Aircraft and Missile Prime Movers Engine Fuel System Components: 6535A, 654055, 658005
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6535A | 2915-00-918-8441 | End Subassy | Michigan Dynamics Inc. (05160) | ||
| 654055 | 2915-01-166-2525 | Fuel Control, Afterburner, Turbine | III End Item Identification: TF30-P-9A aircraft engine Reference Number Differentiating Characteristics: As differentiated by source control dwg no. 2183658 | United Technologies Corporation (77445) | |
| 65422 | 2915-00-177-8247 | Valve, Rocket, By-Pass | III End Item Identification: 29156328972 General Characteristics Item Description: Rubber compound, 0.906 in. O/a dia | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889,59211) | |
| 654233 | 2915-00-821-7954 | Valve, Fuel Pressurizing and Drai | General Characteristics Item Description: For use W/644371 and 674340 nozzle and support assy, 3 hole mtg, 3 port, appl JT8D acft engine | United Technologies Corporation (77445) | |
| 65500-20 6550020 | 2915-01-458-8358 | Nozzle, Fuel Injection | Delavan Inc. (71895) | ||
| 65-5051-1 6550511 | 2915-00-074-0432 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 200 vac, 400 cps, 3 phase, wire lead terminated with 4 male contact electrical connector, 9.312 in. lg, 7.046 in. W, 5.284 in. H, O/a dim., 8 holes 0.316 in. dia evenly spaced around a 7.046 in. by 5.284 in. oval shaped mtg flange, internal or external discharge port for 1.187 in. connection | Nash Engineering Company Inc., The (42280) | |
| 65-5078-1 6550781 | 2915-00-758-8152 | Pump, Submerged, Aircraft | III End Item Identification: KC-135 aircraft, NO.3 cell air refueling body fuel tank installation III Part Name Assigned By Controlling Agency: Pump, fuel transfer III Reference Data and Literature: T.O.1C-135WB-4, figure 62 | Nash Engineering Company Inc., The (42280) | |
| 65-5093-4 6550934 | 2915-00-356-7413 | Pump, Fuel Booster | General Characteristics Item Description: 8.813 in. O/a lg, 4.063 in. O/a dia | Nash Engineering Company Inc., The (42280) | |
| 6-553-9 65539 | 2915-00-349-2238 | Body, Pilot Valve | III End Item Identification: 29153064866 | Parker Hannifin Corporation (92003) | |
| 6-553-9-4 655394 | 2915-00-349-2238 | Body, Pilot Valve | III End Item Identification: 29153064866 | Parker Hannifin Corporation (92003) | |
| 6555028-6 65550286 | 2915-01-498-3206 | Housing, Fuel Pump | III End Item Identification: Cessna citation V aircraft III Part Name Assigned By Controlling Agency: Canister assembly - engine overboard-fuel drain | Cessna Aircraft Company (71379) | |
| 65560-03181-101 6556003181101 | 2915-01-130-2898 | Controller, Fuel Purge | III End Item Identification: Aircraft model H-53 Special Features: Essential to weapon system performance or operation, or the preservation of life or safety of operating personnel Criticality Code Justification: FEAT | Sikorsky Aircraft Corporation (78286) | |
| 656029 | 2915-00-406-2669 | Valve, Fuel, Afterburner | III End Item Identification: Engine, aircraft, model TF30 | United Technologies Corporation (77445) | |
| 65606 | 2915-00-480-8111 | Cable Assy, Amplifie | Page Chester LTD. (81482) | ||
| 6562 | 2915-01-118-9819 | Valve, Fuel Shutoff | III End Item Identification: Boeing acft model 727 General Characteristics Item Description: Motor operated, semi-submerged, U/O tubing instl wing pressure fueling and fuel dump | Argo-Tech Corporation Costa Mesa (86090) | |
| 656338 | 2915-00-195-7408 | Nozzle, Fuel Injection | United Technologies Corporation (77445) | ||
| 657344 | 2915-00-673-8417 | Parts kit, Valve, Cure Date | III End Item Identification: Valve assembly, fuel pump transfer, P/N 247149, engine, J79 General Characteristics Item Description: Consisting of 13 items | United Technologies Corporation (77445) | |
| 65741 | 2915-00-019-2747 | Lever Assy | General Characteristics Item Description: Aluminum | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889,59211) | |
| 657858 | 2915-00-184-5081 | Nozzle Stator, Fuel, Combustion Ch | General Characteristics Item Description: Cobalt alloy, ams 5382, 1.875 & 1.895 in. flange od, 0.045 & 0.055 in. flange thk, 1.760 & 1.780 in. body od, 0.998 & 1.002 in. smallest id, 0.616 & 0.656 in. lg III Fsc Application Data: Engine fuel system, TF30 | United Technologies Corporation (77445) | |
| 658005 | 2915-00-406-8178 | Damper, Fuel | III End Item Identification: Engine, aircraft, model TF30 General Characteristics Item Description: 10.710 in. min 10.730 in. max O/a lg, 1.990 in. min 2.010 in. max O/a dia | United Technologies Corporation (77445) |