too small to be

etched) will be placed in a suitable container that can be marked. Keep consumables

placed into CTKs to the minimum required to perform the job.

10.4.3.4. Refer to paragraph 8.14.6. of this supplement for the roles and

responsibilities of the Lead TODO regarding F-22 Integrated Maintenance

Information System (IMIS) Technical Order Data (TOD) updates.

10.4.3.5. E-Tool ADPE Account Monitor shall provide Lead TODO with a copy of

E-Tool ADPE inventory after completion of annual inventory and whenever primary

monitor changes. A copy of ADPE Monitor appointment letter must accompany

inventory.

10.8.1.5. Upon QA notification, a report number will be issued by QA for CAF Form

145, Lost Tool/Object Report. Enter report number on upper left hand corner of the

CAF Form 145. QA assigned number will be: unit, year, and month, followed by

sequence number—for example: 49 AMXS050430. If the lost tool/item directly

involves an aircraft and the tool/item is not found, a copy of the completed CAF Form

145 will be delivered to P&S to be filed in the aircraft jacket file.

11.19.5. (Added) Procedures for Local Manufacture of Tools/Equipment:

11.19.5.1. (Added) Requesting unit will contact 49 MXG Quality Assurance (QA)

when the need for locally manufactured tools or equipment arises.

11.19.5.2. (Added) Unit will refer to AFI 21-101 paragraph 8.3.9. (AFI 21-101

paragraph 10.6. for Munitions/Armament tools/equipment) to ensure that the request

meets the criteria for a locally manufactured tool/equipment.

11.19.5.3. (Added) Once criteria is met, unit will complete Special Tool Approval

request letter obtained from QA. Unit will ensure that all documentation (drawings,

pictures, item description, etc.) accompanies the request letter.

11.19.5.3.1. (Added) Request letter and documentation will be routed through

all affected agencies and QA for approval.

11.19.5.3.2. (Added) The 49 MXG/CC is the final approval authority on all

local manufacture requests.

11.19.5.4. (Added) Fabrication Flight Local Manufacture Procedures:

11.19.5.4.1. (Added) Steps for AMU/PMP Supply Repair Shop Customer:

Ensure the item requiring Local Manufacture is source-coded JBD (SMR code of

MF--), local manufacture, and cannot be ordered through normal supply channels.

Print and sign AF Form 2005, Local Manufacture Worksheet. Use an AF Form

601, Equipment Action Request, for equipment requests. This lets the Fabrication


Flight Local Manufacture Manager know that items have been checked and

routed through AMU/PMP Supply personnel.

11.19.5.4.2. (Added) If an item required is not source-coded JBD, procurable,

(SMR code of PA---) and is needed immediately for MICAP requirement, the

item will immediately be placed on order to prevent recurring manufacture of

procurable assets. The supply document number associated with this order will

be required when processing the local manufacture. Gather all pertinent technical

data, drawings, samples and supporting documents, and contact the Fabrication

Flight Chief to determine if the part can be locally manufactured. If it can be

manufactured, all data will be brought to the manufacturing facility for evaluation

and corrections. Obtain drawings from the base EDSC or Joint Engineering Data

Management Information and Control System (JEDMICS).

11.19.5.4.3. (Added) Coordinate with appropriate fabrication element to

determine bits and pieces required to manufacture item. Fabrication Flight Local

Manufacture Supply Manager (LMSM) assists in verifying parts availability and

orders bits and pieces.

11.19.5.4.4. (Added) Take all items to Fabrication Flight LMSM.

11.19.5.4.5. (Added) Steps for Fabrication Flight LMSM:

11.19.5.4.5.1. (Added) Receive sample or dimensional drawing, AFTO

Form 350, maintenance snapshot inquiry print-out (IMDS Screen 122), and

completed SJAFB/MXMF/OCT 2002 Local Manufacture Worksheet.

11.19.5.4.5.2. (Added) Verify item is coded as local manufacture (JBD/SMR

code of MF---) and non-procurable through normal supply channels.

11.19.5.4.5.3. (Added) Document transaction on Local Manufacture Daily

Status Sheet.

11.19.5.4.5.4. (Added) Log job control number in database once assets are

completed and picked up by customer.

11.19.5.4.5.5. (Added) Requesters identify all sections that have action on

the AFTO Form 350 for items requiring multiple section processing.

11.19.5.4.6. (Added) Steps for fabricating activity:

11.19.5.4.6.1. (Added) After an item is manufactured, contact the requester

for a fit check, if required.

11.19.5.4.6.2. (Added) After correct adjustments are made, fabricating

activity will call requester for pick up and notify LMSM of job completion.

11.19.5.4.6.3. (Added) Requester will contact Fabrication Flight LMSM for

all status inquiries (AMU/PMP Supply will be the single point of contact for

all LM drop offs and pickups).

11.19.5.4.6.4. (Added) Fabrication Flight LMSM hours will be from 0700-

2400 Monday through Friday. After hours, weekends, and holidays

AMU/PMP Supply will order bits and pieces of all LM requests and route


them directly to manufacturing activity (Fabrication Flight Maintenance).

Fabrication Flight Aircraft Structural Maintenance will ensure local

manufacture process integrity during non-availability of LMSM. In the

absence of the LMSM, the 49 MXS Production Super will be the approving

authority.

12.1.15.1. Location Limits. IPL and safing operations will be conducted in

designated parking areas and hangars.

12.1.15.1.1. (Added) Emergency Precautions. If at any time during IPL or

safing operation an unserviceable condition, safety of flight, or a weapons

malfunction is discovered, all individuals in the immediate area will be advised.

12.1.15.1.2. (Added) Impoundment procedures for hung or multiple release of

ordnance and gun system malfunction.

12.1.15.1.2.1. (Added) The Weapons Section Chief will ensure a qualified 7-

level 2W1 is assigned as lead technician for troubleshooting the aircraft in

question.

12.1.15.1.2.2. (Added) Every attempt will be made to duplicate the

malfunction prior to removing any components from the aircraft. The

Weapons Section will consult the applicable AFETS representative as needed

to assist in isolating the malfunction.

12.1.15.1.2.3. (Added) If the cause of a hung munition, delayed or multiple

release, gun malfunction, or system damage cannot be determined, the aircraft

will be impounded.

12.1.15.1.2.4. (Added) If the hung munition, delayed or multiple release, or

gun malfunction is cause for an aircraft to be impounded and further

troubleshooting can pinpoint the cause to originates from a faulty bomb rack,

missile launcher, or gun system, the owning AMU and QA will clear the

aircraft impoundment and QA will issue new impoundment paperwork for the

affected bomb rack, missile launcher, or gun system.

12.1.15.1.3. (Added) Designated Live Munitions Load Areas. The only areas

sited for live munitions loading operations are Echo Ramp (6 spots), Arm/De-arm

Echo (4 spots), German Air Force (GAF) Live Load Pad (6 spots), Runway 07/25

(18 spots), West Area Hangars 13-20 (8 spots), and North Ramp CAPA (52

spots). Specific requirements and restrictions for each area are as follow:

12.1.15.1.4. (Added) Echo Ramp:

12.1.15.1.4.1. (Added) Sited for HD 1.1 munitions not to exceed 1,500 lbs

NEW per spot. Additional authorizations include: HD 1.2.1 - 269 <60 lbs,

HD 1.2.2 - 1,000 lbs, HD 1.2.3 - (04) 1,000 <60 lbs, HD 1.3 - 1,000 lbs, and

HD 1.4 - 1,000 lbs.

