MIL-DTL-85383A(AS)
c. Procedures for moving the damaged aircraft from the crash site. This shall include
identification of necessary handling equipment, securing the aircraft, required clearances
after loading, and load weights.
d. References to corrosion control and preservation manuals for applicable corrosion
prevention and preservation procedures.
e. Disassembly into structural groups or sections.
f. Weight and center of gravity of each component.
g. When applicable and not included in other available manuals, crating and shipping
instructions. These shall include:
(1) Manufacturing of crates.
(2) Manufacturing of cradles.
(3) Installation of equipment in crates.
(4) Support points.
(5) Weight of each component.
(6) Weight and center of gravity of each crated component.
3.2.8 Typical repair data WPs. Typical repairs are those which are applicable to more than
one structural group or component covered in the manual. To avoid unnecessary duplication,
typical repairs shall be covered in separate WPs and referenced as needed. Typical repair WPs
should include but shall not be limited to the following:
a. Skin patch repair.
b. Transparent panel repair.
c. Honeycomb structure repair.
d. Extrusion repair.
e. Sealed area repair.
f. Formed structure repair.
g. Plastic repair.
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