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MIL-DTL-81218 Manuals, Technical: Aircraft Engine Intermediate And Depot Maintenance, Preparation Of \(Work Package Concept\)This specification covers technical manual content requirements for preparation of aircraft engine intermediate and depot maintenance instructions in work package \(WP\) format for uninstalled reciprocating and gas turbine engines, including turboprop and turboshaft. This specification also covers requirements for an intermediate maintenance manual supplement for the installation, positioning, and identification of external tubing, cabling, clamping and attaching hardware and a Sequence Control Chart \(SCC\) that graphically depicts accomplishment of complete engine repair. When specified by the requiring activity, an Illustrated Parts Breakdown \(IPB\) shall be included.

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MIL-DTL-81218C(AS)
(GAPL), proper line art techniques in the preparation of supporting illustrations, and coordinated
GAPL entries with illustrations (see MIL-DTL-81927 and NAVAIR 00-25-700).
3.2 General requirements. Technical manuals prepared in accordance with this specification
shall be in WP format meeting the general style and format requirements of
MIL-DTL-81927 (see 3.1.4). The instructions shall consist of procedures for performing
intermediate and/or depot level maintenance. Intermediate and depot maintenance will not
normally be combined. Requirements of the gas turbine three-degree intermediate level
maintenance program in accordance with OPNAVINST 4790.2 shall be reflected, as applicable, in
intermediate level maintenance procedures.
3.3 Arrangement. Except when noted for specific application or restricted from use in a
specific application, arrangement shall be in accordance with MIL-DTL-81927 (see 3.1.4).
Arrangement of technical content WPs shall normally be as follows:
a. Description and principles of operation
b. Standard practices (if applicable)
c. Engine handling in shipping container/maintenance stand
d. Preparation for service and storage
e. Preinduction and mandatory inspection requirements
f. Preparation for test (pre-test set up)
g. Engine test
h. Troubleshooting
i. Removal and installation of major assemblies/subassemblies
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