Miscellaneous Aircraft Accessories and Components: H16DW403-26, H16DW404-36, H16DW404-38
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| H16DW403-26 H16DW40326 | 1680-01-095-3579 | Wiring Harness, Branched | End Item Identification: AGM-86B, guide missile; aboard B52G Special Features: Flight control C station 92 to flight matrix assembly; component and part number: connector P/N 16VE049002-51, -57, 16VE049004-53; contact P/N M39029/4-20, /5-20-20, /22-16-16, MS27490-22D; endbell P/N C8821-1-12, -1-16, -2-25, C8824-1-10, C8822-1-8, -1-16, -1-24, C8822-2-21, M83723/75R1624N, /76R0803N, /75R24617, /75R1624N, /75R1212N, /28-20, /28-16; plug P/N MS2746T25F35C, MS2746T21F35S, MS27488-22; receptacle P/N M83723/71R10057; sleeving P/N C8844-1, -2, -3; socket P/N M6106/23-003; splice P/N C4812-23, NAS1744-3; terminal M7928/1-22, /1-23, /1-24; waffer P/N 16VE049011-11, -12 | Lockheed Martin Corporation (81755) | |
| H16DW403-28 H16DW40328 | 1680-01-095-3579 | Wiring Harness, Branched | End Item Identification: AGM-86B, guide missile; aboard B52G Special Features: Flight control C station 92 to flight matrix assembly; component and part number: connector P/N 16VE049002-51, -57, 16VE049004-53; contact P/N M39029/4-20, /5-20-20, /22-16-16, MS27490-22D; endbell P/N C8821-1-12, -1-16, -2-25, C8824-1-10, C8822-1-8, -1-16, -1-24, C8822-2-21, M83723/75R1624N, /76R0803N, /75R24617, /75R1624N, /75R1212N, /28-20, /28-16; plug P/N MS2746T25F35C, MS2746T21F35S, MS27488-22; receptacle P/N M83723/71R10057; sleeving P/N C8844-1, -2, -3; socket P/N M6106/23-003; splice P/N C4812-23, NAS1744-3; terminal M7928/1-22, /1-23, /1-24; waffer P/N 16VE049011-11, -12 | Lockheed Martin Corporation (81755) | |
| H16DW403-29 H16DW40329 | 1680-01-095-3579 | Wiring Harness, Branched | End Item Identification: AGM-86B, guide missile; aboard B52G Special Features: Flight control C station 92 to flight matrix assembly; component and part number: connector P/N 16VE049002-51, -57, 16VE049004-53; contact P/N M39029/4-20, /5-20-20, /22-16-16, MS27490-22D; endbell P/N C8821-1-12, -1-16, -2-25, C8824-1-10, C8822-1-8, -1-16, -1-24, C8822-2-21, M83723/75R1624N, /76R0803N, /75R24617, /75R1624N, /75R1212N, /28-20, /28-16; plug P/N MS2746T25F35C, MS2746T21F35S, MS27488-22; receptacle P/N M83723/71R10057; sleeving P/N C8844-1, -2, -3; socket P/N M6106/23-003; splice P/N C4812-23, NAS1744-3; terminal M7928/1-22, /1-23, /1-24; waffer P/N 16VE049011-11, -12 | Lockheed Martin Corporation (81755) | |
| H16DW403-30 H16DW40330 | 1680-01-095-3579 | Wiring Harness, Branched | End Item Identification: AGM-86B, guide missile; aboard B52G Special Features: Flight control C station 92 to flight matrix assembly; component and part number: connector P/N 16VE049002-51, -57, 16VE049004-53; contact P/N M39029/4-20, /5-20-20, /22-16-16, MS27490-22D; endbell P/N C8821-1-12, -1-16, -2-25, C8824-1-10, C8822-1-8, -1-16, -1-24, C8822-2-21, M83723/75R1624N, /76R0803N, /75R24617, /75R1624N, /75R1212N, /28-20, /28-16; plug P/N MS2746T25F35C, MS2746T21F35S, MS27488-22; receptacle P/N M83723/71R10057; sleeving P/N C8844-1, -2, -3; socket P/N M6106/23-003; splice P/N C4812-23, NAS1744-3; terminal M7928/1-22, /1-23, /1-24; waffer P/N 16VE049011-11, -12 | Lockheed Martin Corporation (81755) | |
