Aircraft and Missile Prime Movers Engine Fuel System Components: 23033919, 23037399, 23053835
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 23033919 | 2915-01-166-7834 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23037272 | 2915-01-251-0688 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23037399 | 2915-01-333-1566 | Fuel Control, Main, Turbine Engine | III End Item Identification: T-56 engine General Characteristics Item Description: Digital electronic control; 12.000 in. O/a dia; 3.905 in. H Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Rolls-Royce Corporation (63005) | |
| 23037765 | 2915-01-282-1772 | Fuel Filter | General Characteristics Item Description: Filtration rating in microns 10.0 nominal; general motors corp, allison transmission div engine mdl 250 | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 23039643 | 2915-01-351-4895 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft engine model T56A427 turbo prop | Rolls-Royce Corporation (63005) | |
| 2304-4 23044 | 2915-00-157-1453 | Terminal, Locking | General Characteristics Item Description: Steel, 0.020 in. thk material, 1ST leg, 0.3906 in. nom lg, 0.2812 in. nom W, 0.1406 in. nom end radius, 2ND leg, 0.3124 in. nom lg, 0.1875 in. nom W, 0.09375 in. nom end radius, 1 slotted hole through 1ST leg, 2 holes through 2ND leg | ITW Shakeproof Automotive Products (78189) | |
| 23051436 | 2915-01-406-0187 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23051852 | 2915-01-318-8915 | Control Assembly, Fuel | III End Item Identification: T-56 eng Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Rolls-Royce Corporation (63005) | |
| 23051979 | 2915-01-383-7131 | Fuel Control, Main, Turbine Engine | Honeywell International Inc. (06848) | ||
| 23051984 | 2915-01-477-0998 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23051985 | 2915-01-354-9381 | Fuel Control, Main, Turbine Engine | Special Features: Inconel steel bracket; anti-rotation tang on throttle balance spring assy | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 23051987 | 2915-01-344-1311 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23051988 | 2915-01-344-5084 | Fuel Control, Main, Turbine Engine | Rolls-Royce Corporation (63005) | ||
| 23051990 | 2915-01-354-1832 | Fuel Control, Main, Turbine Engine | General Characteristics Item Description: Model DP-D3; engine application T63-A-700; approximate weight 4-7 lbs.; approximate envelope size 8 in. X 6 in. X 6 in. | Rolls-Royce Corporation (63005) | |
| 23052010 | 2915-00-871-0948 | Element and Stud Assy Fuel Filte | III End Item Identification: Used on CV580 aircraft | PTI Technologies Inc. (05228) Rolls-Royce Corporation (63005) | |
| 23052011 | 2915-01-245-8193 | Filter Element, Fluid | Media for Which Designed: Fuel/oil, hydrocarbon FSC Application Data: Hp fuel filter assy for T56-7/-9/-15 acft engine | Rolls-Royce Corporation (63005) | |
| 23052613 | 2915-01-446-6487 | Regulator, Fuel Flow, Turbo-jet En | III End Item Identification: C130-J acft. | Rolls-Royce Corporation (63005) | |
| 23052613 | 2915-01-475-7917 | Meter, Fuel Flow | III End Item Identification: C13OJ fixed wing aircraft | Allison Transmission Inc. (73342) | |
| 23053217 | 2915-01-372-1805 | Nozzle, Fuel Injection | Rolls-Royce Corporation (63005) | ||
| 23053280 | 2915-01-196-8483 | Diaphragm-Nozzle En | Rolls-Royce Corporation (63005) | ||
| 23053835 | 2915-01-575-2999 | Tube Assembly, Aircraft Engine | III End Item Identification: AE100D3/C-130J engine | Rolls-Royce Corporation (63005) |