Aircraft and Missile Prime Movers Engine Fuel System Components: 743933-1, 744500L1, 74467
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 743933-1 7439331 | 2915-01-256-9314 | Disk, Valve | Transdigm Inc. (96124) | ||
| 743933-2 7439332 | 2915-01-256-9314 | Disk, Valve | Transdigm Inc. (96124) | ||
| 743943-1 7439431 | 2915-01-339-8991 | Disk, Valve | Transdigm Inc. (96124) | ||
| 74404 | 2915-00-195-5181 | Nozzle, Fuel Injection | Textron Lycoming Inc. (80254) | ||
| 744108-4 7441084 | 2915-00-094-8548 | Ring Seal Assembly | Grimes Aerospace Company (72914) | ||
| 744311-1 7443111 | 2915-00-148-1893 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine, turboshaft model T58 General Characteristics Item Description: Steel | Hamilton Sundstrand Corporation (73030) | |
| 744317-1 7443171 | 2915-00-169-2907 | Cam, Speed, Servo | III End Item Identification: Aircraft engine model J79 General Characteristics Item Description: Aluminum | Hamilton Sundstrand Corporation (73030) | |
| 744322-1 7443221 | 2915-00-431-8829 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine, aircraft, model T58-GE-10 Reference Number Differentiating Characteristics: As differentiated by source control drawing | Hamilton Sundstrand Corporation (73030) | |
| 744322-2 7443222 | 2915-01-394-2258 | Fuel Control, Emergency, Turbine E | III End Item Identification: Engine model T58 Reference Number Differentiating Characteristics: As differentiated by the source control drawing number | Hamilton Sundstrand Corporation (73030) | |
| 744360-1 7443601 | 2915-00-169-2910 | Follower Assembly, cam | III End Item Identification: Aircraft engine model J79 General Characteristics Item Description: Aluminum | Hamilton Sundstrand Corporation (73030) | |
| 744399-1 7443991 | 2915-00-148-1891 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine, turboshaft model T58 General Characteristics Item Description: Steel Reference Number Differentiating Characteristics: As differentiated by source control drawing 6003T91P08 | Hamilton Sundstrand Corporation (73030) | |
| 744399-3 7443993 | 2915-00-148-1891 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine, turboshaft model T58 General Characteristics Item Description: Steel Reference Number Differentiating Characteristics: As differentiated by source control drawing 6003T91P08 | Hamilton Sundstrand Corporation (73030) | |
| 744500L1 | 2915-00-177-7297 | Fuel Control, Main, Turbine Engine | Reference Number Differentiating Characteristics: Source control dwg no. 701696 fscm 77445 | Hamilton Sundstrand Corporation (73030) | |
| 744500L10 | 2915-00-139-0219 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft engine model J52-P-408 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Hamilton Sundstrand Corporation (73030) | |
| 744500L12 | 2915-00-139-0219 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft engine model J52-P-408 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Hamilton Sundstrand Corporation (73030) | |
| 744500L13 | 2915-00-139-0219 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft engine model J52-P-408 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Hamilton Sundstrand Corporation (73030) | |
| 744500L6 | 2915-00-148-7444 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine model J-52 | Hamilton Sundstrand Corporation (73030) | |
| 744500L8 | 2915-00-139-0219 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft engine model J52-P-408 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Hamilton Sundstrand Corporation (73030) | |
| 7445C | 2915-00-011-1532 | Retainer, Disk | III End Item Identification: Valve, fuel P/NAV2G1112 General Characteristics Item Description: Cres per AISI302 18-8; 0.579 in. dia, 0.120 in. thk; recessed surface 0.453 in. dia one side | ITT Corporation (73760) | |
| 74467 | 2915-00-738-3324 | Cover, Shipping | Goodrich Corporation (11599) |