Aircraft and Missile Prime Movers Engine Fuel System Components: 740141, 74033, 74133
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 740141 | 2915-00-296-6635 | SEAT | Transdigm Inc. (96124) | ||
| 7402 | 2915-00-484-6904 | Piston - Sleeve Ass | Goodrich Corporation (11599) | ||
| 74030 | 2915-00-501-4248 | Cover, Filter | Goodrich Corporation (11599) | ||
| 74033 | 2915-00-731-2468 | Cover and Spring Assembly | General Characteristics Item Description: 0.580 in. id | Goodrich Corporation (11599) | |
| 740332-7 7403327 | 2915-01-340-8501 | Nozzle, Fuel Injection | Hamilton Sundstrand Corporation (73030) | ||
| 7-40531-1 7405311 | 2915-00-151-6293 | Input Control, Fuel | General Characteristics Item Description: 3.350 in. lg | Triumph Controls LLC (78710) | |
| 740783-2 7407832 | 2915-01-089-4154 | Lever, Multiplying | III End Item Identification: T-700TURBINEENGINE | Hamilton Sundstrand Corporation (73030) | |
| 740783-3 7407833 | 2915-01-089-4154 | Lever, Multiplying | III End Item Identification: T-700TURBINEENGINE | Hamilton Sundstrand Corporation (73030) | |
| 740785-2 7407852 | 2915-01-087-4204 | Lever, Sensor | III End Item Identification: UH-60 turbine engine, rotary wing aircraft | General Electric Company (99207) Hamilton Sundstrand Corporation (73030,99167) | |
| 740790-7 7407907 | 2915-01-170-2914 | Link, Anti-Rotation | General Electric Company (99207) Hamilton Sundstrand Corporation (73030,99167) | ||
| 740797-2 7407972 | 2915-01-327-1173 | Piston, Valve | III End Item Identification: F112WR100 engine | Hamilton Sundstrand Corporation (73030) | |
| 740925-2 7409252 | 2915-01-070-2710 | Ball, Valve | III End Item Identification: Fuel control JFC110 F100 engine General Characteristics Item Description: 0.375 in. dia. material: vespel SP-1 | Hamilton Sundstrand Corporation (73030) | |
| 740B-13 740B13 | 2915-00-791-7459 | Cock, Poppet Drain | Material: Aluminum alloy body Style Designator: Angle Valve Operation Method: Manual | Auto-Valve Inc. (91511) | |
| 740B8X | 2915-00-610-8682 | Cock, Poppet Drain | Material: Aluminum alloy body Style Designator: Straight thru Valve Operation Method: Manual | Auto-Valve Inc. (91511) | |
| 741100-101 741100101 | 2915-01-125-7982 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Body assembly aluminum alloy COMP356-TL;TEMPERATURE rating ambient m 65F to P 160 f;operating pressure rating 120 psig;designed for turbine fuel JP-4 or JP-5 per MIL-T-5624 | Transdigm Inc. (96124) | |
| 741100-103 741100103 | 2915-01-152-9641 | Valve, Float, Aircraft Fuel Tank | III End Item Identification: Acft model F-18 General Characteristics Item Description: Body assembly aluminum alloy COMP356-T6; temperature rating ambient M65.0 to P160.0 f; operating pressure rating 120.0 psig; designed for turbine fuel JP-4 or JP-5 per MIL-T-5624 | Transdigm Inc. (96124) | |
| 741100-103A 741100103A | 2915-01-186-7870 | Valve, Float, Aircraft Fuel Tank | End Item Identification: Aircraft model F-18 General Characteristics Item Description: Aluminum body material; 5.310 in. lg; 3.500 in. dia; 0 to 60 psig operating pressure | Transdigm Inc. (96124) | |
| 741100-105 741100105 | 2915-01-454-3062 | Valve, Float, Aircraft Fuel Tank | End Item Identification: F-18 Part Name Assigned BY Controlling Agency: Valve, tank defuel Special Features: Temperatures fluid P225F for 5 min max | Transdigm Inc. (96124) | |
| 741-146 741146 | 2915-00-467-9557 | Collar | Goodrich Control Systems LTD (U4287) Goodrich Control Systems LTD T/A (K1464) | ||
| 74133 | 2915-00-987-2105 | Seat and Pin Assemb | Goodrich Corporation (11599) |