Aircraft and Missile Prime Movers Engine Fuel System Components: 738116-3, 738265-3, 73899
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 738116-3 7381163 | 2915-01-328-5121 | Turbine Rotor, Fuel Pump | III End Item Identification: F100PW0229 augmentor fuel pump | Hamilton Sundstrand Corporation (73030) | |
| 738163-1 7381631 | 2915-00-371-2310 | Plate, Retaining | III End Item Identification: Pump, fuel augmentor model TPC-22 General Characteristics Item Description: Cres AMS5512 per HS178, 1.460 in. min, 1.470 in. max aperture dia, 0.073 in. min, 0.087 in. max thk, 3 holes 0.299 in. min, 0.309 in. max dia equally spaced | Hamilton Sundstrand Corporation (73030) | |
| 738164-1 7381641 | 2915-00-371-2330 | Link, Actuator, Fuel Pump | III End Item Identification: Fuel pump, augmentor, model no. TPC-22, engine, F100, aircraft, F15 General Characteristics Item Description: Cres per AMS5735, heat treatment per chandler evans spec no. HS461, 24 to 37 hardness rating, rockwell C scale, 1.10 in O/a lg, 0.60 in. W | Hamilton Sundstrand Corporation (73030) | |
| 7382248-503 7382248503 | 2915-00-585-3815 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, aluminum alloy float, corrosion resisting steel seat seating surface, corrosion resisting steel disk seating surface; anodized finish on aluminum alloy parts passivated finish on corrosion resisting steel parts; float data, 1 float, effective travel of float not rated; port data, inlet port, flange type, U/W 1 in. od tube, flange data, 1-5/16 in. W, mtg hole data, 4, 1/4-28 unf 3B thd size, spaced 1.312 in. by 1.312 in. between centers; mtg data, vertical position, top mounted, 4 mtg holes; fuel data, rated for specific grades of aircraft fuel, spec data, mil, MIL-F-5572, MIL-F-5616 and MIL-F-5624; over-all dim., 4-23/64 in. lg, 2-15/16 in. W, 2-7/8 in. H | Boeing Company, The (18355,88277) | |
| 7382248-507 7382248507 | 2915-00-605-2027 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, cres seat seating surface, cres disk seating surface; anodized finish on aluminum alloy parts, passivated finish on cres parts; float data, 2 floats, 20 deg approx effective travel of floats; W/O solenoids; port data, inlet port, flange type, 1-25/32 in. nom dia, flange data, 3 in. lg, 3 in. W, W/O raised face, mounting hole data, 4, 1/4-28 unf 3B thd size, spaced 2-3/8 in. by 2-3/8 in. between centers; mounting data, vertical position, top mounted 4 mtg holes; fuel data, rated for specific grades of aircraft fuels, specification data, mil, MIL-G-5572D, mil, MIL-T-5624G; over-all dimensions, 5-1/32 in. lg, 5-1/16 in. dia | Boeing Company, The (18355,88277) | |
| 738228-1 7382281 | 2915-00-371-2377 | Disc, Valve, Butterfly, Fuel Pump | III End Item Identification: Fuel pump, augmentor, model no TPC-22, engine, F100, aircraft, F-15 General Characteristics Item Description: Cres per AMS5382, rockwell C hardness 40.0 max, 1.850 in. min, 2.050 in. max approxiate lg, 1.272 in. min, 1.274 in. max od | Hamilton Sundstrand Corporation (73030) | |
| 738265-3 7382653 | 2915-00-371-2311 | Filter, Diffuser, Fuel Pump | III End Item Identification: Pump, fuel augmentor model TPC-22 General Characteristics Item Description: 1.548 in. min, 1.550 in. max O/a dia, on first end, 1.454 in. min, 1.456 in. max id, 1.048 in. min, 1.050 in. max O/a dia on second end, 0.948 in. min, 0.951 in. max id on, second end | Hamilton Sundstrand Corporation (73030) | |
| 738270-1 7382701 | 2915-00-373-6494 | Retainer, Ball | III End Item Identification: Fuel pump type TPC-22, turbofan engine model F100 | Hamilton Sundstrand Corporation (73030) | |
| 7382989-501 7382989501 | 2915-00-618-5824 | Switch, Liquid Level | III Fsc Application Data: Engine fuel system, aircraft Special Features: Float down Overall Length: 3.833 inches nominal | Boeing Company, The (88277) | |
| 738307 | 2915-01-009-2146 | Fuel Control, Main, Turbine Engine | United Technologies Corporation (77445) | ||
| 738319-4 7383194 | 2915-00-371-2306 | Housing and Valve Assembly, Fuel | III End Item Identification: Fuel pump, augmentor, model no. TCP-22, engine, F100, aircraft, F15 | Hamilton Sundstrand Corporation (73030) | |
| 7383547-501 7383547501 | 2915-00-215-0792 | Valve Assembly, Fuel Shut off | III End Item Identification: 43206501723 General Characteristics Item Description: Steel, 3.750 in. O/a dia | Boeing Company, The (18355,88277) | |
| 73850 | 2915-00-791-5762 | Housing and Drive Assembly | III End Item Identification: Engine, acft, J75 General Characteristics Item Description: Aluminum alloy, anodize per AMS2470, consist of 2 items | Goodrich Corporation (11599) | |
| 738518 | 2915-01-175-8471 | Stem and Sleeve Assembly | III End Item Identification: Engine model F-104 | Hamilton Sundstrand Corporation (99167) | |
| 73869 | 2915-00-898-7601 | Parts kit, Fuel Control | Special Features: C/O 25 items End Item Identification: 2915004399314 | Goodrich Corporation (11599) | |
| 73871 | 2915-00-784-4739 | Parts kit, Fuel Control | End Item Identification: Acft eng, J-69 | Goodrich Corporation (11599) | |
| 73875 | 2915-00-992-1133 | Gear and Shaft Asse | Goodrich Control Systems GMBH (C0297) Goodrich Corporation (11599) | ||
| 73877 | 2915-00-992-1134 | Gear and Shaft Assembly | General Characteristics Item Description: U/0 T53 engine, TA-2 fuel regulator, dmwr 55-2915-322, nha pump 85634, nsn 4320-01-200-6685 | Goodrich Control Systems GMBH (C0297) Goodrich Corporation (11599) | |
| 73879 | 2915-00-992-1135 | Shaft and Ring, Fuel | Goodrich Corporation (11599) | ||
| 73899 | 2915-00-071-0846 | Carburetor, Float | Draft Direction: UP Barrel Quantity: 2 Mounting Hole Quantity: 4 | Textron Lycoming Inc. (80254) |