Aircraft and Missile Prime Movers Engine Fuel System Components: 691C816P1, 69401-15, 6941
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 691C816P1 | 2915-00-877-4051 | Differential Assy, N | BAE Systems Controls Inc. (89954) General Electric Co. (24446) | ||
| 6920008E4 | 2915-01-541-4255 | Injector Assembly, Fuel | III End Item Identification: Module, compressor; ge F414 400 engine III Part Name Assigned By Controlling Agency: Nozzle, main fuel Engine Model Number for Which Designed: F414-GE-400 | Parker-Hannifin Corporation (09523) | |
| 6920008E5 | 2915-01-541-4220 | Injector Assembly, Fuel | III End Item Identification: Module, compressor; ge F414-400 engine III Part Name Assigned By Controlling Agency: Nozzle, main fuel Engine Model Number for Which Designed: F414-GE-400 | Parker-Hannifin Corporation (09523) | |
| 69-2204 692204 | 2915-00-534-2259 | Restrictor, Fuel Val | The Boeing Company (81205) | ||
| 69241 | 2915-00-715-2852 | Fitting Assy, Valve | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889,59211) | ||
| 692740 | 2915-00-152-1659 | Nozzle and Support Assembly Fuel | III End Item Identification: Aircraft engine model J58 | United Technologies Corporation (77445) | |
| 69294 | 2915-01-302-7990 | Carburetor, Float | Textron Lycoming Inc. (80254) | ||
| 693335 | 2915-01-495-2684 | Motorpump Assembly | III End Item Identification: A328 transport airbus aircraft | Eaton Aerospace LLC (62983) | |
| 69-37791-1 69377911 | 2915-00-480-5300 | Adapter Fuel Pump | General Characteristics Item Description: Material anodized aluminum, lg O/a 3.75 in, internal dia along lg 1.297 in, one end bevelled and grooved for seal W/threads of 1.875-12, octagon shaped wrenching facility between ends of 1.875 in across flats, square shaped plain flange mounting other end 2.5 by 2.5 in, four bolt holes 0.250 in dia 1.812 in ctoc | The Boeing Company (81205) | |
| 69401-15 6940115 | 2915-00-980-9444 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 2.890 in. min, 2.950 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) | |
| 69401-16 6940116 | 2915-00-979-6290 | Support, Spring | Connecticut Spring & Stamping (81753) Hamilton Sundstrand Corporation (73030) | ||
| 69401-18 6940118 | 2915-00-994-4305 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 3.270 in. min, 3.330 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) | |
| 69401-24 6940124 | 2915-00-918-9756 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 4.040 in. min, 4.100 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | |
| 69401-25 6940125 | 2915-00-980-9497 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 4.310 in. min, 4.370 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.0127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | |
| 69401-26 6940126 | 2915-00-979-6291 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 4.550 in. min, 4.610 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) | |
| 69401-32 6940132 | 2915-00-980-9499 | Support, Expansion Spring | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 cond hard, rockwell C scale 38 min hardness, 6.090 in. min, 6.150 in. max lg, 0.0016 in. min, 0.0024 in. max thk matl, 40 min, 60 max deg bend radius cross-section both ends, 0.123 in. min, 0.127 in. max O/a W, tapered 10 min, 20 max deg to 0.050 in. max W both ends | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | |
| 69402-20 6940220 | 2915-00-942-8367 | Spring, Fuel Control | III End Item Identification: TF33 aircraft engine fuel system | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | |
| 6940403E02 | 2915-01-420-6883 | Nozzle, Fuel Injection | Parker-Hannifin Corporation (09523) | ||
| 6940403E1 | 2915-01-420-6883 | Nozzle, Fuel Injection | Parker-Hannifin Corporation (09523) | ||
| 6941 | 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) |