12.1.15.1.4.2. (Added) Sited for six aircraft parking/loading spots. Spots are

marked and grounding points are available.

12.1.15.1.5. (Added) Arm/Dearm Echo:



NEW per spot. Additional authorizations include: HD 1.2.1 - 1,000 >450 lbs,

HD 1.2.2 - 1,000 lbs, HD 1.2.3 - (12) 1,000 <450 lbs, HD 1.3 - 1,000 lbs, and

HD 1.4 - 1,000 lbs.

12.1.15.1.5. 2 . (Added) Sited for four aircraft parking/loading spots. Sited

spots are marked with painted white boxes with numbers 1 thru 4 and do not

correspond with the aircraft lead-in lines.

12.1.15.1.5.3. (Added) Use of these parking spots requires closure of Rwy

04/22.

12.1.15.1.6. (Added) GAF Live Load Pad:


Net Explosive Weight (NEW) per spot. Additional authorizations include:

HD 1.2.1 - 1,000 >450 lbs, HD 1.2.2 - 1,500 lbs, HD 1.2.3 - (12) 1,500 <450

lbs, HD 1.3 - 1,500 lbs, and HD 1.4 - 1,500 lbs.

12.1.15.1.6.2. (Added) Sited for six aircraft parking/loading spots. Spots are


12.1.15.1.6.3. (Added) Loading operations will not be conducted if aircraft

are present on the Rwy 07/25 Live Load Area.

12.1.15.1.6.4. (Added) Coordination with 49th Wing Plans (49 WG/XP)

GAF liaison is required to schedule parking of aircraft at this location.

12.1.15.1.7. (Added) Runway 07/25:


Net Explosive Weight (NEW) per spot.

12.1.15.1.7.2. (Added) Sited for 18 aircraft parking/loading spots. Spots are


12.1.15.1.7.3. (Added) The runway will be closed during all loading

operations.

12.1.15.1.7.4. (Added) Loading operations will not be conducted if aircraft

are present on the GAF Live Load Pad.

12.1.15.1.8. (Added) West Area Spot 13 – 20:

12.1.15.1.8.1. (Added) Sited for HD 1.1 munitions not to exceed 84 lbs Net

Explosive Weight (NEW) per spot. This is equivalent to a load of four AIM-

120 and two AIM-9 missiles. Additional authorizations include: HD 1.2.1 -

974 <99lbs, HD 1.2.2 - 1,000 lbs, HD 1.2.3 - (06) 1,500 <109lbs, HD 1.3 -

1,000 lbs, and HD 1.4 - 1,000 lbs.

12.1.15.1.8.2. (Added) Parking loaded aircraft in front of each sited spot to

facilitate maintenance and launch in the event of an APU exhaust system

malfunction is authorized.

12.1.15.1.9. (Added) North Ramp CAPA:


12.1.15.1.9.1. (Added) The North Ramp CAPA is sited primarily to support

DOT&E and WESP operations. Each spot is sited for 20 lbs NEW of HD

1.2.2, 1,000 lbs of HD 1.3 and capacity of HD 1.4. Loading of missiles or

rockets with live motors and inert warheads /telemetry packages is authorized.

12.1.15.1.9.2. (Added) Sited for 56 aircraft parking/loading spots. Spots are


12.1.15.1.9.3. (Added) One aircraft parking spot must be skipped between

aircraft if loading external HD 1.3 munitions on row E in order to maintain the

required separation distance between aircraft. This restriction does not apply

to internal countermeasure flares.

12.1.15.1.9.4. (Added) Two aircraft parking spots must be skipped if loading

external HD 1.2.2 munitions on row E. One aircraft parking spot must be

skipped between aircraft when loading external HD 1.2.2 munitions on all

other rows. This is to maintain the required separation distance between

aircraft. This restriction does not apply to HD 1.2.2 internal gun ammunition.

12.1.15.1.9.5. (Added) Forward firing munitions may not be loaded on row

A or row C.

12.1.15.1.10. (Added) Daily loading and unloading of training munitions:

12.1.15.1.10.1. (Added) Loading and unloading of aircraft gun ammunition,

defensive flares, and HD 1.4 munitions (i.e. chaff squibs, captive carry

training munitions, BDU-33s, etc.) in aircraft hangars 1 through 44 on the

west ramp is authorized. At no time will these munitions be loaded, unloaded,

or stored in Hangars 830, 867, 868, 877, or 898.

12.1.15.1.10.2. (Added) Loading and unloading of aircraft gun ammunition,

defensive flares, and HD 1.4 munitions (i.e. chaff squibs, captive carry

training munitions, BDU-33s, etc.) on any main ramp parking location is

authorized. At no time will these munitions be loaded, unloaded, or stored in

the RPA LAMS, Hanger 301, or Hangar 500.

12.1.15.1.10.3. (Added) RPA aircraft loaded with MAU-169D/B or older

model Computer Control Groups (CCG) that contain HD 1.4 explosives may

be sheltered in the RPA LAMS, Hangar 301, or Hangar 500 during Phase 1

wind conditions or greater provided all safety devices are installed and

approval has been obtained from the 49 MXG/CC, 49 MXG/CD, or Wing

Weapons Manager.

12.1.15.1.10.4. (Added) Inert training munitions completely free of all

explosive components may be loaded, downloaded, or stored in the RPA

clamshells, Hangar 301, or Hangar 500 as required to support daily flying or

load training operations.

12.1.15.2. Hung Ordnance: Refer to local checklist LJG 49MXG-021.

12.1.15.2.1. (Added) In the event of confirmed or suspected hung forward firing

ordnance or malfunctioning gun system, the aircraft will request to land runway

22 primary or 25 alternate, stop on the departure end of the runway, and position


the aircraft facing West (270-290 degrees magnetic). The ground crew will verify

the aircraft is properly positioned prior to performing any safing operations on

forward firing munitions. Upon notification, SFS will secure the appropriate

area(s) IAW SFS Quick Reaction Checklist 3, In-Flight Emergency. Emergency

response vehicles will be in place at Arm/De-arm Golf, and will respond to the

aircraft. If the munitions cannot be safed, the aircraft will be shut down and EOD

will be notified. Downloaded munitions that cannot be immediately loaded on

trailers and removed will be positioned and monitored so as not to obstruct

aircraft taxi or other operations.

12.2.2.27. (Added) Bomb straps will be used during all bomb loading/unloading and

transporting procedures to and from the aircraft/trailer at WLT and on the flightline.

12.2.2.28. (Added-MQ-9) the ADU-537 A/E table will be used during all bomb

loading operations to provide adequate clearance between the aircraft’s landing gear

and the loading truck arms.

12.6.1.1. (Added) The RPA load training facility will be a designated spot in

hanger(s) 301 and/or 500.

