01-138-7963
Power Electrical Cable Assembly
Outlet strip w/six outlets second end jack
01-138-8761
Conductor Bus
13.280" overall length tin surface treated
01-138-8762
Conductor Bus
6.680" overall length tin surface treated
01-138-8763
Conductor Bus
01-138-8764
Conductor Bus
5.030" overall length tin surface treated
01-138-8765
Conductor Bus
10.530" overall length tin surface treated
01-138-8766
Conductor Bus
9.980" overall length tin surface treated
01-138-8767
Conductor Bus
1.730" overall length tin surface treated
01-138-8768
Conductor Bus
16.580" overall length tin surface treated
01-138-8769
Conductor Bus
6.130" overall length tin surface treated
01-138-8770
Conductor Bus
7.230" overall length tin surface treated
01-138-8771
Conductor Bus
8.880" overall length tin surface treated
01-138-8775
Conductor Bus
8.340" overall length tin surface treated
01-138-9117
Wiring Harness
F-16 aircraft, tail effectivity 0007-0116
01-139-0004
Wiring Harness
F-16b air combat fighter, part number H16DW094-03 remains effective on type version 5b/5d
01-139-0014
Electrical Winding Wedge
Sq formed wedge formed from duroid matl c/o polyester fiber paper saturated w/heat resistant epoxy resin fully densified
01-139-0214
Branched Wiring Harness
Used on f-16 aircraft. c/o wafer p/n 16VE049011-1; keeperp/n C310-3; tape p/n P5372-1-2; receptacle p/n U92a/u; bus p/n C8865-3; sleeving p/n C8844-1, -3; splice p/n NAS1745-18; exact length to be determined on first installation; braid harness per 16PR106; inner shield to be stripped
01-139-0215
Branched Wiring Harness
Used on f-16a aircraft. c/oconnector p/n 16VE049002-51; wafer p/n 16VE049011-11; keeper p/n C310-3; tape p/n P5372-1-2; receptacle p/n UG92a/u; bus p/n C8865-3; sleeving p/n C8844-1, -3; sleeve p/n C8867-2; splice p/n NAS1744-3, NAS1745-18; exact length to be determined on first installation, braid harness per 16PR106; solder per mil-std-454d requirement 5; part number -01remains effective on two versions-5a
01-139-0280
Electrical Load Bank
Used on bgm 109 glcm.
01-139-1813
Power Electrical Cable Assembly
01-139-1814
Power Electrical Cable Assembly
Used on an/tsc-85a/93a.
01-139-1815
Power Electrical Cable Assembly
01-139-1816
Power Electrical Cable Assembly
01-139-1820
Special Purpose E Cable Assembly
01-139-1822
Special Purpose E Cable Assembly
01-139-1830
Electrical Lead
01-139-1886
Special Purpose E Cable Assembly
Used on nsn 2350-01-085-3792,carrier,cmbt,ftxm981. consists of: 1 ea. connector, p/n MS3102R36-6s; 1 ea. boot, p/n 12306827; 2 ea. cable, p/n M13486/1-9; 2 ea. cable, p/n M13486/1-14; for additional information refer to cage 19207 p/n 12307149
01-139-2009
Branched Wiring Harness
Used on f-16 aircraft.
