MIL-DTL-85383A(AS)
d. Wear tolerance charts.
e. Stress classification.
3.2.10.3 Typical repair procedures. Applicable typical repair procedures (3.2.8) shall be
referenced as specified in MIL-DTL-81927 (see 3.1.4).
3.2.10.4 Specific repair procedures. Information and procedures shall be included for
repairing all major structural assemblies which are identified as repairable. At least one WP shall
be prepared for each major assembly. Additional WPs shall be prepared as required because of
complexity of the data necessary to thoroughly cover a given assembly. These WPs shall include
the following types of data as applicable:
a. Support equipment required lists.
b. Materials required lists.
c. Structurally significant/functionally significant information.
d. Rework tolerances including minimum skin thickness.
e. Temporary repair procedures (including one-time-flight repairs).
f. Permanent repair procedures.
g. Contour data.
h. Procedures for constructing templates and repair jigs for use in repairing the assembly.
i. Precautions to be followed when working with toxic, corrosive, or combustible materials.
3.2.10.4.1 Structure sealing.
3.2.10.4.1.1 Airframe sealing. Sealing information and procedures shall be included for all
areas which require sealing for purposes other than corrosion control. Sealing for corrosion
control purposes shall be covered under corrosion control. The following shall be included in
structure repair:
a. Identification of areas requiring sealing.
b. Type of sealant required in each area.
c. Sealing procedures.
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