12.17. Transient Aircraft Responsibilities. Control and storage of impulse carts removed

from transient aircraft:

12.17.1. (Added) Impulse carts removed from transient aircraft may be stored at/in 49

MXG Munitions Storage Area/Facility, provided the following criteria are met:

12.17.1.1. (Added) Impulse carts will be placed in a separate cart can and

segregated within the cart locker from all other impulse carts.

12.17.1.2. (Added) The can containing the impulse carts removed from transient

aircraft will be clearly marked with the type and quantity of impulse carts and the

type aircraft and tail number the carts were removed from.

14.8.12. (Added) Authorize Cannibalization (CANN) action within squadron resources

and coordinate with MXS superintendent and the jet engine intermediate maintenance

(JEIM) section chief for an engine to aircraft CANN action. Notify the AMU Supply

Section when the decision to CANN is made.

14.10. Crash Damaged or Disabled Aircraft Recovery (CDDAR) Program. Holloman-

specific CDDAR requirements are contained in HAFBI 21-119.

14.13.10. (Added) MOC will:

14.13.10.1. (Added) Immediately transmit all information received from tower SOF

to EOR supervisor via radio, or phone.

14.13.10.2. (Added) Relay all AMU AF Form 2407, Weekly/Daily Flying Schedule

Coordination.

14.13.11. (Added) AMUs will:

14.13.11.1. (Added) Forward any changes to the Weekly Maintenance and Flying

Schedule to MOC and 49 MOS/MXOOA/MXOOP, by AF Form 2407.

14.14. (Added) (RPA) Also includes propeller blending.


14.14.2. (RPA) The same requirements will apply to propeller blend inspections and

repairs.

14.14.3. (RPA) The same requirements will apply to propellers.

14.14.7.1.1. (Added-RPA) AFETS will be certifying officials.

14.14.8. (RPA) The same requirements will apply to propellers.

14.14.8.1. (RPA) The same requirements will apply to propellers.

14.14.8.2. (RPA) Fill out applicable propeller Log with the following information:

blade number, station and employee number of maintenance personnel.

14.14.8.4. (Added) Ensure all installed engine blade/propeller blends are loaded

against the engine/propeller and not the aircraft.

14.15.1. The CAM Contractor engine run certification program will be conducted IAW

contractor’s operating instruction.

14.15.2.5.1. (Added) RPA’s do not require a break rider.

14.15.2.9. (Added-RPA) Maintenance personnel qualified through on-the-job

training (OJT) may motor engines as long as the ignition kill switch is in cold

position.

14.15.5.3. (F-22A) Students will accomplish a minimum of one engine run at

maximum power setting. If a maximum power setting run is not possible at the time

of certifying, students will be certified up to an 80% power setting. When resources

become available for a maximum power setting run, students will be certified to that

power setting.

14.19.2.3. Prime aircraft and spare aircraft inlet covers/plugs can be removed one

hour prior to scheduled aircrew arrival. Spare/Aborted aircraft will have the inlet

covers/plugs and pitot tube covers reinstalled after the scheduled aircraft are airborne.

Inlet covers/plugs will be installed during non-emergency towing operations.

14.19.2.6. Wear of stocking cap (Navy watch) is authorized IAW AFI 36-

2903_HAFBSUP 1, Dress & Personal Appearance of AF Personnel. Cap must be

removed around operating engine danger zones.

14.19.2.6.4. (Added) CAM contractor maintenance personnel may wear baseball

hats year round in the T-38 flightline areas IAW contractor’s operating

instruction.

14.19.2.9. Structural maintenance and rivet replacement in areas where loose objects

could have FOD potential will be supervised and inspected by an individual

possessing a 7-level in the required specialty. Flights will train newly assigned

technicians on engine intake maintenance procedures.

14.19.2.9.1. See Attachment 21 for local checklist.

14.19.2.11. Procedures for FOD walks are as follows:

14.19.2.11.1. (Added) If the unit’s area of responsibility contains a FOD

receptacle, the unit is required to physically inspect the receptacles on a daily


basis, empty as necessary and will never be overflowing.

14.19.2.11.2. (Added) 49 MOS MTF is responsible for the flight line side of

Building 823 out to the red line.

14.19.2.11.3. (Added) Crash Recovery & PMP flights are responsible for

flightline side of Bldg. 877 North out to the red restricted area line.

14.19.2.11.4. (Added) The 7 AMU will FOD walk from the flightline side of

Bldg. 868 out to the red restricted area line and the north end of the aircraft

parking/shelter area inside the red restricted area lines in and around hangars 1-12

and 25-36. The 7 AMU will FOD walk from the flightline side of Bldg. 868 out

to the red restricted area line from the north end of the aircraft parking/shelter area

inside the red restricted area lines to the south end of the ramp in and around

hangars 1-24 and 25-44.

14.19.2.11.5. (Added) The 49 MXS will be responsible for the following areas:

14.19.2.11.5.1. (Added) Propulsion Flight is responsible for flightline side of

Bldgs. 800, 816, and 817 out to the red restricted area line.

14.19.2.11.5.2. (Added) AGE is responsible for the AGE ready line area

extending north to the flightline access road out to the red restricted area line

and the AGE maintenance facility.

14.19.2.11.5.3. (Added) Metals Technology is responsible for flightline side

of Bldg. 820 from access road to Bldg. 823 out to the red restricted area line,

to include the ECP next to the AGE yard.

14.19.2.11.5.4. (Added) Corrosion is responsible for the flightline side of

building 830 out to the red restricted area line up to the ECP on the northwest

end of the MXG area.

14.19.2.11.5.5. (Added) Accessories Flight is responsible for flightline side

of Bldgs. 866 and 868 North, bays 1 and 2, out to the red restricted area line.

Fuels is responsible for flightline side of Bldg. 868 North out to the red

restricted area line.

14.19.2.11.5.6. (Added) WLT is responsible for flightline side of Bldg. 868

South out to the red restricted area line.

14.19.2.11.5.7. (Added) Wheel & Tire and Armament flights are responsible

for flightline side of Bldg. 877 South out to the red restricted area line.

14.19.2.11.5.8. (Added) Fabrication Flight is responsible for flightline side

of Bldg. 898, starting at building 898’s hangar doors out to the red restricted

area line.

14.19.2.11.5.9. (Added) NDI is responsible for the flightline side of building

297 out 50ft and all the way to the red line in the GAF.

14.19.2.11.6. (Added) The 849 AMXS will FOD walk the areas surrounding

hangars 301 and 500. They are also responsible for the immediate area around

aircraft launching on the Main Ramp.


14.19.2.11.6.1. (Added) The 849ACMU will FOD walk the areas contained

within the enclosed GCS Compound.

14.19.2.11.7. (Added) T-38 flightline, FOD walks will be conducted at the

beginning of each shift. Morning FOD walk will begin prior to first aircraft taxi

of the day. Second FOD walk will normally be at the next shift change, but will

in any case be at the discretion of the Production Superintendent.

14.19.2.11.7.1. (Added) The T-38 section is responsible for the parking

apron directly behind buildings 577, 578, and the taxiway between this

parking apron and Alpha taxiway.

14.19.2.11.8. (Added) All personnel will ensure that their area of responsibility

remains free of FO throughout the duty day to prevent damage to aircraft engines

or tires.

