FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-015-2216, 2840-00-015-8540, 2840-00-016-0130
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-015-2216 2840000152216 | 6842633P006 | Spacer, Turbine Rotor, Aircraft Ga | III End Item Identification: Acft eng T-56 Criticality Code Justification: AGAV Material: Steel corrosion resisting | General Motors Corp. (24617) Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-015-2224 2840000152224 | 6843872-6 | Lock Ring, Turbine Blade | III End Item Identification: T56 eng Criticality Code Justification: ADAV Material: Steel corrosion resisting | Precision Rings Incorporated (99121) Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-015-2226 2840000152226 | 6844140 | Seal, Metallic, Aircraft gas Turbi | III End Item Identification: Acft eng T56 Criticality Code Justification: AGAV Engine Section Location: Turbine | Parker-Hannifin Corporation (04319) Abdite Industries Inc. (70042) Rolls-Royce Corporation (63005) | |
| 2840-00-015-2227 2840000152227 | 6844608 | Sleeve, Vent Tube se | III End Item Identification: Acft eng T-56 Criticality Code Justification: AGAV | Rolls-Royce Corporation (63005) General Motors Corp. (24617) Allison Transmission Inc. (73342) | |
| 2840-00-015-2228 2840000152228 | 6844620 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: Acft eng T56 Criticality Code Justification: AGAV Engine Section Location: Turbine | General Motors Corp. (24617) Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | |
| 2840-00-015-4178 2840000154178 | 500293 | Bracket, Ignition Exciter, Turbine | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, cadmium plate, AMS2400, 3.310 in. lg, 2.345-2.360 in. W, 0.057-0.067 in. material thk III Fsc Application Data: Acft jet engine | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 2840-00-015-4179 2840000154179 | 500309 | Support Assembly, Ignition, gas Tu | III End Item Identification: Acft eng TF-33 Criticality Code Justification: ADAV Overall Diameter: 16.135 inches minimum and 16.255 inches maximum | United Technologies Corporation (77445) | |
| 2840-00-015-4181 2840000154181 | 500306 | Support Assembly, Ig | III End Item Identification: TF-33 aircraft engine | United Technologies Corporation (77445) | |
| 2840-00-015-4182 2840000154182 | 500292 | Bracket, Ignition Exciter, Turbine | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or AMS6355, rockwell C32-38 hardness, cacmium plate, AMS2400, 3.310 in. lg, 2.345-2.360 in. W, 0.057-0.067 in. material thk III Fsc Application Data: Acft jet engine | United Technologies Corporation (77445) | |
| 2840-00-015-4183 2840000154183 | 500294 | Bracket, Ignition Exciter, Turbine | III End Item Identification: Engine model TF33 General Characteristics Item Description: Steel, AMS6350 or ams 6355, rockwell C32-38 hardness, cadmium plate, ams 2400, 3.310 in. lg, 2.345-2.360 in. W, 0.057-0.067 in. material thk III Fsc Application Data: Aircraft jet engine | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 2840-00-015-4186 2840000154186 | 500961 | Cover, Oil Tank | III End Item Identification: Acft eng TF-33 General Characteristics Item Description: Steel ams 5645, 2.875 in. dia of bolt circle, 1.600 in. I/D, 0.520 in. W, 0.276 min 0.286 max in. dia of 3 holes | United Technologies Corporation (77445) | |
| 2840-00-015-4188 2840000154188 | 765198 506979 789507 752879 656407 | Rotor, Turbine, Aircraft gas Turbi | III End Item Identification: TF33 acft eng Criticality Code Justification: AGAV | United Technologies Corporation (77445) | |
| 2840-00-015-6934 2840000156934 | 1-060-127-03 | Housing, Bearing Seal | III End Item Identification: Engine T-53 General Characteristics Item Description: Steel AMS6382, rockwell C scale 23 max hardness, black oxidefinish AMS2485 | Honeywell International Inc. (99193) | |
| 2840-00-015-8050 2840000158050 | 502337 | Case and Vane Assembly, Compresso | III End Item Identification: Pratt and whitney TF-33-P-5-9-11A Criticality Code Justification: AGAV Engine Section Location: Compressor | United Technologies Corporation (77445) | |
| 2840-00-015-8537 2840000158537 | 6846215 | Cover Assy, Accessor | III End Item Identification: Acft eng T-56 Criticality Code Justification: AGAV | Allison Transmission Inc. (73342) General Motors Corp. (24617) Rolls-Royce Corporation (63005) | |
| 2840-00-015-8539 2840000158539 | 6846569 | Cover, Scavenge Pump | III End Item Identification: Acft eng T-56 Criticality Code Justification: Adav and agav Special Features: Matl ams 5315 | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) General Motors Corp. (24617) | |
| 2840-00-015-8540 2840000158540 | 6846935 | Housing, Antifriction Bearing, Air | Criticality Code Justification: AGAV Engine Section Location: Turbine Material: Steel housing | Rolls-Royce Corporation (63005) Pacific SKY Supply Inc. (66905) Allison Transmission Inc. (73342) | |
| 2840-00-015-8587 2840000158587 | 619E373G16 619E373G20 619E373G13 619E373G19 | Gearbox, Accessory Drive, Turbine | General Electric Company (07482) General Electric Co. (24446) | ||
| 2840-00-015-8590 2840000158590 | 6842858 | Insert Assy, Passage | III End Item Identification: Acft eng T56 General Characteristics Item Description: Steel ams 5560 for shaft, ams 5639 for mated END;2.562 in. lg, 0.359 min 0.381 max inside dia, 0.437 in. outside dia, 0.125 in. depth of notch | Allison Transmission Inc. (73342) General Motors Corp. (24617) Rolls-Royce Corporation (63005) | |
| 2840-00-016-0130 2840000160130 | 2-080-174-01 | Guide, Oil Filter | General Characteristics Item Description: Steel AMS6455, cadmium plated AMS2400-3, rockwell C scale 42 min, 47 max hardness, 2.080 in. min, 2.090 in. max od | Honeywell International Inc. (99193) |