Aircraft and Missile Prime Movers Engine Fuel System Components: 505421, 5054M72G09, 505P044-02
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 505421 | 2915-00-588-0474 | Plate, Roller Retaining | III End Item Identification: Fuel control, 29159587628 | Hamilton Sundstrand Corporation (73030) | |
| 5054M61 | 2915-01-190-9266 | Distributor, Fuel | General Electric Company (07482) | ||
| 5054M61G02 | 2915-01-190-9266 | Distributor, Fuel | General Electric Company (07482) | ||
| 5054M61G05 | 2915-01-190-9266 | Distributor, Fuel | Cairns Thomas M (45975) General Electric Company (03350,07482) | ||
| 5054M71G02 | 2915-01-190-9267 | Distributor, Fuel | III End Item Identification: Augmentor for F110 acft eng General Characteristics Item Description: 4 per engine | General Electric Company (07482) | |
| 5054M71G06 | 2915-01-304-2130 | Distributor, Fuel | General Electric Company (07482) | ||
| 5054M72G01 | 2915-01-390-8587 | Spraybar, Fuel, Augme | III End Item Identification: F110-GE-100 & -129 turbo fan augmented aircraft main propulsion III Part Name Assigned By Controlling Agency: Fuel spraybar augmentor III Reference Data and Literature: T.O.2J-F110-4, figure 68 | General Electric Company (07482) Parker-Hannifin Corporation (59211) Woodward FST Inc. (65065) | |
| 5054M72G06 | 2915-01-316-7779 | Spraybar, Fuel Augment | III End Item Identification: Engine gas turbine | General Electric Company (03350,07482) | |
| 5054M72G08 | 2915-01-390-8587 | Spraybar, Fuel, Augme | III End Item Identification: F110-GE-100 & -129 turbo fan augmented aircraft main propulsion III Part Name Assigned By Controlling Agency: Fuel spraybar augmentor III Reference Data and Literature: T.O.2J-F110-4, figure 68 | Delavan Inc. (71895) General Electric Company (07482) Parker-Hannifin Corporation (59211) Woodward FST Inc. (65065) | |
| 5054M72G09 | 2915-01-481-8352 | Spraybar, Fuel, Augme | III Part Name Assigned By Controlling Agency: Spraybar, fuel, augmenter-local III Reference Data and Literature: 2J-F110-4 | Delavan Inc. (71895) General Electric Company (07482) Parker-Hannifin Corporation (09523) Woodward FST Inc. (65065) | |
| 5054M97G02 | 2915-01-191-8397 | Spraybar, Fuel, Left hand Ab | III End Item Identification: F110-GE-100 acft eng General Characteristics Item Description: Cres; 2 tubes 10.77 and 4.62 in. l from tip to mtg flange holes, 2 holes thru 0.210 - 0.218 in. dia 1.310 in. dist C-to-C | General Electric Company (07482) | |
| 5054M98G02 | 2915-01-191-6912 | Spraybar, Fuel, Right hand Ab | III End Item Identification: F110-GE-100 acft eng General Characteristics Item Description: Cres per AMS5754; 11.63 in. l from tip to mtg flange holes, 2 holes thru 0.210 - 0.218 in. dia 1.310 in. apart C-to-C | General Electric Company (07482) | |
| 5054M99G02 | 2915-01-191-8398 | Spraybar, Fuel, Left hand Ab | III End Item Identification: F110-GE-100 acft eng General Characteristics Item Description: Cres; 2 tubes 9.00 and 4.62 in. l from tip to mtg flange holes, 2 holes thru 0.210 - 0.218 in. dia 1.310 in. dist C-to-C | General Electric Company (07482) | |
| 5054T86G03 | 2915-01-513-9144 | Tee, Scavenge Filter | GE Engine Services Inc. (062W2) | ||
| 5056T60G01 | 2915-01-529-9126 | Tube Assembly, Aircraft Engine | III End Item Identification: CT7-9 turboprop engine for CN-235 transport aircraft | General Electric Company (99207) | |
| 5058T21G01 | 2915-01-180-7786 | Manifold, Fluid, Engine | III End Item Identification: Engine F404/F104 | General Electric Company (99207) | |
| 505938 | 2915-00-940-9914 | Housing, Afterburner Igniter Valv | 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, O/a dim. 0.620 in. min to 0.640 in. max dia by 0.610 in. min to 0.620 in. max lg, 0.406 in. min to 0.409 in. max dia small end, hexangular end fits 0.381 in. min dia, 6 holes 0.050 in. min to 0.070 in. max dia equally spaced on hex, inside dim. 0.260 in. min to 0.270 in. max dia by approx 0.550 in. min to 0.562 in. max deep, 0.260 in. min to 0.265 in. max and 0.330 in. min to 0.345 in. max dia by 0.058 in. min to 0.060 in. max deep | United Technologies Corporation (77445) | |
| 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 | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 505987 | 2915-00-588-8280 | Shaft, Linkage Lever | III End Item Identification: 29155864023 General Characteristics Item Description: Steel, 2.2200 in. lg, 0.1562 in. dia O/a | Hamilton Sundstrand Corporation (73030) | |
| 505P044-02 505P04402 | 2915-01-343-2939 | Valve, Fuel Manifold | Textron Inc. (21178) |