14.19.2.11.9. (Added) EOR personnel will perform FOD walks prior to the

arrival of the first aircraft at EOR. Area inspection is the parking pad, 25 feet of

taxiway in both directions of parking pad, and road from FOD sign to the parking

pad.

14.19.2.11.10. (Added) Deployed units are responsible for the area of the ramp

they occupy and will follow the guidelines in paragraph 14.19.2.11.1. of this

supplement to ensure any potential FOD problems are alleviated prior to the

arrival of their aircraft. Advanced Echelon (ADVON) units will do a FOD walk

of the area where their aircraft will be parked prior to the arrival of the deployed

aircraft.

14.19.2.16. All aircraft safety pins and Dash 21 equipment will have a ―Remove

Before Flight‖ streamer (minimum four inches) attached directly to the head assembly

to prevent a FOD incident.

14.19.2.16.1. (Added) All other maintenance equipment that uses some type of

quick release pins, locking device pins, covers, etc., will be secured to that

particular piece of equipment by the use of steel cable and swedges.

14.19.2.17.1. (Added) If a flashlight is assigned to the vehicle the flashlight will

be marked with the vehicle identification number and annotated on the AF Form

1800, Operator’s Inspection Guide and Trouble Report (General Purpose

Vehicles).

14.19.2.17.2. (Added) Unit Vehicle Control Officer/Vehicle Control NCO

VCOs/VCNCOs will brief supervisors and vehicle operators on prevention and

control of FOD. This briefing will be established by VCO/VCNCO and will

periodically spot check assigned vehicles to ensure operators are complying with

intent of the FOD prevention program. It is the responsibility of the vehicle

operator to ensure vehicle is free of debris and cleanliness is maintained.

14.19.2.25. (Added) All vehicle key chain contents, i.e. gas key, identification tag or

any additional items attached, will be marked with the vehicle registration number (if

possible) and total number of keys will be annotated in TAS and/or AF Form 1800,


blocks 13-19. If any of these items are ever noted missing, it will be treated as a lost

tool/object.

14.19.4.7. Each AMU/MXS Flight will appoint a primary and alternate FOD

representative. Deployable FOD program is addressed in HAFBI 21-37, Foreign

Object Debris/Damage Aircraft Recovery (CDDAR) Program. The CAM contractor

will use procedures set in the contractor’s operating instruction, Foreign Object

Damage Control, and Prevention Program.

14.19.4.8. (Added) FOD bulletin boards should include the following:

14.19.4.8.1. (Added) Visual aid listings of names and phone numbers of the

49th Wing Vice Commander, 49th Wing FOD Manager, and also the contact

information for the Squadron/Flight FOD representative.

14.19.4.8.2. (Added) For CE sweeper support contact Airfield Operations at

572-5411. For CE sweeper support contact Airfield Operations at 572-5411.

14.19.4.8.3. (Added) Selected FOD incident reports, photographs, and other

material specifically designated may be displayed.

14.19.4.8.4. (Added) Current FOD meeting minutes should be available for

review by all unit members.

14.22.1. Hangar queen management principles and actions will be applied to RPA

Ground Crew Stations. This will include definitions, management actions and local

status briefings in paragraphs 14.22.2. through 14.22.8.

14.30.1. Red Ball documentation procedures:

14.30.1.1. (Added) For F-22As, utilize Cap Code-5 reporting to document red ball

actions that do not lead to a Ground Abort in IMIS, which does not affect the landing

status code:

14.30.1.1.1. (Added) Debrief as normal until user gets to the Fault Reporting

Code (FRC) page. If there is no FRC that can be attributed to the red ball, create

an ADHOC FRC. Go to create JCNs and select the FRC for the red ball. The

symbol will be a diagonal, change the Cap Code to 5, change the When

Discovered Code to before flight, in the discrepancy block enter the discrepancy

followed by the word ―Red ball, and create the JCN. After the discrepancy has

been created print a copy of the FRC page, change the Cap Code-5 back to a

Code-1, complete the remainder of the debrief as normal, and annotate on the

FRC print out that the FRC/JCN is for the redball.

14.30.1.2. (Added) For RPA Red Balls:

14.30.1.2.1. (Added) Debrief a Red Ball action using the same procedures as in-

flight discrepancy documentation, utilizing Cap Code-5, which does not affect the

landing status code.

14.30.1.3. (Added) Upon completion of Red Ball maintenance, the individual who

completed the task will ensure all required documentation is entered and cleared from

the aircraft forms prior to aircraft flight.


14.30.1.3.1. (Added) If the Red Ball created a Red X discrepancy, the job must

be cleared from the forms IAW TO 00-20-1 prior to flight.

14.30.1.3.2. (Added) For F-22As, individuals will ensure that the documented

red ball maintenance reflects accurately in IMDS once the aircraft forms have

been docked and the maintenance actions have pushed from IMIS to IMDS.

14.30.1.3.3. (Added) For RPAs, individuals will make every effort to input and

clear IMDS prior to flight.

14.30.1.3.4. (Added) Red Ball documentation for deploying aircraft:

14.30.1.3.4.1. (Added) For F-22As, all Red Ball maintenance will be

documented on AFTO Form 781A’s in accordance with T.O. 00-20-1. Upon

arrival to the deployed or TDY location, annotate aircraft electronic forms

with maintenance actions accomplished during the deployment launch Red

Ball maintenance. Once information is transcribed, dispose of Red Ball 781

series forms IAW 00-20 series TOs, this instruction, AFMAN 33-363, AF

Records Disposition Schedule located at

https://www.my.af.mil/afrims/afrims/afrims/rims.cfm and applicable Dash-

6 TOs.

14.30.2. Red Ball Maintenance Procedures. Ensure Red Ball Checklists are readily

available and aircraft AFTO 781A/IMIS are documented in accordance with TO 00-20-1

for all maintenance performed.

14.30.5. (Added) Red Ball parts ordering and delivery will be handled by the

appropriate AMU Supply Section. Supply will check tail number bins (TNB) for parts on

hand.

14.30.5.1. (Added) If the required part is on hand in TNB, AMU Supply will ensure

that documentation is completed for the ―MARK FOR change.

14.30.5.2. (Added) If the part requires ordering, the Production Supervisor may

direct that the part be ordered and immediately picked up from supply, if available, or

an authorized CANN Authority may approve the item for CANN.

14.30.6. (Added) Ensure any follow-on actions related to operational checks are

accomplished prior to the aircraft flying its sortie. Pilot may perform the operational

checks in chocks. All follow-on operational checks will be documented in the aircraft

forms prior to flight.

14.30.7. (Added) During Red ball maintenance specialist/technician will collect all

parts removed to FOM. Place attaching hardware in parts bags and tie to the assembly.

Parts bags will have the aircraft tail number, content, quantity, panel number (or aircraft

component nomenclature) marked on each bag. Attach a completed AFTO Form 350

with blocks 1, 2, and 14 documented to all removed aircraft parts and turn parts in to the

AMU support section for proper storage in the tail number bin.

https://www.my.af.mil/afrims/afrims/afrims/rims.cfm


Table 14.1. Mandatory Special Certification Roster (SCR) and Prerequisites.

