Aircraft and Missile Prime Movers Engine Fuel System Components: 3802323-RX, 381400-24, 3820790-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3802323-RX 3802323RX | 2915-01-441-7293 | Nozzle, Fuel Injection | Cummins Inc. (15434) | ||
| 380264 | 2915-00-776-0949 | Retainer, Fuel Nozzle | III End Item Identification: Fuel nozzle, part no. 404156, engine, acft, J60 General Characteristics Item Description: Cres, AMS5521 or AMS5551, 0.248 in. min, 0.256 in. max od, 0.041 in. min, 0.063 in. max O/a lg | United Technologies Corporation (77445) | |
| 3802833 | 2915-01-480-3661 | Injector Assembly, Fuel | Cummins Inc. (15434) | ||
| 3803 | 2915-00-166-6500 | Liner, Fuel Pump | General Characteristics Item Description: Steel, 1.625 in. min, 1.626 in. max O/a lg, 1.469 in. id | Goodrich Corporation (11599) | |
| 380312 | 2915-01-160-6390 | Housing, Heater, Fuel | III End Item Identification: Heater 500405, TF33-PW-102 eng General Characteristics Item Description: Stainless steel per AMS5646; 8.47 in. nom lg; mtg flange one end W/10 holes 0.276 - 0.286 in. dia on 5.50 in. bcd; mtg flange other end W/8 holes 0.276 - 0.286 in. dia and 2 holes 250-28UNF-3B thd on 5.50 in. bcd; triangular boss one side of body W/3 mtg holes 3125-24UNF-3B thd; rectangular boss other side of body W/4 mtg holes .250-28UNF-3B thd | United Technologies Corporation (77445) | |
| 380449 | 2915-00-732-1988 | Regulator Assembly | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | ||
| 380912 | 2915-00-611-2045 | Nozzle, Fuel, Turboje | Purolator Products Co. Div. Motor (72850) | ||
| 380990 | 2915-00-767-5194 | Nozzle Assembly, Fuel | III End Item Identification: Engine, acft, J79 | Parker-Hannifin Corporation (09523) | |
| 38-125-12 3812512 | 2915-00-373-6765 | Seal, Face | III End Item Identification: Pump type TPC-22, turbofan engine, model F100 General Characteristics Item Description: Material consists of cres, carbon P-5600 or P-658RC nichols 8474A, backup tfe AMS3842 or AMS3843, operating pressure 0 to 750 psi, temperature range minus 65 degrees F to plus 250 degrees F | Rexnord Industries LLC (91587) | |
| 381300-7 3813007 | 2915-00-132-0933 | Housing Assembly, Submerged Pump | III End Item Identification: Acft submerged fuel pump, F15 acft General Characteristics Item Description: 12.010 in. lg, 11.937 in. W, 7.750 in. H approx O/a dim. | Eaton Industrial Corporation (59875) | |
| 38-131-02 3813102 | 2915-00-373-6391 | Seal, Face | III End Item Identification: Pump type TPC-22, turbofan engine, model F100 General Characteristics Item Description: 0.590 in. min 0.610 in. max W, 1.968 in. min 1.970 in. max O/a dia | Apache Corp. (24981) | |
| 381400-16 38140016 | 2915-01-013-9164 | Pump, Submerged, Aircraft | III End Item Identification: Acft F15 fuel pump General Characteristics Item Description: Designed for partially submerged operation, 1 impeller, 115/200V ac, 400 hz 3 ph 2.8 hp, 70000 phr at 14 psi using JP4 fuel, 13.360 in. lg 4.091 in. largest dia, twist-lock type mounting by insertion into cylindrical housing in fuel tank, W/3 thermal protectors, 5 contact electrical connector mounted in handle III Part Name Assigned By Controlling Agency: Submerged pump subassembly | Eaton Industrial Corporation (59875) | |
| 381400-20 38140020 | 2915-01-035-3791 | Pump, Submerged, Aircraft | Eaton Industrial Corporation (59875) | ||
| 381400-24 38140024 | 2915-01-065-8525 | Pump, Submerged, Aircraft | III End Item Identification: Acft model F-15 III Fsc Application Data: Aircraft engine fuel system III Part Name Assigned By Controlling Agency: Submerged pump subassembly | Eaton Industrial Corporation (59875) | |
| 381715 | 2915-00-960-9507 | Nozzle Assembly, Fuel | III End Item Identification: Engine, aircraft, turbojet model no. J79 | Parker-Hannifin Corporation (09523) | |
| 381824 | 2915-00-933-5426 | Shield, Heat, End, Fuel Nozzle Clus | III End Item Identification: Fuel manifold and fuel nozzle manifold sets, P/ns 657165, 657166 and 657167 General Characteristics Item Description: Material stainless steel, arc shaped, O/a dim. approx 1.050 in. min to 1.070 in. max lg by 0.022 in. min to 0.024 in. max thk W/0.120 in. min to 0.140 in. max radius | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 381MS135P001 | 2915-00-328-3809 | Valve, Fuel Drain | Raytheon Company (49956) Raytheon Electronic Systems Inc. (04164) Raytheon Technical Services Company (3B150) | ||
| 3820071-127 3820071127 | 2915-01-491-9857 | Actuator, Electro-Mechanical, line | Parker Hannifin Corporation (92003) | ||
| 3820789-1 38207891 | 2915-00-757-9153 | Body Assembly, Valve | General Characteristics Item Description: Aluminum alloy, QQ-A-696, class b, 11.688 in. O/a lg, anodize finish | Boeing Company, The (18355,88277) | |
| 3820790-1 38207901 | 2915-00-758-4056 | Valve, Float, Aircraft Fuel Tank | III End Item Identification: Acft, A4, A4B, A4C III Fsc Application Data: Fuel control, engine acft | Boeing Company, The (18355,88277) |