MIL-DTL-87158C
3.12.3.4 Fuel system assessment. This system assessment shall contain the requirements of 3.12.3.
Illustrations shall include isolation points, access covers, single point receptacles, typical fuel tank
arrangements, and fuel tank components and plumbing locations. Distinction shall be made between fuel leaks
that constitute a light safety hazard, and those that do not. Alternate settings or modiications to the fuel
control panel, which will permit isolation of various tanks, shall be included. Weight and balance implications
of these actions shall be addressed. Any specialized fuel tank sealing instructions shall be provided.
3.12.3.5 Armament system assessment. This system assessment shall contain the requirements of 3.12.3.
The minimum/maximum power and voltage requirements, needed for operation of each armament system,
shall be included. Warnings concerning maximum power/voltage usable for system checks shall be speciied,
to preclude inadvertent system operations (e.g., munitions). Quick repair methods, such as "hot-wiring"
around inoperative black boxes, in order to operate the armament, shall be included. Armament limitations
shall be speciied for operation of systems, regardless of gear/wing positions.
3.12.3.6 Landing gear system assessment. This assessment category shall contain the requirements of
3.12.3. Pressure/volume/travel limits shall be speciied, if applicable.
3.12.3.7 Egress system assessment. This system assessment shall contain the requirements of 3.12.3. Repair
of damaged egress systems shall be restricted to direct replacement of components, or minor acceptable
repair to hoses, tubing, cables, wiring, and crew ejection systems. Acceptable repair limits, such as size,
location of damage, and minimum distance between repairs, shall be speciied. Repair procedures for each
seat type, rather than for aircraft type, shall be developed.
3.13 Chapter (n+1) engines. This chapter shall contain a brief description and illustrations, showing location
of mission essential engine system/components.
3.13.1 Illustrations. Each illustration shall consist of an orthographic view drawing of the engine system
components within that zone.
3.13.2 Tables. There shall be a minimum of two tables. Table 1 shall include system/subsystem, mission
serviceability criteria, and remarks (see Figure 6). Table 2 shall include index number, nomenclature,
acceptable damage, maintenance action/repair reference, functional checks, and effects/restrictions (see Figure
7). Pressure/volume/travel limits shall be speciied, if applicable. Minimum required functional capabilities
for appropriate components, shall be described. Allowable limited repairs shall be included. Any repairs to
propellers of propeller-driven aircraft shall be included. A table outlining the engine minimum power
requirements and functional checks shall be included. Full and partial operational capabilities shall be
reined per mission reinements.
3.14 Chapter (n+2) peculiar and special mission equipment wiring. A list of essential wiring by zone,
harness number, connector number, pin number, wire tie number and location, ground point and location,
system and aircraft effectivity by mission, shall be provided in this chapter, with specialized repair, if
applicable. The electrical wiring/harness data may be organized by harness number, location, or other method
as required (see Figure 8).
VERIFICATION
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4.1 Veriication. Veriication Requirements. When the technical data produced according to this speciication
is offered for acceptance, all tests, reviews, and veriications required by the acquiring activity to determine
that it conforms to the requirements in section 3 of the speciication, shall be performed as speciied
in the solicitation or contract. The Air Force Technical Order Policy and Procedures (AF TOPP) team,
AFMC/A4UE, provides the speciic requirements for veriication of technical data developed and delivered
through this speciication, as well as guidance for including these requirements in the solicitation or contract
(see TO 00-5-3, AF Technical Order Life Cycle Management, 2.2.2).
4.2 Compliance. Technical manuals (TMs) shall meet all requirements of Section 3 of this speciication and
the appropriate DTD appendix, as required by the acquiring activity (see 6.2). The requirements set forth in
this speciication shall become a part of the contractor s overall inspection system or quality program.
The absence of any requirements in this speciication shall not relieve the contractor of the responsibility
of ensuring that all products or supplies, submitted to the government for acceptance, comply with all
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