14.38.4.2.1. Transient Alert will:

14.38.4.2.1.1. (Added) Ensure oil sampling procedures compliance, IAW the

weapon systems applicable -6 technical order. (Ensure analysis requests are

immediately delivered to the supporting Oil Analysis Program (OAP) lab with

additional DD Form 2026, Oil Analysis Request. The additional form will be

held on file at the OAP lab.) Inform OAP lab personnel of projected aircraft

departure time. Transient alert oil analysis request will be given priority

based on this time.

14.38.4.2.2. (Added) Applicable AMUs and MXS will:

14.38.4.2.2.1. (Added) Obtain oil samples when one of the following

conditions occurs:

14.38.4.2.2.1.1. (Added) Within 30 minutes of engine shut down after first

flight engine shutdown of the day and prior to next sortie.

14.38.4.2.2.1.2. (Added) Sheared Power Take Off (PTO) shaft.

14.38.4.2.2.2. (Added) Ensure IMIS is utilized to assist in tracking engine

oil consumption data.

14.38.4.2.2.3. (Added) All owning organizations and sections requiring OAP

support will:

14.38.4.2.2.3.1. (Added) Notify OAP Lab of any oil servicing cart not

sampled that week and reason why (any oil cart not sampled for reasons

other than TDY will be placed on ―P code until sample is received and

results have been released by OAP Lab).

14.38.4.2.2.3.2. (Added) Each oil sample must be accompanied by DD

Form 2026 correctly filled out IAW T.O. 33-1-37-1, Joint Oil Analysis

Program Laboratory Manual, page 3-12, Para. 3-6b. The following

exception applies to oil servicing cart sample documentation only; place

―N/A in the following blocks:

14.38.4.2.2.3.2.1. (Added) End item model/hull number.

A B

ITEM Mandatory SCR Item Titles Prerequisites

46. (Added) Clear Repeat/Recur

Discrepancies

7-Level SSgt or Higher (or

civilian equivalent) (Note 2)

47. (Added) Clear Cannot Duplicate

(CND) Discrepancies

7-Level SSgt or Higher (or

civilian equivalent) (Note 2)

NOTES:

(Added) 4----Munitions inspectors who are trained and certified may annotate serviceability tags

for munitions items (TO 11A-1-10).

(Added) 5---Appointed by the Nuclear Weapons Related Material Accountable Officer

(NWRMAO).


14.38.4.2.2.3.2.2. (Added) Hours/miles since overhaul.

14.38.4.2.2.3.2.3. (Added) Hours/miles since oil change.

14.38.4.2.2.3.2.4. (Added) Oil added since last sample.

14.38.4.2.2.4. (Added) Oil servicing carts undergoing periodic maintenance

will have oil analysis verification prior to being placed back into routine

service.

14.38.4.5. 1 (Added) Aircraft engines with such discrepancies will be placed on a

―D code restricting them from operation/flight until discrepancies are corrected.

14.38.5.7. (Added) Ensure 3 special oil samples are taken during a 45-minute

ground run, at 15-minute intervals; the following consecutive sample will not be

tested until the results are known from the previous sample. These samples are

required subsequent to the following:

14.38.5.8. (Added) After oil-wetted area maintenance is performed.

14.38.5.9. (Added) After OAP lab recommends system drain and flush.

14.38.5.10. (Added) Ensure the OAP lab is notified of all engines removed from

service as a result of excessive or abnormal oil consumption.

14.38.5.11. (Added) Ensure installed/uninstalled engines undergoing test are not

removed from test bed until OAP sample results are known.

14.38.5.12. (Added) Ensure detailed maintenance feedback is provided to the OAP

Lab whenever maintenance is performed due to an OAP recommendation. Feedback

must be received within 1 duty day of maintenance completion upon submission of

sample. Aircraft sample results will not be released until completed maintenance

feedback is received.

14.38.6.5. (Added) Ensure the following personnel are immediately notified of any

aircraft/engine grounding or abort recommendations from OAP lab: Maintenance

Operation Officer/Superintendent, AMU OIC/NCOIC, Program/Division Manager,

Production Superintendent, and Propulsion Flight Chief.

14.38.6.6. (Added) Notify appropriate expediter immediately when a

recommendation code is anything other than code ―A‖ and post information on the

aircraft status display board. Aircraft requiring Red Cap/special oil samples will not

be released for flight until results are known and recommendations have been

forwarded to MOC or affected squadron maintenance supervision.

14.38.6.7. (Added) Ensure no aircraft engines are operated until the following DD

Form 2026 discrepancies are corrected and verified with the OAP Lab: equipment

and/or end item serial number error, hours since overhaul (EOT or EFH), oil change

error, and oil added since last sample error. These items are essential to oil analysis

trending and removes that engine from service until discrepancy is corrected. IAW

paragraph 14.38.5.5., aircraft engines with such discrepancies will be placed on ―D

code restricting them from operation/flight until discrepancies are corrected.


14.38.6.8. (Added) Coordinate all requested OAP support during non-duty hours by

notifying the OAP standby personnel.

14.38.7.9. (Added) Ensure administration of OAP.

14.38.7.10. (Added) Ensure a qualified oil analysis supervisor/evaluator is available

during flying window.

14.38.7.11. (Added) Ensure OAP lab supervisor monitors daily flying schedule for

oil sample requirements and reconciles deviations with applicable MOC.

14.38.7.12. (Added) Ensure any abnormal oil analysis trends are verified and the

findings/proper status codes are reported to the MOC.

14.38.7.13. (Added) Maintain a daily sample receipt log where all samples, from all

organizations, will be annotated.

14.38.7.14. (Added) Ensure abnormal OAP trends/results/proper status codes are

communicated to any transient aircraft s home station oil analysis laboratory and to

MOC.

14.38.7.15. (Added) Ensure qualified OAP evaluators are available on standby at all

times after normal duty hours.

14.38.7.16. (Added) Ensure all oil samples with DD Form 2026 documentation

errors are immediately reconciled with customer.

14.38.7.17. (Added) The Wing OAP will maintain paper copy oil analysis records

for MQ-9 aircraft engines processed by Honeywell. (OAP lab will not provide

recommendation codes and/or tracking of sampling.)

14.38.7.18. (Added) Conduct a briefing for all involved organizations when a JOAP

feedback form is initialized to ensure the procedures/maintenance recommendations

are understood.

14.38.10.1. OAP customers are responsible for obtaining complete oil analysis

records for their equipment from the losing laboratory and for delivery of the records

to the gaining laboratory at the new operating site.

14.38.10.3.1. (Added) Aircraft sample results will not be placed on a ―D code

and will not be released until all required paperwork is received.

14.38.10.6. (Added) Ensure oil sampling procedures compliance, IAW the weapon

systems applicable -6 technical order. (Ensure analysis requests are immediately

delivered to the supporting OAP lab with additional DD Form 2026. The additional

form will be held on file at the OAP lab.) Inform OAP lab personnel of projected

aircraft departure time. Transient alert oil analysis request will be given priority

based on this time.

