NAVAIR 01-1A-509-3
01 March 2005
TM 1-1500-344-23-3
TO 1-1-689-3
3-2.5. EVALUATION OF CORROSION DAMAGE.
NOTE
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:
torque values.
a. Repairable damage is damage that does not
exceed the limits specified in the applicable service
directives. The damaged surface or component shall
be cleaned, treated, and a preservative applied, as
Compound, Corrosion Preventative 3
applicable.
Water-Displacing
MIL-C-81309
b. Replacement is required when damage exceeds
repair limits.
j. (Navy/Army Only) Where applicable, apply MIL-
C-81309 Type II (Vol IV, Chapter 2) to threads of
3-2.6. Additional information on corrosion of specific
fasteners before reinstallation.
metals and nonmetals is found in Volume I of this
manual.
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.
3-5/(3-6 Blank)
3-5