MIL-DTL-85383A(AS)
c. Aircraft leveling and alignment.
d. Contour data.
e. Repair materials.
f. In-service tolerances.
3.2.7.1 Aircraft description. The first technical content WP(s) shall contain descriptive
material applicable to structural repair of the aircraft. This shall include information of the
following types plus any additional descriptive information pertinent to repair of the aircraft:
a. Types of construction used on the aircraft.
b. New materials used.
c. Principle dimensions.
d. Station location diagrams.
e. Structurally significant information.
f. Functionally significant information.
3.2.7.1.1 Types of construction. Brief descriptions and locations, supported by illustrations as
necessary, of principle types of construction used in the aircraft shall be included. This should
include such types as cantilever construction, stressed skin, tapered skin, plastics, and
honeycomb.
3.2.7.1.2 Principle dimensions. An illustration showing principle dimensions of the aircraft
shall be prepared. All significant dimensions required for structure repair shall be included.
3.2.7.1.3 Station location diagram. A diagram showing location of significant stations on the
aircraft shall be prepared. Reference points shall be identified as established in the engineering
drawings for the aircraft.
3.2.7.1.4 New types of materials. Brief descriptions of relatively new or unfamiliar materials
such as composite materials and high strength steels not covered in general series manuals shall be
included.
3.2.7.2 Repair materials. A separate WP containing lists of all materials required to make
repairs detailed in the manual/volume shall be prepared. The following shall be shown for each
item listed:
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