14.38.11. (Added) Engine oil servicing carts OAP requirements:

14.38.11.1. (Added) Engine oil servicing cart oil samples are required on a weekly

basis. Samples will be taken from all 49 WG engine oil carts the first duty-day of

each week and delivered to the JOAP Lab prior to 1600.


14.38.11.2. (Added) If an oil servicing cart is in maintenance, storage, TDY, etc.,

AGE will report this to the JOAP Lab the first duty day of each week by 1600. In

addition, the OAP Lab will be notified of any oil servicing cart serial number

changes.

14.38.12. (Added) All Organizations requiring OAP will:

14.38.12.1. (Added) Appoint monitors for OAP. Appointment letters will include

grade, name, duty phone, AFSC, organization and office symbol.

14.38.12.2. (Added) Provide current letters of appointment. Letters shall be updated

annually or every time a new monitor is appointed. Personnel appointed will be

contacted should any consultation concerning the OAP be required.

14.38.12.3. (Added) Ensure appointed monitors receive proper Oil Analysis

Program training from NDI/JOAP Lab. Personnel taking oil samples must receive

training on oil analysis sampling procedure, IAW applicable technical data. Training

shall be documented in individual training records and Integrated Maintenance Data

System (IMIS).

14.38.12.4. (Added) Ensure each oil sample must be accompanied by DD Form

2026, correctly filled out IAW AFI 21-101_CAF_Holloman Sup, Para. 14.38.5.3.

DD Form 2026’s with the following documentation errors; End item model/hull

number, Hours/miles since overhaul, Hours/miles since oil change, Oil added since

last sample, will be placed on D code restricting them from operation/flight until

discrepancies are corrected.

14.38.12.5. (Added) OAP customers are responsible for obtaining complete oil

analysis records for their equipment from the losing laboratory and for delivery of the

records to the gaining laboratory at the new operating site.

14.38.12.6. (Added) Upon return, TDY/deployed oil analysis records will be

returned to the home station laboratory. Aircraft/Oil analysis records not returned

will not be placed on D code and will not be released until all required paperwork is

received.

14.38.12.7. (Added) Engine oil servicing cart oil samples are required on a weekly

basis. Samples will be taken from all 49 WG engine oil carts the first duty-day of

each week and delivered to the JOAP Lab prior to 1600.

14.38.12.8. (Added) If the oil servicing cart is in maintenance, storage, TDY, etc., it

will be reported to the JOAP Lab the first duty day of each week by 1600. In addition,

the OAP Lab will be notified of any oil servicing cart serial number changes.

14.38.12.9. (Added) Oil servicing carts undergoing periodic maintenance will

require an oil analysis sample prior to routine service release.

14.38.12.10. (Added) Notify the OAP lab of any oil servicing cart not sampled that

week and reason why (oil carts not sampled for reasons other than TDY will be

placed on ―P‖ code until sample is received and results have been released by OAP

Lab).


14.38.12.11. (Added) Ensure aircraft oil barrels (55 gal drums or other) that are to

be transferred to oil carts for the servicing of aircraft engines are sampled and results

are known prior to addition of the oil into the cart.

14.38.13. (Added) 7th AMU Debrief will:

14.38.13.1. (Added) Ensure oil analysis samples are entered into IMIS prior to

JOAP Laboratory receipt of sample.

14.38.13.2. (Added) Should aircraft data be delayed and/or an error occurs during

download; personnel will notify JOAP Laboratory and provide estimated time until it

can be rectified. Aircraft/Engines without proper IMIS documentation entries will be

placed on D code restricting them from operation/flight until discrepancies are

corrected.

ANDREW A. CROFT, Colonel, USAF

Commander, 49th Wing


Attachment 1

GLOSSARY OF REFERENCES AND SUPPORTING INFORMATION

References

ACCI 21-105_HOLLOMANAFBSUP, Fabrication Program, 17 January 2012

AFI 21-101, Aircraft and Equipment Maintenance Management, 26 July 2010

AFI 21-101 Combat Air Forces (CAF) Supplement, Aircraft and Equipment Maintenance

Management, 11 July 2012

AFI 21-103, Equipment Inventory, Status and Utilization Reporting, 26 January 2012

AFI 36-2903_HAFBSUP1, Dress & Personal Appearance of AF Personnel, 22 April 1999

AFMAN 33-363, Management of Records, 1 March 2008

HAFBI 11-101, Squadron Programming/Airspace/Range Scheduling, 15 March 1996

HAFBI 11-250, Airfield Operations Instruction, 10 August 2012

HAFBI 21-37, Foreign Object Debris/Damage Aircraft Recovery (CDDAR) Program, 15

February 2012

HAFBI 21-38, Tool/Equipment Control and Accountability Program, 15 February 2012

HAFBI 21-119, Crashed, Damaged or Disabled Aircraft Recovery (CDDAR) Program, 27 April

2010

T.O. 00-20-1, Aerospace Equipment Maintenance Inspection, Documentation, Policies, and

Procedures, 15 June 2011

Forms Prescribed.

Holloman AFB Form 36, Local Flight Clearance – Flight Orders, 1 December 1980

Adopted Forms.

