FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-071-5981, 2840-00-071-6421, 2840-00-071-9069
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
2840-00-071-5981 2840000715981 | 37E500196P103 37E500006P106 37E500196P119 | Blade, fan, Aircraft gas Turbine E | General Electric Co. (24446) General Electric Company (99207) | ||
2840-00-071-5983 2840000715983 | 6789558 516884 6846127 6792964 6808638 | Seal, Air, Aircraft gas Turbine En | III End Item Identification: T56 aircraft engine Criticality Code Justification: AGAV Engine Section Location: Turbine | Rolls-Royce Corporation (63005) SKF USA Inc. (80201) General Motors Corp. (24617) | |
2840-00-071-6169 2840000716169 | 495121 | Case and Vane Assembly, Compresso | III End Item Identification: Acft eng TF33 Criticality Code Justification: AGAV Engine Section Location: Compressor | United Technologies Corporation (77445) | |
2840-00-071-6420 2840000716420 | RA17137 | Cover, Protective | Special Features: Polyethylene or other pliable plastic material | Crane Co. (51663) | |
2840-00-071-6421 2840000716421 | RA16551 | Spring, Helical | Special Features: Material cres, type 16 Material: Steel corrosion resisting | Crane Co. (51663) | |
2840-00-071-6425 2840000716425 | RA15545 | Spring, Helical | Special Features: Cres 17, 17 ph per AMS5673 Material: Steel corrosion resisting | Crane Co. (51663) | |
2840-00-071-6426 2840000716426 | RD17136 | Cover, Protective | III End Item Identification: Eng J-85 | Crane Co. (51663) | |
2840-00-071-7032 2840000717032 | 576556 | Bracket Assy, Ignition | III End Item Identification: Acft eng TF30 Criticality Code Justification: AGAV | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
2840-00-071-7038 2840000717038 | 569773 | Bracket Assembly, Bleed Control | General Characteristics Item Description: Consisting of-three 490231 and one 569772 fscm 77445 III Fsc Application Data: Aircraft jet engine, TF30 | United Technologies Corporation (77445) | |
2840-00-071-7045 2840000717045 | 567407 | Shield, Heat, Aircraft gas Turbine | Engine Section Location: Turbine End Item Identification: Acft eng TF30 Diameter: 10.460 inches nominal | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
2840-00-071-8673 2840000718673 | P41756 | Support, Engine Fron | United Technologies Corporation (77445) | ||
2840-00-071-8677 2840000718677 | 596127 596126 762932 597376 597994 | Case, Diffuser, Turbine Engine | United Technologies Corporation (77445) | ||
2840-00-071-8678 2840000718678 | 572523 | Support Assembly, Lower | General Characteristics Item Description: 13.130 in. min, 13.170 in. max lg O/a | United Technologies Corporation (77445) | |
2840-00-071-8681 2840000718681 | 565487 | Housing, Antifriction Bearing, Air | United Technologies Corporation (77445) | ||
2840-00-071-8688 2840000718688 | 558279P5 | Liner Fuel Control | Royal Oak Gage Inc. (00088) United Technologies Corporation (77445, 52661) | ||
2840-00-071-8689 2840000718689 | 2900T96P01 | Plate, Ignitor | General Electric Company (99207) | ||
2840-00-071-8693 2840000718693 | 231957 | Shroud, Turbine Rota | Curtiss-Wright Controls Inc. (0AHP5) | ||
2840-00-071-8701 2840000718701 | 6900T06G01 | Liner Shell-Flange | Training Aids Inc. (99027) General Electric Company (99207) | ||
2840-00-071-8703 2840000718703 | 597472 | Cover Assy, Main Pum | United Technologies Corporation (77445) | ||
2840-00-071-9069 2840000719069 | 463504 | Disk, Turbine, Aircraft gas Turbin | III End Item Identification: Acft eng TF33 Engine Section Location: Turbine Special Features: 0.499-0.501 in. dia. of 20 holes; 0.624-0.625 in. dia. of 10 holes | United Technologies Corporation (77445) |