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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
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.
4 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 5
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
6 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 7
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
8 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 9
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.
10 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 11
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.
12 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 13
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.
14 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 15
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.
16 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 17
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
18 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 19
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:
20 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
12.1.15.1.5.1. (Added) Sited for HD 1.1 munitions not to exceed 2,000 lbs
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:
12.1.15.1.6.1. (Added) Sited for HD 1.1 munitions not to exceed 1,000 lbs
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
marked and grounding points are available.
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:
12.1.15.1.7.1. (Added) Sited for HD 1.1 munitions not to exceed 2,000 lbs
Net Explosive Weight (NEW) per spot.
12.1.15.1.7.2. (Added) Sited for 18 aircraft parking/loading spots. Spots are
marked and grounding points are available.
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:
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 21
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
marked and grounding points are available.
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
22 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 23
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
24 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 25
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,
26 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 27
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.
28 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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).
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 29
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.
30 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 31
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).
32 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 33
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
34 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 35
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
36 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
Attachment 15 (Added)
IMIS WORK CENTER MNEMONIC CREATION REQUEST LETTER
Figure A15.1. IMDS Work Center Mnemonic Creation Request Letter.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 37
Attachment 16 (Added)
IMDS WORKCENTER MNEMONIC DELETION REQUEST LETTER
Figure A16.1. IMDS Work Center Mnemonic Deletion Request Letter.
38 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
Attachment 17 (Added)
MEMORANDUM FOR IMDS DATABASE MANAGER
Figure A17.1. Memorandum for IMDS Database Manager.
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 39
Attachment 18 (Added)
DATA INTEGRITY APPOINTMENT LETTER
Figure A18.1. Data Integrity Appointment Letter.
40 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
Attachment 19 (Added)
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 41
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
42 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
Attachment 20 (Added)
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 43
Attachment 21 (Added)
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
44 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 45
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
46 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
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
AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013 47
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
48 AFI21-101_CAFSUP_HOLLOMANAFBSUP 18 NOVEMBER 2013
Attachment 22 (Added)
PRIVACY ACT STATEMENT
Figure A22.1. Privacy Act Statement.
Recommended