AF Form 847, Recommendation for Change of Publication, 22 September 2009

AF Form 2005, Issue/Turn-In Request, 26 August 2008

DD Form 2026, Oil Analysis Request, March 1999

DD Form 2027, Oil Analysis Record, August 1976

AF Form 2407, Weekly/Daily Flying Schedule Coordination, 1 June 1972

AF Form 2434, Munitions Configuration and Expenditure Document, 1 December 1996

AF Form 2691, Aircraft/Missile Equipment Property Record, 1 May 1978

AF Form 2692, Aircraft/Missile Equipment Transfer/Shipping Listing, 1 May 1976

DD Form 2875, System Authorization Access Request (SAAR), August 2009

Abbreviations and Acronyms

49 AMXS—-49th Aircraft Maintenance Squadron


49 LRS—-49th Logistics Readiness Squadron

49 MOS—-49th Maintenance Operation Squadron

49 MOS/MXOOA—-49th Maintenance Operations Squadron Maintenance Analysis

49 MOS/MXOOE—-49th Maintenance Operations Squadron Engine Management

49 MOS/MXOOP—-49th Maintenance Operations Squadron Plans, Scheduling &

Documentation

49 MXS—-49th Maintenance Squadron

49 MXS/MXMP—-49th Maintenance Squadron Test Cell

49 MXG—-49th Maintenance Group

49 MXG/CC—-49th Maintenance Group Commander

49 MXG/CD—-49th Maintenance Group Deputy Commander

49 MXG/CEM—-49th Maintenance Group Chief Master Sergeant

49 MXG/MXQ—-49th Maintenance Group Quality Assurance Office

49 OSS/AFE—-49th Operations Support Squadron Aircrew Flight Equipment Section

49 WG/XP—-49th Wing Plans

849 AMXS— 849th Aircraft Maintenance Squadron

ADVON—-Advanced Echelon

AFFF—-Aqueous Film Forming Foam

AFRIMS—-Air Force Records Information Management System

AR—-Action Request

ATT—-Audit Trail Tape

BEM—-Base Engine Manager

BF/FCIF—-Bold Face and Flight Crew Information File

CAM—-Consolidated Aircraft Maintenance

CANN—-Cannibalization

CCG—-Computer Control Groups

CSFDB—-Contractor Support Field Database

EAC—-Emergency Action Checklist

EOF—-End of Firing Day

FRC—-Fault Reporting Code

FSP—-Forward Supply Point

GCS—-Ground Control Station

GDT—-Ground Data Terminal


HAFBI—-Holloman Air Force Base Instruction

IBD—-Inhabited Building Distance

IMC—-Instrument Meteorological Conditions

IPT—-Integrated Product Team

JEDMICS—-Joint Engineering Data Management Information and Control System

JOAP—-Joint Oil Analysis Program

LOASM—-Low Observable Aircraft Structural Maintenance

NWRMAO—-Nuclear Weapons Related Material Accountable Officer

OAP—- Oil Analysis Program

OML—-Outer Mold Line

PCA—-Permanent Change of Assignment

PCS—-Permanent Change of Station

PSK—-Personal Survival Kit

PTO—-Power Take Off

RAPCON—-Radar Approach Control

RDS—-Records Disposition Schedule

TA—-Transient Alert

TOD—-Technical Order Data

UGSR—-49 MXG Unit Ground Safety Representative

VFR—-Visual Flight Rules

VMC—-Visual Meteorological Conditions

WTR—-Workable TCTO Report


Attachment 15 (Added)

IMIS WORK CENTER MNEMONIC CREATION REQUEST LETTER

Figure A15.1. IMDS Work Center Mnemonic Creation Request Letter.



IMDS WORKCENTER MNEMONIC DELETION REQUEST LETTER

Figure A16.1. IMDS Work Center Mnemonic Deletion Request Letter.



MEMORANDUM FOR IMDS DATABASE MANAGER

Figure A17.1. Memorandum for IMDS Database Manager.



DATA INTEGRITY APPOINTMENT LETTER

Figure A18.1. Data Integrity Appointment Letter.



FLIGHT WWID

Table A19.1. 49th Maintenance Group WWID.

49th Maintenance

Group

Flight WWID

Quality Assurance HSXQ

Weapons

Standardization

HSXW

AFREP HSXG

QAE HSXE

Table A19.2. 49th Maintenance Squadron WWID.

49th Maintenance

Squadron

Flight WWID

AMMO

Munitions Line-

Delivery

HSSB

Munitions Inspection HSSI

Munitions Support

Equipment

Maintenance

HSSL

Conventional

Maintenance

HSSO

Munitions Storage HSSW

Munitions Plans/ HSSK

PGM HSSX

Deployment/Training

AGE

AGE 7/8th

AT/Mobility

HSSG

PMEL HSSD

Accessories

Egress HSSC

Fuels HSSF

Wheel & Tire HSST

Armament HSSR

Fabrication

F-22 Sheet Metal

/Structures /LO

HSSM

NDI HSSN

Metals Tech HSSA

RPA Sheet metal

Structures

HSSU

Props

Support & Test Cell HSSP


Table A19.3. 49th Aircraft Maintenance Squadron WWID.

49th Aircraft

Maintenance

Squadron

Flight WWID

7th AMU HSA7 & HSA8

Crash Recovery /

PMP

HSAC

Table A19.4. 49th Operations Group WWID.

49th Operations

Group

Flight WWID

7th Life Support HSO7

20th Life Support HSO2

49th OSS Life

Support

HSO4

OG Staff HSOG

Table A19.5. 372d Training Squadron WWID.

372d Training

Squadron

Flight WWID

DET 10 HSD0

Table A19.6. 49th Aircraft Maintenance Squadron WWID.

849th Aircraft

Maintenance

Squadron

Flight WWID

MQ-1 HSU1

MQ-9 HSU2



M1 SUPPORT SERVICES

Table A20.1. World Wide Identifier’s (WWID’s) And Equipment Identifier’s (EID’s)

WORKCENTER WWID CTK NO’S. EQUIPMENT

IDENTIFIER

(EID)/CTK

NUMBER’S

T38 ACFT MAINT

UNIT (MAAM)

HSCA A0100 – S9900 HSCAA0100 –

HSCAS9900

TRANSIENT ALERT

(MAAMT)

HSCA T0100 – T3000 HSCAT0100 –

HSCAT3000

QUALITY CONTROL

(MAQQC)

HSCA U0100 – U3000 HSCAU0100 –

HSCAU3000

AGE SHOP

(MAEAG)

HSCM A0100 – A3000 HSCMA0100 –

HSCMA3000

AVIONICS SHOP

(MAEAV)

HSCM A3100 – A6000 HSCMA3100 –

HSCMA6000

BATTERY SHOP

(MAEBT)

HSCM B0100 – B1000 HSCMB0100 –

HSCMB1000

ELECTRIC SHOP

(MAEEL)

HSCM B1100 – B3000 HSCMB1100 –

HSCMB3000

EGRESS SHOP

(MAEG)

HSCM C0100 – C3000 HSCMC0100 –

HSCMC3000

ENVIRONMENTAL

SHOP (MAEEV)

HSCM D0100 – D3000 HSCMD0100 –

HSCMD3000

ENGINE SHOP

(MAEGE)

HSCM E0100 – E9900 HSCME0100 –

HSCME9900

FUEL SHOP

(MAEJP)

HSCM F0100 – F3000 HSCMF0100 –

HSCMF3000

HYDRAULIC SHOP

(MAEHD)

HSCM H0100 – H3000 HSCMH0100 –

HSCMH3000

MACHINE SHOP

(MAEMS)

HSCM M0100 – M5000 HSCMM0100 –

HSCMM5000

PAINT SHOP/WASH

RACK (MAECC)

HSCM P0100 – P9900 HSCMP0100 –

HSCMP9900

SHEETMETAL SHOP

(MAESM)

HSCM S0100 – S5000 HSCMS0100 –

HSCMS5000

WELDING SHOP

(MAEWD)

HSCM W0100 – W5000 HSCMW0100 –

HSCMW5000

WHEEL & TIRE

SHOP

(MAEWT)

HSCM T1100 – T5000 HSCMT1100 –

HSCMT5000



LOCAL RADIO CALL SIGNS

Table A21.1. The 49th Wing.

CALL SIGN OPERATOR

MOC Maintenance Operation Center

Fighting 1 Wing Commander

Fighting 2 Vice Wing Commander

Fighting Chief Command Chief

Fighting 3 Operations Group (OG) Commander

Fighting 3 Alpha OG Deputy Commander

Fighting 3 Chief OG Chief

Fighting 5 MXG Commander

Fighting 5 Alpha MXG Deputy Commander

Fighting 5 Chief MXG Chief

MXG Super MXG Weekend duty OIC

MXG Super MXG after hours NCOIC/OIC

Fighting 10 Chief of Safety

Fighting 10 Alpha Chief of Flight Safety

Fighting Safety Safety Duty Officer

Mobile Command Post Disaster Control Group

QA Chief Quality Assurance (QA) Chief

QA 1 QA Chief Inspector

QA2-QA40 MXG Inspector

EOR End of Runway Inspection Team

WSS Weapons Standardization

Table A21.2. Fighter Operations.

