Aircraft and Missile Prime Movers Engine Fuel System Components: 11320-02A1, 113B4647P2, 113B6035P1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 11320-02A1 1132002A1 | 2915-01-429-4978 | Pump, Fuel, jet Engine | Goodrich Corporation (11599) | ||
| 113260 | 2915-00-767-3681 | Bulb and Bellows, Control | III End Item Identification: Fuel control, P/N 37R601909G005, engine, acft, J85 | Robertshaw Tennessee/Cookeville (80439) | |
| 113320A1 | 2915-01-429-4974 | Pump, Fuel, jet Engine | Goodrich Corporation (11599) | ||
| 11-3360-1 1133601 | 2915-01-245-2805 | Parts kit, Actuator Overhaul | III End Item Identification: Electro-mech actuator assy P/N 40575-1 III Functional Description: Overhaul of actuator assy 3360-1 III Reference Data and Literature: T.O.8D1-14-164-3 | Argo-Tech Corporation Costa Mesa (86090) FL Aerospace Corp. (06987) | |
| 113390-01A1 11339001A1 | 2915-01-443-4316 | Pump, Fuel, jet Engine | III End Item Identification: Preprovisioning support navicp is poe Reference Number Differentiating Characteristics: As differentiated by source control drawing | Goodrich Corporation (11599) | |
| 113390-01B1 11339001B1 | 2915-01-563-7038 | Pump, Fuel, jet Engin | Goodrich Corporation (11599) | ||
| 11-341-15 1134115 | 2915-00-449-1893 | Plate | III End Item Identification: Aircraft, model B26 | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (45681) | |
| 11-341-15D17 1134115D17 | 2915-00-449-1893 | Plate | III End Item Identification: Aircraft, model B26 | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (45681) | |
| 11-354-4 113544 | 2915-00-707-5203 | Plunger, Pilot | General Characteristics Item Description: Steel case, used on valve, solenoid, dual, pilot precheck, part no. 14-657-1, F104 aircraft | Parker Hannifin Corporation (92003) | |
| 11-357-1 113571 | 2915-00-585-3652 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, aluminum alloy seat seating surface, nonmetallic composition disk seating surface; anodized finish on aluminum alloy parts; float data, 1 float, 15 deg approx effective travel of float; W/O solenoids; port data, inlet port, thd male, U/W 1/2 in. od tube, thd data, 3/4-16 thd size, unf, class 3A fit, rh, not flared tube end type, not threaded male or female compression end type; mounting data, vertical position, top mounted, 1 mtg hole; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-G-5572 and MIL-T-5624; over-all dim., 2-1/2 in. lg, 2-1/2 in. dia | Parker Hannifin Corporation (92003) | |
| 113860 | 2915-00-795-4054 | Bellows, Sensor, Fuel Control | End Item Identification: Fuel control, P/N 37R601924G003 General Characteristics Item Description: Bellows material, cres or brass, end plates material, cres or brass, 1.605 in. min, 1.615 in. max approx lg | Robertshaw Tennessee/Cookeville (80439) | |
| 113B2552P1 | 2915-00-020-9349 | Ball Joint | Special Features: Hole dia 0.186/0.190 in.;max shank wdth 0.625 in.;unthd ball end:type female, od 0.240/0.245 in., id 0.189/0.190 in., depth 0.189/0.190 in. End Item Identification: Nozzle fuel injection, aircraft engine Style Designator: Single, straight, holed shank | BAE Systems Controls Inc. (89954) | |
| 113B2724G1 | 2915-00-020-6546 | Support, Mounting Arms | General Characteristics Item Description: Maple wood, yellow lacquer per ana bulletin no. 166 color no. 505, 5.801 in. min, 5.811 in. max lg, 0.98 in. min, 1.02 in. max dia | BAE Systems Controls Inc. (89954) General Electric Co. (24446) | |
| 113B2738P1 | 2915-00-955-1023 | Plate, Crank arm | III End Item Identification: Control, nozzle area P/N 512D715P10 | BAE Systems Controls Inc. (89954) General Electric Co. (24446) | |
| 113B2799G1 | 2915-00-911-8677 | Rod and Clevis Assy | BAE Systems Controls Inc. (89954) | ||
| 113B4169G1 | 2915-00-938-4200 | Cam and Clutch Assembly, Fuel Con | III End Item Identification: J79-GE17 aircraft engine fuel system | BAE Systems Controls Inc. (89954) | |
| 113B4386G1 | 2915-00-798-8430 | Plate | BAE Systems Controls Inc. (89954) | ||
| 113B4647P1 | 2915-00-572-5191 | Arm, Crank, jet Nozzle | General Characteristics Item Description: Cres per QQ-S-763, passivate, 0.670 in. min 0.690 in. max lg, 0.270 in. min 0.290 in. max H, 0.170 in. min 0.190 in. max W, two 0.128 in. min 0.132 in. max holes drilled thru entire width 0.330 in. min 0.340 in. max center to center, one 0.125 in. min 0.129 in. max dia hole drilled thru entire length 0.095 in. min 0.105 in. max from top and 0.270 in. min 0.290 in. max from left end, 0.013 in. min 0.019 in. max saw slot cut out 0.270 in. min 0.290 in. max lg | BAE Systems Controls Inc. (89954) | |
| 113B4647P2 | 2915-00-572-5191 | Arm, Crank, jet Nozzle | General Characteristics Item Description: Cres per QQ-S-763, passivate, 0.670 in. min 0.690 in. max lg, 0.270 in. min 0.290 in. max H, 0.170 in. min 0.190 in. max W, two 0.128 in. min 0.132 in. max holes drilled thru entire width 0.330 in. min 0.340 in. max center to center, one 0.125 in. min 0.129 in. max dia hole drilled thru entire length 0.095 in. min 0.105 in. max from top and 0.270 in. min 0.290 in. max from left end, 0.013 in. min 0.019 in. max saw slot cut out 0.270 in. min 0.290 in. max lg | BAE Systems Controls Inc. (89954) | |
| 113B6035P1 | 2915-00-020-9349 | Ball Joint | Special Features: Hole dia 0.186/0.190 in.;max shank wdth 0.625 in.;unthd ball end:type female, od 0.240/0.245 in., id 0.189/0.190 in., depth 0.189/0.190 in. End Item Identification: Nozzle fuel injection, aircraft engine Style Designator: Single, straight, holed shank | BAE Systems Controls Inc. (89954) |