MIL-DTL-85383A(AS)
3.2.10.1 Repair data. Specific repair WPs shall show compliance with all relevant design
requirements. They shall contain complete repair data including the following;
a. Definite, positive statements regarding repair decisions to preclude misinterpretation and
indecision concerning use of typical repairs.
b. Cautions prohibiting all unauthorized repairs and procedures including combinations which
would weaken or overstiffen structure beyond safe limits.
c. Where loads, material thickness, and margins of safety vary, tables shall be provided
indicating the following data which is required to transfer design loads safely:
(1) location,
(2) material thickness,
(3) fastener size,
(4) fastener pattern,
(5) fastener spacing,
(6) doubler overlap,
(7) bonding requirements, and
(8) reinforcements.
d. Where loads do not vary, identification of typical loads and minimum design tolerance in
tension, compression, and shear.
e. Illustrations showing where various types of repairs are to be used.
3.2.10.2 Damage identification and evaluation data. Damage identification and evaluation
data (3.2.3 and 3.2.4) shall be included for each component covered in the structural group repair
WPs. Each applicable category of damage shall be clearly defined for each component. Examples
shall be prepared when necessary. Damage evaluation data shall include the following to the
extent necessary to guide a technician to the procedure required to repair the aircraft:
a. Material specifications (composition, gauge, temper).
b. Structurally significant/functionally significant information.
c. Identification of damage limits.
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