Aircraft and Missile Prime Movers Engine Fuel System Components: 648874, 650400, 650857CL3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 648874 | 2915-00-124-3663 | Nozzle, Fuel, Afterburner Igniter | III End Item Identification: Engine, aircraft, model no. TF30 General Characteristics Item Description: Nickel alloy AMS5754, 6.582 in. lg | United Technologies Corporation (77445) | |
| 649052A1-1 649052A11 | 2915-01-415-1689 | Injector Assembly, Fuel | III End Item Identification: Beechcraft bonanza and beechcraft baron acft | Teledyne Industries Inc. (28839) | |
| 649052A1-1R 649052A11R | 2915-01-415-1689 | Injector Assembly, Fuel | III End Item Identification: Beechcraft bonanza and beechcraft baron acft | Teledyne Industries Inc. (28839) | |
| 6493 | 2915-00-918-8450 | Cup, Seal Retaining | Michigan Dynamics Inc. (05160) | ||
| 649323-1 6493231 | 2915-01-392-5853 | Housing, Fuel Pump | III Part Name Assigned By Controlling Agency: Vapor separator and relief valve housing Media for Which Designed: Fuel, aviation Usage Design: Aircraft engine accessory | L-3 Communications Corporation (02978) | |
| 649806 | 2915-00-070-6190 | Diaphragm, Actuator Valve, Special | Fsc Application Data: Valve, butterfly | Goodrich Corporation (99551) Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889) | |
| 649813 | 2915-00-075-3873 | Disk, Valve | Material: Steel comp 420 Fsc Application Data: Valve, butterfly Material Document and Classification: Ams 5621 assn std single material response | Goodrich Corporation (99551) Parker-Hannifin Corporation (3H889,59211) Superior Metal Mfg Inc. (67459) | |
| 649814 | 2915-00-406-8182 | Housing, Valve, Afterburner | III End Item Identification: Engine, aircraft, model TF30 | United Technologies Corporation (77445) | |
| 64A74003 | 2915-00-071-6038 | Cup, Diaphragm, Fuel | General Characteristics Item Description: Steel AMS5613, rockwell C 26-32, 0.875 in. dia, 0.122 in. min, 0.128 in. max lg, 0.190 in. min, 0.200 in. max id one side, 0.600 in. min, 0.620 in. max id 0.075 in. deep | Goodrich Corporation (11599) | |
| 6500 | 2915-00-486-3886 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 24V dc 11 amps 1800 phr at 18 psi 6500 rpm, 9.203 in. lg 5.687 in. W 4.452 in. H O/a dim., 16 holes 0.218 in. dia equally spaced around a mtg flange on a 3.687 in. dia circle, 3 contact ms type electrical connector, 90 deg ell 1-1/4 in. hose type discharge connection | Eaton Industrial Corporation (59875) | |
| 650036 | 2915-01-149-8811 | Fuel Control, Main, Turbine Engine | United Technologies Corporation (77445) | ||
| 65010-2 650102 | 2915-00-031-5305 | Switch, Liquid Level | III Fsc Application Data: Switch, float, liquid, engine, aircraft Overall Length: 8.370 inches nominal Overall Diameter: 2.930 inches nominal | Grimes Aerospace Company (72914) | |
| 6501-5 65015 | 2915-01-518-4545 | Actuator, Electro-Mechanical, Rota | III End Item Identification: C-135 III Part Name Assigned By Controlling Agency: Actuator, fuel valve Body Length: 5.160 inches minimum and 5.370 inches maximum | Sota Corporation (61604) | |
| 650400 | 2915-00-738-5181 | Filter Element, Fluid | III Fsc Application Data: Filter, fluid, pressure, engine fuel system, acft Material: Any acceptable container/cartridge paper filtering medium any acceptable seal Media for Which Designed: Fuel/oil, hydrocarbon | Michigan Dynamics Inc. (05160) | |
| 65044-1 650441 | 2915-00-124-3676 | Cap, Strainer, Sediment | III End Item Identification: Strainer, sediment part no. 6658043 General Characteristics Item Description: Aluminum alloy type 356-T6, 3.625 in. dia, 1.625 in. lg | Arvinmeritor Inc. (64829) PTI Technologies Inc. (05228) | |
| 65045 | 2915-00-018-5035 | Rod, Retaining | General Characteristics Item Description: Steel QQ-S-633 type B1113, cadmium plated; 6.125 in. lg O/a; flat end to collar 2.344 in. lg, hole thru 0.093 in. dia, 0.080 in. cen-to-end; rounded end threaded 0.250 in. from tip; both ends 0.312-24UNF-3A thd | Arvinmeritor Inc. (64829) PTI Technologies Inc. (05228) | |
| 650857 | 2915-01-163-1612 | Ring, Locking, Fuel Manifold | III End Item Identification: TF33-PW-102 aircraft engine General Characteristics Item Description: Nickle alloy per AMS5663; 0.371 -0.394 in. W O/a; flange 0.080 in. nom thk, 0.825 - 0.850 in. dia W/cutout 0.130 X 0.230 in. nom; 0.462 in. nom od, 0.294 in. nom id III Functional Description: Used on nozzle cluster | United Technologies Corporation (77445) | |
| 650857CL1 | 2915-01-162-3174 | Ring, Locking, Fuel Manifold | III End Item Identification: TF33-PW-102 aircraft engine General Characteristics Item Description: Nickle alloy per AMS5663; 0.368 -0.391 in. W O/a; flange 0.080 in. nom thk, 0.825 - 0.850 in. dia W/cutout 0.130 X 0.230 in. nom; 0.462 in. nom od, 0.294 in. nom id III Functional Description: Used on nozzle cluster | United Technologies Corporation (77445) | |
| 650857CL2 | 2915-01-163-1612 | Ring, Locking, Fuel Manifold | III End Item Identification: TF33-PW-102 aircraft engine General Characteristics Item Description: Nickle alloy per AMS5663; 0.371 -0.394 in. W O/a; flange 0.080 in. nom thk, 0.825 - 0.850 in. dia W/cutout 0.130 X 0.230 in. nom; 0.462 in. nom od, 0.294 in. nom id III Functional Description: Used on nozzle cluster | United Technologies Corporation (77445) | |
| 650857CL3 | 2915-01-162-3175 | Ring, Locking, Fuel Manifold | III End Item Identification: TF33-PW-102 aircraft engine General Characteristics Item Description: Nickle alloy per AMS5663; 0.374 -0.397 in. W O/a; flange 0.080 in. nom thk, 0.825 - 0.850 in. dia W/cutout 0.130 X 0.230 in. nom; 0.462 in. nom od, 0.294 in. nom id III Functional Description: Used on nozzle cluster | United Technologies Corporation (77445) |