NSN 2915-01-251-4453
Part Details | JET ENGINE FUEL PUMP
2915-01-251-4453 A device specifically designed to deliver fuel to a jet engine. The device may be of single/multistage and positive/nonpositive displacement design. It mounts on a jet engine accessory drive case or on the fuel control and is driven by the engine. Excludes all pumps not specifically designed to be used on a jet engine.
Alternate Parts: 02469211901, 024692-119-01, 02469211801, 024692-118-01, 02469211418, 024692-114-18, 02469211218, 024692-112-18, 02469211118, 024692-111-18, 02469211018, 024692-110-18, 02469210918, 024692-109-18, 02469210618, 024692-106-18, 2186906, 2183963, 758773, 715112, 626011, 563146, 2915-01-251-4453, 01-251-4453, 2915012514453, 012514453
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 29 | MAR 19, 1987 | 01-251-4453 | 32360 ( PUMP, FUEL, JET ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2915-01-251-4453
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 024692-119-01 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-118-01 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-114-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-112-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-111-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-110-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-109-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 024692-106-18 | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 2186906 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 2183963 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 758773 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 715112 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 626011 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 563146 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2915-01-251-4453
| Characteristic | Specifications |
|---|---|
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DWG NO. 2186906 |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| FUNCTIONAL DESCRIPTION | AXIAL PISTON PUMP,SUPPLIES HIGH PRESSURE HYDRAULIC POWER RQRD TO ACTUATE ENG SYSTEMS USING FUEL AS HYDRAULIC FLUID |