| H16DW403-505 H16DW403505 | 1680-01-145-3359 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-517 H16DW403517 | 1680-01-194-3653 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-522 H16DW403522 | 1680-01-229-5526 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-546 H16DW403546 | 1680-01-308-0254 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-547 H16DW403547 | 1680-01-308-0255 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-548 H16DW403548 | 1680-01-308-0253 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-549 H16DW403549 | 1680-01-308-0256 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-566 H16DW403566 | 1680-01-308-0260 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-567 H16DW403567 | 1680-01-308-0261 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-573 H16DW403573 | 1680-01-308-0257 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-574 H16DW403574 | 1680-01-308-0258 | Wiring Harness, Branched | Lockheed Martin Corporation (81755) | ||
| H16DW403-82 H16DW40382 | 1680-01-148-4259 | Wiring Harness, Branched | III End Item Identification: F-16B aircraft tail effectivity 62 O1OO O1OO, 62 O1O3 O1O4, 62 O1O6 O115, 62 O116 9999 Special Features: C/O connector P/N 16VE049002-51, -57, 16VE049004-53;WAFER P/N 16VE049011-11, -12;TAPE P/N P5372-1-2;PLUG P/N M83723/75R1624M, /75R0803N, 75R24617, /75R1212N, MS27467T25F35SC, MS27467T21F35S, M83723/28-20, MS27488-22;RECEPTACLE P/N M83723/71R10057;CLAMP P/N C8821-1-16, -2-25, C8824-1-10;ADAPTER P/N C8822-1-8, -1-12, -1-16, -1-24, -1-21;SLEEVING P/N C8844-1, -2, -3;SPLICE P/N NAS1744-3;TERMINAL P/N M7928/1-15, /1-24 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
| H16DW403-83 H16DW40383 | 1680-01-148-4259 | Wiring Harness, Branched | III End Item Identification: F-16B aircraft tail effectivity 62 O1OO O1OO, 62 O1O3 O1O4, 62 O1O6 O115, 62 O116 9999 Special Features: C/O connector P/N 16VE049002-51, -57, 16VE049004-53;WAFER P/N 16VE049011-11, -12;TAPE P/N P5372-1-2;PLUG P/N M83723/75R1624M, /75R0803N, 75R24617, /75R1212N, MS27467T25F35SC, MS27467T21F35S, M83723/28-20, MS27488-22;RECEPTACLE P/N M83723/71R10057;CLAMP P/N C8821-1-16, -2-25, C8824-1-10;ADAPTER P/N C8822-1-8, -1-12, -1-16, -1-24, -1-21;SLEEVING P/N C8844-1, -2, -3;SPLICE P/N NAS1744-3;TERMINAL P/N M7928/1-15, /1-24 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
| H16DW404-20 H16DW40420 | 1680-01-056-9781 | Wiring Harness, Branched | III End Item Identification: U/O flt ctl D sta 92 to flt ctl matrix assy acft F16 Special Features: Plug 4, receptacle 2, end bell 3 | Lockheed Martin Corporation (81755) | |
| H16DW404-36 H16DW40436 | 1680-01-140-4411 | Wiring Harness, Branched | End Item Identification: F-16A aircraft, tail effectivity 61 0443 9999 Special Features: Components: adapter 5; bus 1; clamp 4; connector 5; receptacle 2; splice 2; terminal 17; waffer 10; plug, sleeve, sleeving, tape, tubing as required; exact wire length to be determined on first installation; braid per 16PR106 using two tracers per 16PR145; add C2065-14 braid over wires from 2705J121/L and 2705J121/R to aft side of bulkhead 65; service data -38 may be used for all replacements of -36 | Lockheed Martin Corporation (81755) | |
| H16DW404-38 H16DW40438 | 1680-01-140-4411 | Wiring Harness, Branched | End Item Identification: F-16A aircraft, tail effectivity 61 0443 9999 Special Features: Components: adapter 5; bus 1; clamp 4; connector 5; receptacle 2; splice 2; terminal 17; waffer 10; plug, sleeve, sleeving, tape, tubing as required; exact wire length to be determined on first installation; braid per 16PR106 using two tracers per 16PR145; add C2065-14 braid over wires from 2705J121/L and 2705J121/R to aft side of bulkhead 65; service data -38 may be used for all replacements of -36 | Lockheed Martin Corporation (81755) |