01-139-2143
Special Purpose E Cable Assembly
Dust cap 1, splice 2, tubing 1, band 2, boot 1 receptacle
01-139-2147
Special Purpose E Cable Assembly
01-139-2389
Electrical Cable Assembly-switch
Used on test stand. c/o 4 conductors, 1 ea red, green, white
01-139-2390
Electrical Cable Assembly-switch
Used on ch-53e helicopter. approx 12.000 in.lg; 1 21SM284-js-5
01-139-2391
Electrical Cable Assembly-switch
Stx terminals, two switches with insulation sleeving, connector
01-139-2403
Branched Wiring Harness
Used on f-16a/b acft. t.o. 1f-16a-4-24; braid per 16PR106
01-139-2404
Branched Wiring Harness
Used on f-16a aircraft. consists of 78 contacts; tape as required; 5 clamps; 1 adapter; sleeving asrequired; 10 sleeves; 6 terminals; 10 receptacles; plugs as required; exact wire length to be determined on first installation; braid harness per 16PR106; service data-26 may be used for all replacements of -23
01-139-2405
Branched Wiring Harness
Used on f-16 a/b aircraft. uconsists of 1 connector; 1 wafer; tape as required; 12 contacts; plugs as required; 6 splices; 4 clamps; 2 adapters; 1 cap; sleeving as required; 4 sleeves; 9terminals; exact wire length to be determined on first installation; braid PER16PR106; 4911WT35 splice is called out on H16DW1739 for F16a
01-139-2407
Branched Wiring Harness
Used on f-16 aircraft. c/oconnector p/n 16VE049002-55, -52; wafer p/n 16VE049011-11, -12, -1, -2; tape p/n P5372-1-2; contact p/n C8862-20-185; plug p/n M83723/75R1624n, /75R24616, M83723/28-20; splice p/n C4812-23; clamp p/n C8821-1-16, -1-24; tubing p/n C2026-1-5; sleeving p/n C8844-2, -3; terminalp/n M7928/1-22, /1-23, /1-24; braid harnes per 16PR106, using 2 tracers per 16PR145
01-139-2408
Branched Wiring Harness
Used on f-16a aircraft. consists of 1 connector; 4 wafers; tape as required; contacts as required; plugs as required; 3 receptacles; 5 clamps; 7 adapters; sleeving as required; 7 terminals; exact wire lengths to be determined on first installation; braid harness per 16PR106
01-139-2410
Branched Wiring Harness
Used on f-16 aircraft. c/oconnector p/n 16VE049002-52; wafer p/n 16VE049011-1, -50, -12; contact p/n M39029/5-16-20, C2107-50-2, M39029/30-16S16; backshell p/n C10558-1, -3; clampp/n C8821-1-8, -10, -12, -16, -20; plug p/NMS27488-20, MS3459L10sl-4s, M83723/75R0803n, M83723/75R08039, C8807-1-1, M83723/75R2028n, MS345942s-4s, MS3459L16-11s, M83723/75R0836, MS3476L12-3s, M83723/28-20, -16, -12, MS3187-16-2, C8916-7-6; adapter p/n C8822-1-8, C8822-1-12; sleeving p/n C8844-1, -2, -3; splice p/n NAS1744-2, C4812-23; sleeve p/n C8951-11, -12; terminalp/n M7928/1-13, -15, -24, -11, M7928/1-29, -58; switch p/n MS24658-30f
01-139-2411
Branched Wiring Harness
Used on f-16a acft. f-16a belguim peculiar; tail effectivity 6h 0066 9999; consist of: 8 wafer; 4 connector; 10 adapter; 5 terminals; 2 splice; 1 ferrule; plug; contacts; bus
01-139-2412
Branched Wiring Harness
Used on f-16 aircraft. c/oconnector p/n 16VE049002-51; wafer p/n 16VE049011-1, -50; tape p/n P5372-1-2; plug p/n MS3475L24-61s, M83723/28-20; splice p/n C4812-23; backshell p/n C10558-3; clamp p/n C8824-1-24; sleevingp/n C8844-2, -3; sleeve p/n C8951-2; exact length to be determined on first installation
01-139-2413
Branched Wiring Harness
Used on f-16 aircraft. c/owafer p/n 16VE049011-12, -11, -1, -2, -50; connector p/n 16VE049002-55, -54; tape p/n P5372-1-2; contact p/n C8862-20-18s; splice p/n C4812-23; clamp p/n C8821-1-24; sleeving p/n C8844-2, -3; plug p/n M83723/75R24616, 28-20; braid harness per 16PR106, using two tracers per 16PR145
01-139-2510
Wiring Harness
Used on f-16b air combat fighter,tail effectivity 62 0077 9999. f-16b aircraft, service data-02 may be used for all replacements of -01
01-139-2511
Wiring Harness
Used on f-16b/d acft. t.o. 1f-16a/c-4-24; p/o interphone communication system
01-139-2518
Special Purpose E Cable Assembly
01-139-2519
Special Purpose E Cable Assembly
01-139-2671
Conductor Bus
01-139-2714
Special Purpose E Cable Assembly
Dual receptacle
01-139-2715
Special Purpose E Cable Assembly
2 boot, 2 dust cap dual receptacle
01-139-2716
Special Purpose E Cable Assembly
