Aircraft and Missile Prime Movers Engine Fuel System Components: 752078-1, 75284-1, 753216
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 752078-1 7520781 | 2915-01-013-9147 | Plate, Fuel Adjustment | III End Item Identification: Acft fuel CONTROL2915001260160 General Characteristics Item Description: Cres, 0.600 in. lg 0.740 in. longest radius, serrated face 24 teeth | Hamilton Sundstrand Corporation (73030) | |
| 75208 | 2915-00-953-4967 | Fitting and Stopcock, Seal Assemb | III End Item Identification: Fuel control P/N 81700C2 | Goodrich Control Systems GMBH (C0297) Goodrich Corporation (11599) | |
| 752080-1 7520801 | 2915-01-013-9148 | Plate Assembly, Fuel Control | III End Item Identification: Acft fuel CONTROL2915001260160 General Characteristics Item Description: C/O spring loaded stop shaft, pins, rivet and irregular shaped plate | Hamilton Sundstrand Corporation (73030) | |
| 752086-1 7520861 | 2915-01-013-9151 | Plug, Fuel Control | III End Item Identification: Acft fuel CONTROL2915001260160 General Characteristics Item Description: Aluminum alloy ams 4117, 0.414 in. lg 0.420 in. dia one end, 0.622 in. dia other end, 0.770 in. dia 0.034 in. thk flange 0.100 in. from first end | Hamilton Sundstrand Corporation (73030) | |
| 752087-1 7520871 | 2915-01-013-9150 | Stop, Part Power | III End Item Identification: Acft fuel CONTROL2915001260160 General Characteristics Item Description: Cres, 2.160 in. lg, 0.56 in. W, 0.560 in. H approx O/a dim., includes shaft and ell shaped block | Hamilton Sundstrand Corporation (73030) | |
| 752100-1 7521001 | 2915-00-126-0160 | Fuel Control, Main, Turbine Engine | Hamilton Sundstrand Corporation (73030) | ||
| 75223 | 2915-00-285-6646 | Follower Assembly, P, Piston | General Characteristics Item Description: Arm, cres, AMS5350, chrome plate, AMS2406, 26 min, 34 max rockwell chardness, 1.8745 in. min, 1.8755 in. max effective lg, 0.1250 in. min, 0.1255 in. max hole through each end on both sides, one end 0.940 in. W, 0.626 in. min, 0.632 in. max fork spread, opposite end, 0.630 in. W, 0.377 in. min, 0.383 in. max fork spread, roller, rocker arm, cam follower, cres, AMS5616, immunized, 0.3748 in. min, 0.3750 in. max od, 0.1252 in. min, 0.1257 in. max id, 0.154 in. min, 0.158 in. max W, shaft, straight, cres, AMS5616, 42 min, 50 max rockwell C hardness, immunized, 0.660 in. lg, 0.1246 in. min, 0.1249 in. max dia, one hole 0.040 in. min, 0.050 in. maxlocated 0.090 in. from one end, spacer, sleeve, cress, AMS5640, immunized, 75 min, 100 max rockwell b hardness, 0.185 in. min, 0.195 in. max od, 0.125 in. min, 0.127 in. max id, 0.053 in. min, 0.059 in. max thk | Goodrich Corporation (11599) | |
| 7523-1 75231 | 2915-01-527-8356 | Fuel Flow Switch Assy | Overall Width: 4.980 inches minimum and 5.020 inches maximum End Item Identification: B-52 aircraft Part Name Assigned BY Controlling Agency: Fuel flow switch assembly, -1 configuration | ITT Corporation (73760) Sota Corporation (61604) | |
| 7523-2 75232 | 2915-01-527-8364 | Fuel Flow Switch Assy | III End Item Identification: B-52 aircraft III Part Name Assigned By Controlling Agency: Fuel flow switch assembly, -2 configuration Overall Length: 5.980 inches minimum and 6.020 inches maximum | ITT Corporation (73760) Sota Corporation (61604) | |
| 7523-3 75233 | 2915-01-527-8382 | Fuel Flow Switch Assy | Overall Width: 4.480 inches minimum and 4.520 inches maximum End Item Identification: B-52 aircraft Part Name Assigned BY Controlling Agency: Fuel flow switch assembly, -3 configuration | ITT Corporation (73760) Sota Corporation (61604) | |
| 75233 | 2915-01-084-6742 | Housing, Fuel Pump | III End Item Identification: TF-33 engine Special Features: Used on two-stage pump models 9455-A15/-A17, 9470-A15/-A17, 9478-A12/A14 | Goodrich Corporation (11599) | |
| 75247 | 2915-01-109-5993 | Pump, Fuel, cam Actuated | Textron Lycoming Inc. (80254) | ||
| 75284-1 752841 | 2915-01-220-7431 | Tank Baffle Assembly | Naval Air Depot (91145) | ||
| 75286-5 752865 | 2915-01-469-6202 | No Item Name Available | Senior Operations LLC (07649) | ||
| 7528W25G700 | 2915-01-131-4530 | Shell Assembly | III End Item Identification: Jet engine model F404 | Ametek Inc. (97424) | |
| 75290-04 7529004 | 2915-01-466-4389 | Lever, cap, Assembly | III End Item Identification: Power unit, front | Parker-Hannifin Corporation (09990) | |
| 753198 | 2915-01-114-3502 | Nozzle and Support Assembly | III End Item Identification: TF30-P-3 aircraft engine III Fsc Application Data: Acft eng fuel system components | United Technologies Corporation (77445) | |
| 753199 | 2915-01-234-0731 | Nozzle and Support Assembly | III End Item Identification: TF30-P-3/-103 acft engine General Characteristics Item Description: Incl support, 2177709; 4 ea nozzle lock 590916, nut 664829, nozzle assy 568700, seal 734746 | United Technologies Corporation (77445) | |
| 753215 | 2915-01-234-0733 | Nozzle and Support Assembly | III End Item Identification: TF30-P-7/-107, -9/-109 acft eng General Characteristics Item Description: Incl support 2177708; 4 ea nozzle lock 590916, nut 664829, nozzle assy 568705, seal 734746 | United Technologies Corporation (77445) | |
| 753216 | 2915-01-020-7923 | Support, Fuel Nozzle | III End Item Identification: Engine model TF30 | United Technologies Corporation (77445) |