TO 35-1-3 - Robins Air Force Base
TO 35-1-3 - Robins Air Force Base
TO 35-1-3 - Robins Air Force Base
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>TO</strong> <strong>35</strong>-1-3<br />
3.26.7 Wire Harness and Cables. Instructions for cleaning<br />
the wire harness and cables are as follows:<br />
Replace all connectors that show moderate to severe<br />
corrosion damage.<br />
3.26.5.1 Apply CPC MIL-L-87177, Grade B, to internal surfaces.<br />
Preserve outer shell with MIL-PRF-16173, Grade 4.<br />
Wipe off excess with a clean cloth.<br />
3.26.5.2 For equipment operating, deploying to, or based in,<br />
severe corrosion prone locations, the use of Av-DEC “HiTAK”<br />
polyurethane stretch seal is authorized for use around mated<br />
electrical connectors, coaxial connectors, and electrical quick<br />
disconnect fittings.<br />
3.26.6 Switches. Cleaning instructions for the switches are<br />
as follows:<br />
3.26.6.1 Scrub switch with isopropyl alcohol, TT-I-7<strong>35</strong> and<br />
toothbrush, A-A-59 or A-A-123. Wipe with clean cloth, CCC-<br />
C-46. Allow to air dry.<br />
3.26.6.2 Apply a thin coat of CPC MIL-L-87177, Grade B to<br />
the electrical contact points.<br />
3.26.6.3 Wipe all sliding contacts, cams, and contact points<br />
with a clean cloth, CCC-C-46, Class 4 or pipe cleaner to<br />
remove CPC.<br />
NOTE<br />
• Contact points must be clean of CPC to function<br />
properly.<br />
• Cleaning solvents and compounds may adversely<br />
react with plastics such as harness tubing, gaskets,<br />
seals, etc. Test a small area for softening or reaction<br />
prior to general use.<br />
3.26.7.1 Scrub corroded area with MIL-PRF-29608. Flush<br />
area with cleaning compound. Shake excess solvent from wire<br />
harness. Remove residue with a clean cloth, CCC-C-46 and<br />
allow to air dry.<br />
3.26.8 Heli-Coil Insert Replacement. Steps for removal of<br />
the insert are as follows.<br />
3.26.8.1 Remove the defective insert.<br />
3.26.8.2 Clean and dry the female thread from which the<br />
defective insert was removed.<br />
3.26.8.3 Apply MIL-PRF-23377, Type I, Class 2 primer<br />
sparingly to the cleaned female thread.<br />
3.26.8.4 Before the primer dries, install new insert and<br />
remove the insert driving tag.<br />
3-19/(3-20 blank)