01 March 2005
3-2.5. EVALUATION OF CORROSION DAMAGE.
Where torquing is required to tighten hardware,
Correct evaluation of avionic corrosion damage is
refer to specific technical manual for proper
necessary, and shall be classified as follows:
a. Repairable damage is damage that does not
exceed the limits specified in the applicable service
directives. The damaged surface or component shall
Compound, Corrosion Preventative 3
b. Replacement is required when damage exceeds
j. (Navy/Army Only) Where applicable, apply MIL-
3-2.6. Additional information on corrosion of specific
fasteners before reinstallation.
metals and nonmetals is found in Volume I of this
k. (Air Force Only) Where applicable apply MIL-C-
81309 Type II or MIL-L-87177 (Vol V, Chapter 2) to
threads of fasteners before reinstallation.
l. Secure access/compartment doors.
m. Repeat water test until no leaks are detected.