Aircraft and Missile Prime Movers Engine Fuel System Components: 492953, 49447, 49474
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 492953 | 2915-00-942-5279 | Seat Assembly, Afterburner Ignite | III End Item Identification: TF30-P-1 aircraft engine fuel control, P/N 531874 General Characteristics Item Description: Rockwell-C 35 to 40 hardness, approx 2.146 in. min to 2.153 in. max O/a lg by approx 1.024 in. min to 1.068 in. max O/a dia, includes P/ns 492899 and 492952 | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 492976 | 2915-00-942-5280 | Valve, Fuel Check Afterburner Ign | III End Item Identification: TF30-P-1 aircraft engine fuel control General Characteristics Item Description: Ams 5643 stainless steel W/rockwell-C 40 to 48 hardness, O/a dim. 0.488 in. min to 0.489 in. max by 1.000 in. min to 1.030 in max lg, right end 0.300 in. min to 0.320 in. max dia and left end 0.189 in.min to 0.190 in. max dia W/taper to flat end, 6 holes 0.111 in. min to 0.121 in. max dia equally spaced thru side | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 492986 | 2915-00-940-9893 | Tube, Transfer, Fuel Control | III End Item Identification: TF-30-P-1 aircraft fuel control General Characteristics Item Description: Material steel, O/a dim. 0.2347 in. min to 0.2352 in. max dia by 0.180 in. min to 0.190 in. max lg, 0.186 in. min to 0.190 in. max inside dia | United Technologies Corporation (77445) | |
| 493219 | 2915-00-688-9489 | Sleeve, Joint, Heater Support | General Characteristics Item Description: Stainless steel per AMS5613, 30 to 38 hardness rating, rockwell C scale, 0.885 in. min, 0.905 in. max O/a lg, 0.365 in. min, 0.367 in. max body id, 0.090 in. min, 0.110 in. max dia thr 6 holes equally spaced within 0.005R of true position | United Technologies Corporation (77445) | |
| 493221 | 2915-00-688-9490 | Guide, Fuel Heater | III End Item Identification: Heater assembly, fuel, P/N 493224, engine, J60 General Characteristics Item Description: Stainless steel per AMS5613, 30 to 38 hardness rating, rockwell C scale, 0.945 in. min, 0.975 in. max lg, 0.279 in. min, 0.281 in. max od first end, 0.250 in. min, 0.254 in. max dia second end, 0.572 in. W, 0.505 in. H, 0.045 in. thk O/a flange | United Technologies Corporation (77445) | |
| 493622 | 2915-01-160-6391 | Bracket, Heater, Fuel | III End Item Identification: Heater, P/N 500405, for TF33-PW-102 aircraft engine General Characteristics Item Description: Stainless steel per AMS5504; 4.30 in. lg. W/3 mtg holes 0.276 - 0.286 in. dia; 90 deg angle 0.950 in. W, W/mtg hole 0.264 - 0.268 in. dia, 1.50 in. lg tapering to 0.220 in. W. | United Technologies Corporation (52661,77445) | |
| 493629 | 2915-00-759-9261 | Support, Heater, Fuel | III End Item Identification: Heater assembly, fuel de-icing, engine, acft, TF33 | Aero Components Inc. (59213) Kent Associates Inc. (8R034) Monroe Machined Products Inc. (7F311) Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) W P E Inc. (5N444) Wesco Industries Inc. (1JN57) | |
| 4937065 | 2915-01-585-6781 | Injector Assembly, Fuel | Part Name Assigned BY Controlling Agency: Engine parts injector assy. | Cummins Inc. (15434) | |
| 4939061 | 2915-01-556-4392 | Injector Assembly, Fuel | END Item Identification: Pandur ii diesel engine | Cummins Inc. (15434) | |
| 494017000 | 2915-01-556-4392 | Injector Assembly, Fuel | END Item Identification: Pandur ii diesel engine | Cummins Inc. (15434) | |
| 494333 | 2915-00-278-9420 | Housing, Fuel Heater | III End Item Identification: 29157246177 General Characteristics Item Description: Aluminum alloy | United Technologies Corporation (77445) | |
| 49447 | 2915-00-873-8212 | Seal, Fuel Nozzle | III End Item Identification: T63-A-700 & T63-A-720 turbine engine | Delavan Inc. (71895) | |
| 4-945-75 494575 | 2915-00-313-1199 | Swing, Valve, Check | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (45681) | ||
| 494618 | 2915-00-943-5633 | Filter Element, Fluid | III Fsc Application Data: Fuel filter, engine, acft Material: Paper container/cartridge paper filtering medium Media for Which Designed: Fuel/oil, hydrocarbon | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 494619 | 2915-00-942-2519 | Support, Fuel Filter Element | III End Item Identification: TF30-P-1 aircraft engine fuel control General Characteristics Item Description: Ams 4135 aluminum alloy W/hardcoat and anodized finish, O/a dim. 4.110 in. min to 4.130 in. max dia by 1.510 in. min to 1.550 in. max lg, small end 1.170 in. min to 1.190 in. max outside dia and 1.135 in. min to 1.139 in. max inside dia | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 494621 | 2915-00-942-2520 | Spacer, Fuel Filter rod | III End Item Identification: TF30-P-100 aircraft engine fuel filter P/N 513823 General Characteristics Item Description: Ams 5613 stainless steel W/rockwell-C 35 to 40 hardness, O/a dim. 1.740 in. min to 1.760 in. max dia by 1.465 in. min to 1.475 in. max lg, 1.123 in. min to 1.127 in. max dia W/35 deg chamfer to 0.865 in. min to 0.885 in. max dia small end, inside 0.888 in. min to 0.892 in. max dia W/taper to 0.803 in. min to 0.807 in. max dia and 0.650 in. min to 0.670 in. max dia, 4 holes 0.120 in. min to 0.130 in. max dia equally spaced on front behind flange, 4 holes 0.136 in. min to 0.146 in. max dia thru side | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 494622 | 2915-00-942-2521 | Cover Assembly, Fuel Filter | III End Item Identification: TF30-P-1 aircraft engine fuel filter P/N 513823 General Characteristics Item Description: Includes 2 assembled parts, P/ns 494623 and MS9105-1 | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 494631 | 2915-00-922-8986 | Orifice Bolt, Filter | United Technologies Corporation (77445) | ||
| 494632 | 2915-00-942-2522 | Plug, Fuel Filter | III End Item Identification: TF30-P-1 aircraft engine fuel control filter P/N 513823 General Characteristics Item Description: Ams 5613 stainless steel W/rockwell-C 25 to 33 hardness, O/a dim. 0.482 in. dia by 1.290 in. min to 1.310 in. max lg, 0.429 in. min to 0.433 in. max small end dia, inside dim. 0.240 in. min to 0.260 in. max dia by 0.140 in. min to 0.180 in. max deep right end, 0.190 in. min to 0.210 in. max dia by 0.730 in. min to 0.780 in. max deep left end, both ends chamfer outside, 2 grooves around side 0.095 in. min to 0.105 in. max and 0.084 in. min to 0.104 in. max W, 2 holes 0.060 in. min to 0.080 in. max dia on left side | United Technologies Corporation (77445) | |
| 49474 | 2915-00-708-4280 | Guide, Spring Seat | Goodrich Corporation (11599) |