Aircraft and Missile Prime Movers Engine Fuel System Components: 704811-1, 704968-1, 705000
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 704811-1 7048111 | 2915-00-890-7809 | Lever, Speed Adjustment | III End Item Identification: Fuel control, engine acft turboprop, chinook helicopter, T-55-L-11 | Hamilton Sundstrand Corporation (73030) | |
| 704811-2 7048112 | 2915-01-111-0166 | Lever, Speed Adjustm | Hamilton Sundstrand Corporation (73030) | ||
| 704812-1 7048121 | 2915-00-890-7808 | Lever, Turbine Linkage | III End Item Identification: Fuel control, engine acft turboprop, chinook helicopter, T-55-L-11 | Hamilton Sundstrand Corporation (73030) | |
| 704814-2 7048142 | 2915-00-810-5853 | Bracket, Linkage, fue | Hamilton Sundstrand Corporation (73030) | ||
| 704814-3 7048143 | 2915-01-111-0167 | Bracket, Linkage | Hamilton Sundstrand Corporation (73030) | ||
| 704819-1 7048191 | 2915-00-890-7807 | Lever and Roller, Fuel | III End Item Identification: Fuel control, engine acft turboprop, chinook helicopter, T-55-L-11 | Hamilton Sundstrand Corporation (73030) | |
| 704898-1 7048981 | 2915-00-727-9943 | Cover, Valve | General Characteristics Item Description: Aluminum alloy, united acft spec HS2077 or AMS4260, anodized, rockwell hardness rating, RB27-60, 0.622 in. dia first end, 1.520 in dia of flange on second end, 0.860 in. lg | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | |
| 704901-1 7049011 | 2915-00-728-0005 | Cover and Restrictor | General Characteristics Item Description: Aluminum alloy, anodized per MIL-A-8625, type I | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) The Durol Company (7D869) | |
| 704935-2 7049352 | 2915-00-235-4592 | Piston, Servo, Fuel Control | General Characteristics Item Description: Aluminum alloy, AMS4117, 2.193 in. min, 2.203 in. max O/a lg, 1.168 in.min, 1.176 in. max head dia, 0.280 in. head H, 0.8758 in. min, 0.8760 in.max shank dia, 4 ring grooves 0.040 in. min, 0.050 in. max W, 0.028 in. min, 0.038 in. max deep, 1 groove 0.034 in. min, 0.039 in. max W, all grooveslocated on shank | Hamilton Sundstrand Corporation (73030) | |
| 704935-3 7049353 | 2915-01-108-7295 | Piston, Speed, Servo | Hamilton Sundstrand Corporation (73030) | ||
| 704962-1 7049621 | 2915-00-918-6789 | Housing and Insert | Hamilton Sundstrand Corporation (73030) | ||
| 704964-1 7049641 | 2915-00-998-0911 | Lever, Feedback | Hamilton Sundstrand Corporation (73030) | ||
| 704965-1 7049651 | 2915-00-109-8787 | Valve Assy, Fuel | Hamilton Sundstrand Corporation (73030) Ontic Engineering & Manufacturing (45934) | ||
| 704966-1 7049661 | 2915-00-109-8788 | Valve, Fuel, Poppet | Hamilton Sundstrand Corporation (73030) | ||
| 704968-1 7049681 | 2915-00-229-0965 | Sleeve, Valve Guide | III End Item Identification: 29159549585 General Characteristics Item Description: Steel | Hamilton Sundstrand Corporation (73030) | |
| 704969 | 2915-00-718-0927 | Guide, Poppet Valve | Hamilton Sundstrand Corporation (73030) | ||
| 704969-1 7049691 | 2915-00-718-0927 | Guide, Poppet Valve | Hamilton Sundstrand Corporation (73030) | ||
| 704977-1 7049771 | 2915-01-180-6119 | Lever and Bracket, Multiplying | III End Item Identification: Main fuel control 572100, 711286, for TF33-PW-7/-102 acft engine General Characteristics Item Description: Lever, P/N 704976-1, 1.61 in. l by 0.995 in. H, bracket, P/N 572798, must rotate freely after assembled; part of throttle valve assy 704978 | Hamilton Sundstrand Corporation (73030) | |
| 704977-3 7049773 | 2915-01-180-6119 | Lever and Bracket, Multiplying | III End Item Identification: Main fuel control 572100, 711286, for TF33-PW-7/-102 acft engine General Characteristics Item Description: Lever, P/N 704976-1, 1.61 in. l by 0.995 in. H, bracket, P/N 572798, must rotate freely after assembled; part of throttle valve assy 704978 | Ontic Engineering & Manufacturing (45934) | |
| 705000 | 2915-00-968-8538 | Adapter, Fueling and Defueling | General Characteristics Item Description: Operating pressure 0.0 to 60.0 psig, proof pressure 120.0 psig, fueling in-flow 250.0 gpm, 2.5 psi max pressure drop, defueling out-flow 60.0 gpm, 0.45 psi max pressure drop, square shape size 4.719 in. lg by 4.719 in. W, 4 mtg holes size 0.326 in. min to 0.333 in. max dia, used with aircraft fuels and vapor system | Transdigm Inc. (96124) |