Turbo Power & Marine System Inc. NSN Parts: 646255 - 767409
FSC 2915 Engine Fuel System Components, Aircraft and Missile Prime Movers
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 646255 | 2915-00-119-6131 | Support, Strainer El | 11449 | ||
| 749902 | 2915-01-003-5572 | Tip, Fuel Nozzle | III End Item Identification: Acft engine TF34P100 fuel lines General Characteristics Item Description: Steel, 1.245 in. min 1.255 in. max lg, 1.197 in. od 0.935 in. id one end, 1.037 in. dia other end | 11449 | |
| 739597 | 2915-01-010-1305 | Tip, Metering, Fuel Nozzle | III End Item Identification: Acft engine TF33P7, P7A General Characteristics Item Description: Cres AMS5630, 0.393 in. lg, 0.218 in. min 0.223 in. max dia approx O/a dim. | 11449 | |
| 557476 | 2915-00-940-9941 | Tube Assembly, Afterburner Spray | III End Item Identification: J57 aircraft fuel control General Characteristics Item Description: Includes ferrule tube, P/N 560648, W/brazed connections each end, P/ns 175823, 462056 and 557477 | 11449 | |
| 483981 | 2915-00-688-9936 | Tube Assembly, Fuel | III End Item Identification: Engine, TF33P5 General Characteristics Item Description: Braze per AMS2666, 14.563 in. min, 14.603 in. max lg, consists of P/N 493354, P/N 546692, P/N 475122, P/N 419163, and P/N 403768 | 11449 | |
| 483984 | 2915-00-688-9938 | Tube Assembly, Fuel | General Characteristics Item Description: Braze per AMS2666, 0.940 in. gage dia both ends consists of 2 ea, P/N 307928, 2 ea, P/N 227428, 2 ea, P/N 419487, and 1 ea, P/N 391892 | 11449 | |
| 434297 | 2915-00-873-6540 | Tube Assy, Fuel Drai | 11449 | ||
| 481260 | 2915-00-967-0377 | Tube Assy, Metal | III End Item Identification: TF33-P-7, 7A aircraft engine General Characteristics Item Description: Tube od 1.000 in, id 0.920 in. connects fuel pump to anti-icing heater | 11449 | |
| 496329 | 2915-00-940-9924 | Tube, Transfer Packing | III End Item Identification: TF30-P-1 aircraft fuel control General Characteristics Item Description: Material aluminum alloy, O/a dim. 0.495 in. min to 0.497 in. max dia by 0.600 in. min to 0.620 in. max lg, 2 grooves, 0.095 in. min to 0.105 in. max W, around side and spaced 0.020 in. min to 0.040 in. max from each end, 0.270 in. min to 0.280 in. max inside dia | 11449 | |
| 500686 | 2915-00-940-9932 | Tube, Transfer, Fuel Control | III End Item Identification: TF30-P-1 aircraft engine fuel control, P/N 464200 General Characteristics Item Description: Ams 5643 stainless steel W/rockwell-C 31 to 39 hardness, O/a dim. 3.209 in. min to 3.211 in. max dia by 6.950 in. min to 6.970 in. max lg, 2.905 in. min to 2.925 in. max inside dia, 2 grooves around side 0.162 in. min to 0.172 in. max W | 11449 | |
| 538714 | 2915-00-941-9625 | Tube, Transfer, Packing | General Characteristics Item Description: Stainless steel, rockwell hardness C 31-39 or equal, O/a dim. approx 0.930 in. min to 1.050 in. max dia by 5.840 in. min to 5.860 in. max lg, 0.820 in. min to 0.840 in. max inside dia, approx wt 0.268 lbs used as transfer from fuel filter to hydraulic pump | 11449 | |
| 367102 | 2915-00-626-3796 | Valve and Liner Ass | 11449 | ||
| 468942 | 2915-00-738-6158 | Valve Assembly, Afterburner | III End Item Identification: Engine, aircraft, J75 | 11449 | |
| 353174 | 2915-01-075-9613 | Valve, Diaphragm, Flat, Ab Igntr Re | III Fsc Application Data: Acft engine fuel system components | 11449 | |
| 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 | 11449 | |
| 4050548 | 2915-01-035-3771 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Acft engine model F100-PW-100 General Characteristics Item Description: 4.85 in. l, 3.70 in. H, 2.30 in. W, max wt 1.4 lb Reference Number Differentiating Characteristics: As differentiated by source control no. 4050548 | 11449 | |
| 464392 | 2915-00-942-5270 | Valve, Fuel Pressurizing and Drai | III End Item Identification: TF30-P-1 aircraft engine fuel system, P/N 539735 General Characteristics Item Description: Ams 5616 stainless steel, rockwell-C 45 to 50 hardness, chromium plated and surface roughness, O/a dim. 1.747 in. dia by 1.680 in. min to 2.720 in. max lg, small end 0.640 in. min to 0.660 in. max dia, inside 1.535 in. min to 1.545 in. max dia | 11449 | |
| 477080 | 2915-00-072-8762 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Engine TF33P9 | 11449 | |
| 505939 | 2915-00-940-9915 | Valve, Fuel, Afterburner Igniter | III End Item Identification: TF30-P-1 aircraft fuel control, P/N 531874 General Characteristics Item Description: Material stainless steel W/rockwell C 45 to 50 hardness, front location, O/a dim. 0.649 in. min to 0.653 in. max dia by 1.672 in. lg, left end dim. 0.185 in. min to 0.195 in. max dia W/hole 0.030 in. min to 0.040 in. max dia thru side, thd section size 0.250-28 UNJF-3A, right end dim. 0.310 in. min to 0.315 in. max dia W/0.003 in. min to 0.010 in. max radius 3 places | 11449 | |
| 767409 | 2915-00-940-9915 | Valve, Fuel, Afterburner Igniter | III End Item Identification: TF30-P-1 aircraft fuel control, P/N 531874 General Characteristics Item Description: Material stainless steel W/rockwell C 45 to 50 hardness, front location, O/a dim. 0.649 in. min to 0.653 in. max dia by 1.672 in. lg, left end dim. 0.185 in. min to 0.195 in. max dia W/hole 0.030 in. min to 0.040 in. max dia thru side, thd section size 0.250-28 UNJF-3A, right end dim. 0.310 in. min to 0.315 in. max dia W/0.003 in. min to 0.010 in. max radius 3 places | 11449 |
