Aircraft and Missile Prime Movers Engine Fuel System Components: 543580, 5439999-509, 544317
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 543580 | 2915-00-918-8960 | Tube and Collar, Dra | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | ||
| 543591 | 2915-00-719-8736 | Housing, Bearing | Hamilton Sundstrand Corporation (73030) | ||
| 5439999 | 2915-00-315-8412 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, electrically driven, ac current, 200 volts, 400 cycles, 3 phase, for use with fuel and oil, vertical pumping position, rotates counter clockwise, 2 inlet ports, 1 outlet port, square flange, 2.375 in. sq, O/a dim. approx 11.187 in. lg by 7.875 in. dia, flange mounting W/16 holes, size 0.281 in. dia, equally spaced on 7.250 in. bcd, external discharge | Boeing Company, The (88277) | |
| 5439999-505 5439999505 | 2915-00-967-6548 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 200V ac, 400 cps, 3 ph, 7200 rpm, 5 amps, 10000 phr at 17.5 psi rated capacity, 11.187 in. lg, 8.000 in. W, 7.875 in. H O/a dim., 16 mtg holes 0.281 in. dia equispaced around mtg flange on a 7.250 in. dia circle, 4 wire electrical leads unprocessed, 90 deg external sq flange 1.312 in. id discharge connection | Boeing Company, The (88277) | |
| 5439999-509 5439999509 | 2915-00-626-2485 | Pump, Submerged, Aircraft | Boeing Company, The (18355,88277) | ||
| 544-0200-00-0 5440200000 | 2915-01-322-3597 | Cap, Valve | Special Features: 2.252 in. min, 2.258 in. max lg from flange to end of rod; item C/O valve cover P/N 044-1190-00-0; set screw P/N 018-1102-72-0; piercing rod P/N 012-1080-00-0 | Hale Products Inc. (26840) Naval Inventory Control Point (03950) | |
| 544052 | 2915-00-911-4873 | Tube Assy, Fuel | III End Item Identification: TF33-P3/11A aircraft engine General Characteristics Item Description: Fuel line assy to fuel control | United Technologies Corporation (77445) | |
| 544056 | 2915-00-908-6967 | Tube Assy, Fuel, Uppe | United Technologies Corporation (77445) | ||
| 54411-01 5441101 | 2915-00-725-7106 | Filter, Fuel, Servo | General Characteristics Item Description: Cres, twill weave mesh, 62 micron absolute filtration rating, 70 phr rated flow W/ JP-4 fuel, 1.120 in. lg by 0.550 in. dia O/a dim. | 3M Purification Inc. (15472) | |
| 544133 | 2915-00-654-2747 | Nut and Insert, Retaining | III End Item Identification: Control assembly, afterburner, fuel, engine, J79, turbojet aircraft General Characteristics Item Description: Assemble inserts with wet ams 3110 zinc chromate primer, assemble inserts 0.100 in. min below mounting surface, inserts must not protrude beyond back surface | Hamilton Sundstrand Corporation (13983,73030) | |
| 544180 | 2915-00-084-3951 | Seal, cam, Guide Tappet | General Characteristics Item Description: Aluminum alloy AMS4150, 1.4993 in. min, 1.4995 in. max dia, 0.62 in. lg | Hamilton Sundstrand Corporation (73030) | |
| 544190 | 2915-00-979-6372 | Cover, Adjustment | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | ||
| 544227 | 2915-00-797-0029 | Body and Screen, Filter | III End Item Identification: 29158467128 General Characteristics Item Description: Heat treat MIL-H-6875, per HS461 | Hamilton Sundstrand Corporation (73030) | |
| 544242 | 2915-00-084-3952 | Bracket, Spring | General Characteristics Item Description: Steel QQ-S-763 class 304, 0.48 in. lg, 0.160 in. W | Hamilton Sundstrand Corporation (73030) Reliable Manufacturing Company (2U656) | |
| 544247 | 2915-00-084-8128 | Roller, Push bar | General Characteristics Item Description: Cres, AMS5630, 560.0 min, 653 .0 max V hardness, 0.380 in. O/a lg, 0.187 in. min, 0.188 in. max O/a dia, both ends 0.062 in. dia, 0.105 in. lg | Hamilton Sundstrand Corporation (73030) | |
| 54427-01 5442701 | 2915-01-059-1009 | Filter Element, Fluid | 3M Purification Inc. (15472) | ||
| 544288 | 2915-00-084-8121 | Retainer and Ball, Lever | General Characteristics Item Description: Retainer, cres, QQ-S-763 class 410, 0K580 in. O/a lg, 0.249 in. O/a dia, 0.170 in. dia bore, 0.189 in. dia counterbore, ball, cres, AMS7445, 58 min, 64 max rockwell C scale hardness, 0.1875 in. dia | Hamilton Sundstrand Corporation (73030) | |
| 544296 | 2915-00-778-9093 | Governor, Pump, Pressure Regulatin | III End Item Identification: Fuel control P/N 729900, model JFC25-29;TF33 turbo fan aircraft engine III Fsc Application Data: Fuel systems component, turbo fan, aircraft engine III Part Name Assigned By Controlling Agency: Cage and valve, flyball | Hamilton Sundstrand Corporation (73030) | |
| 544316 | 2915-00-971-0256 | Plug, Selector | Hamilton Sundstrand Corporation (73030) | ||
| 544317 | 2915-00-976-9927 | Indicator, Fuel | General Characteristics Item Description: Aluminum alloy, AMS4026, comp 6061, 0.595 in. nom O/a lg, 0.360 in. nom O/a W, 0.400 in. nom O/a H, 1 mtg slot, 0.150 in. nom W slot, 0.190 in. nom lg slot, 0.105 in. nom distance from 1ST end to slot, 2ND end, 1 slot 0.170 in. W terminating in 2 holes 0.060 in. nom dia, 0.190 in. nom distance from 2ND end to holes, indicator pointer 0.140 in. nom W located between holes, 0.180 in. nom distance from 2ND end to indicator pointer | Hamilton Sundstrand Corporation (73030) |