Aircraft and Missile Prime Movers Engine Fuel System Components: 10-20045, 10-20229-1, 102-1046
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 10-20045 1020045 | 2915-00-585-3651 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, cres seat seating surface, aluminum alloy disk seating surface; anodized finish on aluminum alloy parts, passivated finish on cres parts; float data, 2 floats, 30 deg approx effective travel of floats; W/solenoids, 3 solenoids, dc; port data, inlet port, flange type, U/W 2 in. od tube, flange data, 3 in. lg, 3IN. W, W/O raised face, mounting hole data, 4, 17/64 in. dia, spaced 2.400 in. by 2.400 in. between centers, outlet port, plain hole type /irregular shape/; mounting data, vertical position, bottom mounted, 4 mtg holes; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-T-5624G; over-all dimensions, 5.780 in. lg, 4.870 in. W, 7.600 in. H | The Boeing Company (81205) | |
| 10-20045-1 10200451 | 2915-00-585-3651 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, cres seat seating surface, aluminum alloy disk seating surface; anodized finish on aluminum alloy parts, passivated finish on cres parts; float data, 2 floats, 30 deg approx effective travel of floats; W/solenoids, 3 solenoids, dc; port data, inlet port, flange type, U/W 2 in. od tube, flange data, 3 in. lg, 3IN. W, W/O raised face, mounting hole data, 4, 17/64 in. dia, spaced 2.400 in. by 2.400 in. between centers, outlet port, plain hole type /irregular shape/; mounting data, vertical position, bottom mounted, 4 mtg holes; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-T-5624G; over-all dimensions, 5.780 in. lg, 4.870 in. W, 7.600 in. H | The Boeing Company (81205) | |
| 10-20045-1 10200451 | 2915-00-691-1580 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, steel seat seating surface, aluminum alloy disk seating surface; anodized finish on aluminum alloy parts, passivated finish on steel parts; float data, 2 floats, 20 deg approx effective travel of floats; W/solenoids, 3, dc; port data, inlet port, flange type, U/W 2 in. od tube, flange data, 3 in. lg, 3 in. W, mtg hole data, 4, 0.266 in. dia, spaced 2.40 in. by 2.40 in. between centers, outlet port, plain hole type; mtg data, vertical position, top mtd, 4 mtg holes; fuel data, rated for specific grades of aircraft fuels, spec data, mil, MIL-F-5624C; O/a dim., 5.700 in. lg, 5.375 in. W, 7.860 in. H | The Boeing Company (81205) | |
| 10-20048 1020048 | 2915-00-658-9967 | Valve Assembly, Fuel Check | III End Item Identification: Plumbing installation, fuel system, boeing airplane co pwg no 25-4416, B52 aircraft General Characteristics Item Description: Aluminum alloy and steel 8.13 in. O/a lg, 3.31 in. O/a W, 3.19 in. O/a H, ambient temperature M65 deg F to P160 deg F | The Boeing Company (81205,82918) | |
| 10-20048-1 10200481 | 2915-00-658-9968 | Valve Assembly, Fuel Check | III End Item Identification: Plumbing installation fuel system, boeing dwg no 25-4416, B52 aircraft General Characteristics Item Description: 8.20 in O/a lg, 3.19 in. od | The Boeing Company (81205,82918) | |
| 10-20048-501 1020048501 | 2915-01-520-7168 | Valve, Fuel System | III End Item Identification: B-52 aircraft Special Features: Nha PN:35-18384 Media for Which Designed: Fuel, jet | The Boeing Company (81205) | |
| 10-20049-505 1020049505 | 2915-00-788-6900 | Parts kit, Fuel Pump | III End Item Identification: 29157891781, 29158930389 General Characteristics Item Description: Consist of 3 items Special Features: Formerly cure date pump | The Boeing Company (81205,82918) | |
| 102-008 102008 | 2915-00-211-4981 | Body Assembly, Pump, | III End Item Identification: 43200508615 General Characteristics Item Description: Steel | Hamilton Sundstrand Corporation (99167) | |
| 10-20229-1 10202291 | 2915-00-627-4168 | Valve, Gate, Motor Ac | The Boeing Company (81205,82918) | ||
| 10-20229-3 10202293 | 2915-00-778-8024 | Fitting, Gate Shut off | III End Item Identification: Fuel valve, P/N 25-4416, acft, B52 | The Boeing Company (81205,82918) | |
| 10-20229-4 10202294 | 2915-00-715-5522 | Actuator, Electro-Mechanical, Rota | III Fsc Application Data: Fuel valve, engine acft Body Diameter: 3.784 inches nominal Body Length: 5.727 inches nominal | The Boeing Company (81205) | |
| 10-20229-502 1020229502 | 2915-00-778-8024 | Fitting, Gate Shut off | III End Item Identification: Fuel valve, P/N 25-4416, acft, B52 | The Boeing Company (81205) | |
| 10-20279 1020279 | 2915-00-790-0277 | Heater Assembly, fue | III End Item Identification: Heater instl, P/N 35-7376, acft, B52 General Characteristics Item Description: 12.250 in. lg | The Boeing Company (81205,82918) | |
| 10-20279-1 10202791 | 2915-00-654-3742 | No Item Name Available | III End Item Identification: Heater installation, fuel, engine, boeing dwg no 35-7376, B52 aircraft General Characteristics Item Description: 12.00 in. max O/a lg, 4.51 in. max O/a W, 7.800 in. height | The Boeing Company (81205,82918) | |
| 102,036-14 10203614 | 2915-01-312-3883 | Valve, Fuel-Air Mixture Control, a | Vapor Corp. (80234) | ||
| 1020E1001 | 2915-01-525-2238 | Ejector, Transfer | Allen Aircraft Products Inc. (82829) | ||
| 1020E102 | 2915-01-507-6071 | Ejector, Transfer | Allen Aircraft Products Inc. (82829) | ||
| 102-10003 10210003 | 2915-00-310-6303 | Body Assembly, Fuel | III End Item Identification: Fuel pump part no. 022136 | Hamilton Sundstrand Corporation (73030,99167) | |
| 102-10020 10210020 | 2915-00-314-9648 | Body Assembly, Fuel | Hamilton Sundstrand Corporation (99167) | ||
| 102-1011 1021011 | 2915-00-754-4830 | Diaphragm Assy, Pump | Hamilton Sundstrand Corporation (99167) | ||
| 102-1046 1021046 | 2915-00-940-9906 | Spool and Sleeve Assembly, Fuel C | III End Item Identification: TF30 aircraft engine fuel pump, axial piston, P/N 024692-102-14 | Hamilton Sundstrand Corporation (99167) |