Demon 1 7 FS Commander

Demon 2 7 FS DO

Raptor 1 49 OSS Commander

Demon Ops 7 FS Ops

Table A21.3. 49 AMXS.

AMXS 1 AMXS Commander

AMXS 2 AMXS MOO

AMXS Chief AMXS Chief

AMXS Super AMXS Production Supervisor

Demon Super 7 AMU Production Supervisor

Demon 3 7 APG Expeditor

Demon 4 7 APG Expeditor

Demon 5 7 Specialist Expeditor

Demon 6 7 Weapons Expeditor

Demon Chief 7 AMU Superintendent

Demon Lead 7 AMU OIC

Demon Lead Alpha 7 Assistant OIC


Demon Lead Bravo 7 Assistant OIC

Demon Ramp Rat 7 AMU APG Line Supervisor

Demon Debrief 7 AMU Debrief Section

Demon Tow 7 AMU Aircraft Tow Team

Demon Support 7 AMU Support Section

Demon Supply 7 AMU Supply

Demon AGE 7 AMU Designated AGE Driver

Table A21.4. 49 MXS.

MXS 1 MXS Commander

MXS 2 MXS Maintenance Supervisor

MXS Chief MXS Maintenance Superintendent

MXS Super MXS Production Supervisor

Fabrication Fabrication Flight Chief

LO Lead Low Observable Element Expeditor

LO 1-3 Low Observable Dispatch Crew

LO ASM Low Observable Structural Repair Crew

Structures Base Remote Piloted Aircraft Structural Maintenance

Structures 1-3 Remote Piloted Aircraft Structural Maintenance

Metals Tech Metals Technology

NDI Nondestructive Inspection Station

Accessories Accessories Flight Chief

Egress Base Egress Element

Egress 1-2 Egress Element

Fuels Base Fuels System Repair Element

Fuels 1-2 Fuels Element Dispatch

AGE Flight AGE Flight Chief

AGE Super AGE Superintendent

Armament Armament Element

Props 1 Propulsion Element

Props 2 Propulsion Element

PMP Programmed Maintenance Package Element

Recovery Base Crash Recovery

Recovery 1 Crash Recovery

Recovery 2 MB2/UTE – Tow Vehicle

Recovery 3 Crash Recovery

Recovery 4 MB2 - Tow Vehicle

AFETS 1- 4 AFETS Field Service Representatives


Table A21.5. Munitions Support .

Ammo Control Munitions Control

Shadow Alternate Control

Blocker 1-10 Munitions Entry Control

Ammo 1 Munitions Flight OIC

Ammo 2 Munitions Flight Assistant OIC

Ammo Chief Munitions Flight Chief

Ammo 3 Munitions Flight Superintendent

System Super Systems Superintendent

Prod Super Production Superintendent

Mat Super Material Superintendent

Mobile 1 & 2 Munitions Mobility

Trainer 1-5 Munitions Training

Stacker 1–30 Munitions Storage

Hammer Dispatch Munitions Line Delivery Dispatch

Hammer 1-20 Munitions Line Delivery

TM 1-10 Munitions Trailer Maintenance

Iron 1-20 Munitions Conventional Maintenance

PGM 1–20 Precision Guided Munitions

Ammo Ops 1-10 Munitions Accountability

Inspector 1-10 Munitions Inspection

Table A21.6. Consolidated Aircraft Maintenance (CAM).

Table A21.7. CAM Division (T38).

Talon Chief T-38 Maintenance Superintendent

Talon Super T-38 Production Supervisor

Talon 1 T-38 Team Leader

Talon 2 T-38 Maintenance Crew/Tow Team

Talon 3 T-38 Maintenance Crew/Tow Team

Talon Debrief T-38 Debrief Section

Talon Phase T-38 Phase Docks

Talon COSO T-38 COSO

Talon EOR T-38 End of Runway Inspection Crew

M1 CAM Program Manager

DOC CAM Maintenance Operations Manager

Quality Control (QC) 1 PISM Division Manager

Quality Control (QC) 2-8 PISM Inspectors

Environmental Environmental

QAE 49 MXG CAM Contract Surveillance

Assurance Evaluators


Table A21.8. CAM Maintenance Division.

AGE 1 AGE Team Leader

Talon AGE AGE Driver

Egress Egress Shop

Prop 1 JEIM Supervisor

Test Cell Test Cell Maintenance Team

Alert 1-3 Transient Maintenance Vehicle

Fuels Fuels Shop

Table A21.9. 44 Fighter Group (FG)—AFRC

8 Ball 01 44 FG/CC

8 Ball 02 44 FG/CD (Ops)

8 Ball 03 44 FG/CD (Mx)

8 Ball 04 44 FG/CCC

Katz 01 301 FS/CC

Katz 02 301 FS/DO

Katz 03 44 OSF/CC

Katz 04 44 OSF/DO

Katz 05 44 OSF/DOL

Blue 01 44 AMXS/CC

Blue 02 44 AMXS/MXA (Ops O)

Blue Chief 44 AMXS/MXA

Gold 01 44 MXS/CC

Gold 02 44 MXS/MXM (Ops O)

Gold Chief 44 MXS/MXM

Table A21.10. ATKS Reaper Ops.

Warrior 1 29 ATKS Commander

Warrior 2 29 ATKS DO

Warrior Ops 29 ATKS Operations Supervisor

Table A21.11. 849 AMXS.

Rattler 1 AMXS Commander

Rattler 2 AMXS MOO

Rattler Chief AMXS Chief

Rattler Super AMXS Production Supervisor

Table A21.12. 6 AMU.

Venom Super AMU Production Supervisor

Venom 3 APG Expeditor

Venom 4 APG Expeditor

Venom 5 Specialist Expeditor

Venom 6 Weapons Expeditor


Venom Chief AMU Superintendent

Venom Lead AMU OIC

Venom Lead Alpha Assistant OIC

Venom Lead Bravo Assistant OIC

Venom Ramp Rat AMU APG Line Supervisor

Venom Debrief AMU Debrief Section

Venom Tow AMU Aircraft Tow Team

Venom Support AMU Support Section

Venom Supply AMU Supply

Table A21.13. 29 AMU.

Diamondback Super AMU Production Supervisor

Diamondback 3 APG Expeditor

Diamondback 4 APG Expeditor

Diamondback 5 Specialist Expeditor

Diamondback 6 Weapons Expeditor

Diamondback Chief AMU Superintendent

Diamondback Lead AMU OIC

Diamondback Lead Alpha Assistant OIC

Diamondback Lead Bravo Assistant OIC

Diamondback Ramp Rat AMU APG Line Supervisor

Diamondback Debrief AMU Debrief Section

Diamondback Tow AMU Aircraft Tow Team

Diamondback Support AMU Support Section

Diamondback Supply AMU Supply

Diamondback AGE AMU Designated AGE Driver

Table 21.14. 849 ACMU.

Gorilla Lead Maintenance Officer

Gorilla Lead Alpha Assistant OIC

Gorilla Chief Superintendent

Gorilla Super Production Supervisor

Gorilla 1 Expediter

Gorilla 2 Expediter

Gorilla 3 Technician

Gorilla 4 Technician



PRIVACY ACT STATEMENT

Figure A22.1. Privacy Act Statement.

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