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)

6.4 Specification figures. The figures previously included in this specification were intended

to illustrate methods of presentation of technical data. They are being revised for incorporation

into NAVAIR 00-25-700. Sample illustrations can be provided by the requiring activity, if

requested. The sample figures shall not be interpreted as limiting the technical content

requirements that are established by the text. The text must take precedence over all examples

shown in the sample figures.

6.5 Subject term (key word) listing.

Aircraft engine maintenance

External tubing, cabling and clamping

Illustrated parts breakdown

Sequence control chart

Work package concept

6.6 Changes from previous issue. Marginal notations are not used in this revision to identify

changes with respect to the previous issue due to the extent of the changes.

CONCLUDING MATERIAL

Preparing activity:

Navy-AS

(Project TMSS-N270)