Aircraft and Missile Prime Movers Engine Fuel System Components: 739677-5, 73974, 740139
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 739677-5 7396775 | 2915-01-066-8832 | Housing and Stop, Orifice | III End Item Identification: Acft engine F100, fuel control JFC11O General Characteristics Item Description: Orifice dia. 0.034 in. nom III Fsc Application Data: Acft fuel system | Hamilton Sundstrand Corporation (73030) | |
| 739677-8 7396778 | 2915-01-408-5463 | Housing and Stop, or | Hamilton Sundstrand Corporation (73030) | ||
| 739703-1 7397031 | 2915-00-491-5331 | Valve Assy, Fuel Con | Hamilton Sundstrand Corporation (73030) | ||
| 739713-1 7397131 | 2915-00-485-9788 | Shaft, Power Lever | Hamilton Sundstrand Corporation (73030) | ||
| 739722-1 7397221 | 2915-00-176-3721 | Lever and Roller Assembly, Auxili | General Characteristics Item Description: Lever, cres, HS2076, class 1, condition T600, 45 min, 53 max rockwell C scale hardness, 1.745 in. C to C distance between link and shaft holes, 0.0994 in. min, 0.0999 in. max dia hole on one fork tongue, 0.1011 in. min, 0.1016 in. max dia hole on opposite fork tongue, 0.125 in. min, 0.135 in. max distance between fork inside spread, 0.0103 in. min 0.0133 in. max fork tongue thk, 0.067 in. min, 0.770 in. max offset height, 0.185 in. min, 0.195 in. max distance from link hole center to end, 0.105 in. distance from shaft hole center to end, 0.1095 in. min, 0.1103 in. max dia link end hole, pin, straight headless, cres, ams 5616, 0.310 in. min, 0.320 in. max lg, 0.1000 in. min, 0.1005 in. max dia, 446 min, 513 max vickers hardness, roller, cres, ams 5630, 560 min, 653 max vickers hardness, 0.110 in. lg, 0.251 in. dia, 0.101 in. min, 0.103 in. max dia bore, 16 microinches aa outside surface | Hamilton Sundstrand Corporation (73030) | |
| 739729-1 7397291 | 2915-00-176-3720 | Housing, Fuel Control | III End Item Identification: 29154623228 | Hamilton Sundstrand Corporation (73030) | |
| 739-738-1 7397381 | 2915-00-176-3319 | Cover, Fuel Control | III End Item Identification: Aircraft engine model J79 General Characteristics Item Description: Aluminum | Hamilton Sundstrand Corporation (73030) | |
| 73974 | 2915-00-805-6483 | Gear Assy, Matched s | Goodrich Corporation (11599) | ||
| 739757-2 7397572 | 2915-00-556-0356 | Stop, Fuel Flow | General Characteristics Item Description: Cres, 1.293 in. O/a lg, 1.940 in. dia 0.063 in. lg flange one end, 1.304 in. dia other end | Hamilton Sundstrand Corporation (73030) | |
| 739913-5 7399135 | 2915-01-411-8771 | Control-Sensor, Fuel Flow | Hamilton Sundstrand Corporation (73030) | ||
| 74003 | 2915-00-793-2394 | Retainer, Seal | III End Item Identification: Engine, acft, J69 General Characteristics Item Description: Cres, AMS5610, rockwell hardness RC26-34, 1.850 in. min, 1.860 in. max flange dia, 0.440 in. O/a H, 0.996 in. min, 0.998 in. max body od, 0.145 in. min, 0.155 in. max flange thk | Goodrich Corporation (11599) | |
| 740100 | 2915-00-034-6000 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, aluminum alloy seat seating surface, cres disk seating surface; anodized finish on aluminum alloy parts, passivated finish on cres parts; float data, 2 floats, 25 deg approx effective travel of floats; W/solenoids, 2 solenoids, dc; port data, inlet port, flange type, U/W 2 in. od tube, flange data, 3 in. lg, 3 in. W, W/O raised face, mounting hole data, 4, 1/4-28 unf 3B thd size, spaced 2-3/8 in. by 2-3/8 in. between centers, primary sensing port, thd female type, U/W 1/4 in. od tube, thread data, 7/16-20 thd size, unf, class 3 fit, rh, secondary sensing port, thd female type, U/W 1/4 in. od tube, thread data, 7/16-20 thd size, unf, class 3 fit, rh; mounting data, vertical position, bottom mounted, 12 mtg holes; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-G-5572D, mil, MIL-T-5624G; over-all dimensions, 8-21/32 in. lg, 5-3/8 in. dia | Transdigm Inc. (96124) | |
| 740105 | 2915-00-960-9433 | Body, Lower | Transdigm Inc. (96124) | ||
| 740110 | 2915-00-296-6564 | Poppet | Transdigm Inc. (96124) | ||
| 740112 | 2915-00-939-1543 | Poppet, Secondary, Valve, Fuel Cont | III End Item Identification: C-141 aircraft engine fuel control, P/ns 731700 and 731300 General Characteristics Item Description: Aluminum alloy W/anodized finish, O/a dim. 2.150 in. dia by approx 0.360 in. deep, 1 hole 0.125 in. dia in lower back | Transdigm Inc. (96124) | |
| 740113 | 2915-00-296-6575 | Backer, Diaphragm | Transdigm Inc. (96124) | ||
| 740117 | 2915-00-296-6607 | Diaphragm | Transdigm Inc. (96124) | ||
| 740117-1 7401171 | 2915-00-622-3874 | Diaphragm, Actuator Valve, Special | Transdigm Inc. (96124) | ||
| 740121 | 2915-00-296-6614 | Pin, Orifice | Transdigm Inc. (96124) | ||
| 740139 | 2915-00-437-9414 | Shroud, Valve | III End Item Identification: Valve part no. 731700 aircraft C141 | Transdigm Inc. (96124) |