ARMY TM 9-6115-673-13&P
AIR FORCE TO 35C2-3-512-1
NOTES:
PROCEDURES:
1. Dimensions are shown in inches and
1. Cut each wire to length indicated, then strip 0.50
dimensions in [ ] are in millimeters.
[13] from ends of each wire.
2. Refer to Appendix F, F-33 for materials
2. Insert wires ref. no. 1-6 into pins from connector
required.
(6) and crimp using crimping tool.
3. Connector shall be marked "P2" on insulation
3. Slide tubing (9) and 1.75 to 2.25 [44.4 to 57.2] of
sleeving with 0.18 [5] minimum high characters
insulation sleeving (8) over wires ref. no. 1-6).
IAW MIL-STD-130, using rubber stamp or
stencil.
4. Insert pins from connector (6) through clamp (7)
and using a pin insertion tool, insert pins from
connector (6) into connector (6) until pins lock
into place, following termination indicators in
wire list reference table.
5. Clamp wires ref. no. 1-6 to connector (6).
6. Slide tubing (9) up to clamp (7), slide insulation
sleeving (8) over tubing (9) and clamp (7), and
heat shrink to a firm fit.
7. Cut tubing (4) into a 19 inch length and a 22
inch length. Slide 22 inch tubing (4) over wire
ref. no. 1. Slide 19 inch tubing (4) over wires ref.
no. 3, 4, 5 and 6.
8. Insert tubings (4) and (9) into tee (10) and close
tee clamping tubes.
9. Slide nipple (2) over wire ref. no. 1. Slide
terminal lug (1) over wire ref. no. 1 and crimp.
10. Slide boot (15) over wire ref. no. 2. Slide
terminal lug (16) over wire ref. no. 2 and crimp.
11. Slide quick disconnect terminals (14) over wires
ref. no. 5 and 6 and crimp. Slide quick
disconnect terminal (13) over wire ref. no. 3 and
crimp.
12. Slide nipple (2) over wire ref. no. 4. Slide
terminal lug (12) over wire ref. no. 4 and crimp.
14. Position straps (3) at 3-inch intervals and at all
breakouts.
15. Mark the appropriate wire number which will
consist of the "FROM" termination, a double-
headed arrow (↔), and the "TO" termination.
Figure G-10. Wiring Harness, Engine (P/N: 95-8029) (Sheet 3 of 3)
G-18
