Aircraft and Missile Prime Movers Engine Fuel System Components: 6941-2, 6944377, 695540-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6941-2 69412 | 2915-00-045-5097 | Valve, Transfer Control, Fuel | III End Item Identification: F111 acft pylon fuel system General Characteristics Item Description: 8.5 in. l, approx 4.0 in. H X 4.5 in w; parts incl air hsg, actuator 80214, piston 40744; fuel hsg, float 40782, piston 25003, diaphragm 25018 and housing; single coil, continuous duty solenoid, duty 18-30 V, M65-350 deg F III Fsc Application Data: Valve linear, directional control, powered, engine acft | Argo-Tech Corporation Costa Mesa (86090) | |
| 6944377 | 2915-01-446-1099 | Housing and Tubes | III End Item Identification: Acft eng F101 | Parker-Hannifin Corporation (09523,59211) | |
| 6944393 | 2915-01-446-1000 | Cartridge Assy, Valv | III End Item Identification: Acft eng F101 | Parker-Hannifin Corporation (09523,59211) | |
| 6944397 | 2915-01-446-1012 | Cover, Core Spray Ba | III End Item Identification: Acft eng F101 | Parker-Hannifin Corporation (09523,59211) | |
| 6944406 | 2915-01-459-8001 | Support, Nozzle | III End Item Identification: Right hand fuel nozzle, P/N6830087, for TF39 acft eng | Parker-Hannifin Corporation (09523) | |
| 6944407 | 2915-01-459-8002 | Support, Nozzle | III End Item Identification: Center fuel nozzle, P/N 6770136, for TF39 acft eng | Parker-Hannifin Corporation (09523) | |
| 6944408 | 2915-01-459-8003 | Support, Nozzle | III End Item Identification: Left hand fuel nozzle, P/N 6830098 for TF39 acft eng | Parker-Hannifin Corporation (09523,59211) | |
| 6944409 | 2915-01-459-8004 | Support and Meterin | III End Item Identification: Right hand fuel nozzle, P/N 6830087 for TF39 acft eng | Parker-Hannifin Corporation (09523,59211) | |
| 6944410 | 2915-01-459-5485 | Support and Meterin | III End Item Identification: Cen fuel nozzle assy, P/N 6770136 for TF39 acft eng | Parker-Hannifin Corporation (09523,59211) | |
| 6944411 | 2915-01-459-5486 | Support and Meterin | III End Item Identification: L.H. fuel nozzle assy, P/N 6830098, for FT39 acft eng | Parker-Hannifin Corporation (09523,59211) | |
| 69458A4 | 2915-00-791-5760 | Lock, Serrated | III End Item Identification: Fuel control, P/N 547300L2 engine, acft, J75 General Characteristics Item Description: Cres, rockwell hardness RC31-39 core, 1000VH min case hardened, 36 serrations equally space, 3/8-32UNEF-3A thd data, surface coating, per MIL-L-25504 per HS298, class 40, type 1 | Hamilton Sundstrand Corporation (73030) | |
| 69460A4 | 2915-00-780-2158 | Lock Serrated Detent | General Characteristics Item Description: Cres, hamilton standard spec no. HS178, rockwell hardness, RC31-39, case harden, 1000 vh min, 0.170 in. min, 0.175 in. max O/a lg, 0.221 in. min, 0.223 in. max body od, 0.320 in. min, 0.330 in. max head dia, 36 serrations equally spaced | Hamilton Sundstrand Corporation (73030) | |
| 694717 | 2915-00-152-1985 | Heater, Fuel Turbine | III End Item Identification: Aircraft engine model J60 General Characteristics Item Description: Steel | United Technologies Corporation (77445) | |
| 69476-150 69476150 | 2915-00-716-2545 | Tab, Locking | Hamilton Sundstrand Corporation (73030) | ||
| 695001002 | 2915-00-445-3454 | Control unit, Fuel | Messier Dowty LTD (K0654) | ||
| 6950-011-100 6950011100 | 2915-01-475-0623 | Actuator, Electro-Mechanical, Rota | Special Features: Gearing - 17 4PH s.s.;switches - 250 vac 10 amp Environmental Protection: Any acceptable | Curtiss-Wright Corporation (63600) | |
| 695046 | 2915-00-169-2878 | Nozzle, Afterburner | III End Item Identification: Aircraft engine model J79 General Characteristics Item Description: Nickel alloy, 3.470 in. min, 3.530 in. max O/a, lg | Triumph Actuation Systems (57850) United Technologies Corporation (77445) | |
| 695046 | 2915-00-595-1652 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, electrically driven, 0.8 hp, alternating current, 200 volts, 400 cps, 3 phase, 11.0 starting amps and 4.6 amps flow rate, 6000.0 pph max rated flow, for use with fuel and oil, 15.2 gpm max rated capacity, 5450.0 rpm, vertical pumping position, rotates counter clockwise, single stage impeller, 2 inlet ports W/strainers, 2.500 in. dia opening on lower port, 1 outlet port size 1.500 in. min to 1.510 in. max dia opening, O/a dim. 9.000 in. lg by 8.225 in. W, flange mtg W/4 ears, mtg holes size 0.276 in. min to 0.286 in. max dia spaced 4.700 in. and 3.145 in. C to C, explosive proof case, external discharge | Lockheed Martin Corporation (98897) | |
| 695311 | 2915-01-507-3112 | Pump Assembly, Submerged, Aircraft | Hamilton Sundstrand Corporation (99167) | ||
| 695346-1 6953461 | 2915-01-558-6638 | Tube Assembly, Aircraft Engine | III End Item Identification: Gas turbine aircraft engine, model number GTCP95-2, GTCP95-3, GTCP95-10 III Part Name Assigned By Controlling Agency: High pressure line (tube) Overall Diameter: 0.250 inches nominal | Honeywell International Inc. (99193) | |
| 695540-1 6955401 | 2915-00-506-3593 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, aluminum alloy seating surface, stainless steel seat seating surface; anodized finish on aluminum surfaces; float data, 2 floats, 12 deg approx effective travel of floats; W/solenoids, 2 solenoids, dc; port data, inlet port, thd female, U/W 1/4 in. od tube, thread data, 7/16-20 thd size, unf, class 3 fit, rh; mounting data, horizontal position, side mounted, 16 mtg holes; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-G-5572 and MIL-T-5624; over-all dimensions, 7-7/8 in. lg, 3-23/64 in. W, 5-7/8 in. H | Lockheed Martin Corporation (98897) |