MIL-DTL-38769E
6.12 Time change, conigured article, serially controlled, and warranty tracked items. These items will be
approved by the acquiring activity (see 3.2.10.1).
6.13 End item identiication. End item identiication is intended to aid the maintenance technicians
in identifying what equipment should be entered in the "end item Work Unit Code" block of the
maintenance forms (see 3.2.11).
6.14 Area site. In determining the area of skin panel size for individual coding, the rivet lines are
normally used as a boundary. It is a matter of judgement to contain an area large enough to provide
the ability to localize deiciencies (see 3.2.16.2).
6.15 Work unit code manual. Work unit code manual construction will vary depending on the concept
dictated by the equipment to which it applies. SE that is commonly used in the Air Force is included in the
TO 00-06-series Work Unit Code manuals. Clariication of equipment applicability will be provided by the
applicable system manager through the acquiring activity (see 3.3).
6.16 Chapters 1, 2, and 3. These chapters provide information used by maintenance personnel to
record maintenance tasks accomplished directly on the end item, components, or equipment undergoing
repair, servicing, testing, calibration, or bench check in specialized shops (see 3.3.1.1, 3.3.1.2, 3.3.2.1,
6.17 Effectivity date. The effectivity date will be a minimum of 30 days subsequent to the actual
distribution date. All effectivity dates will be the irst day of the month. The effectivity date will be
established by the acquiring activity (see 3.2.1).
6.18 Page numbering. Print Presentation: The irst page of the table of contents will be I-001, and the ifth
page of the how malfunctioned codes engine related (alphabetical sequence) will be X-005. The irst page of
the support general codes will be 01-001, and the eleventh page of inertial guidance systems codes (air
launched missile) will be 62-011. The irst page of the engine turbine/turboprop/combustion section will be
72-30-01, and the sixth page of the landing gear/steering section will be 32-50-06 (see 3.1.6).
6.19 Acronyms. The acronyms used in this document are deined as follows:
ADM
- Air Defense Missile.
AFI
- Air Force Instruction.
AFSATCOM
- Air Force Satellite Communications.
AGM
- Air to Ground Missile.
AMAC
- Aircraft Monitor and Control.
AWACS
- Airborne Warning and Control System.
AWCS
- Airborne Weapon Control System.
CAE
- Computer Assisted Enrollment.
CE
- Communication Electronic.
CIE
- Controlled Interval Extension.
DODISS
- Department of Defense Index of Speciications and Standards.
DTD
- Document Type Deinition.
EMUX
- Electrical Multiplex.
HF
- High Frequency.
HMC
- How Malfunction Code.
IFF
- Identiication, Friend or Foe.
IR
- Infrared Radiation.
JCALS
- Joint Computer-aided Acquisition and Logistics Support.
LF/LCF
- Low Frequency/Low Cycle Fatigue.
LLC/TCI
- Limited Life Component/Technical Critical Item.
MCS
- Maintenance Cost System.
MDS
- Mission Design Series.
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