FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-070-0221, 2840-00-070-0222, 2840-00-070-0539

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
2840-00-070-0221
2840000700221
501015CL2Spacer, Turbine AirIII End Item Identification: TF-33 aircraft engine
Criticality Code Justification: AGAV
United Technologies Corporation (77445)

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2840-00-070-0222
2840000700222
501015CL3Spacer, Turbine AirIII End Item Identification: TF-33 aircraft engine
Criticality Code Justification: AGAV
United Technologies Corporation (77445)

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2840-00-070-0450
2840000700450
706902Case and Vane Assembly, Axial ComUnited Technologies Corporation (77445)

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2840-00-070-0483
2840000700483
6789199
6845703
Housing, Antifriction Bearing, AirRolls-Royce Corporation (63005)
General Motors Corp. (24617)
Allison Transmission Inc. (73342)

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2840-00-070-0493
2840000700493
3001T90P01Retainer, Igniter CoIII End Item Identification: Eng J-85
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0501
2840000700501
4000T72P01Synchronizing Ring, Augmentor ExhIII End Item Identification: Acft eng J85
Criticality Code Justification: AGAV
Material: Steel
General Electric Company (99207)
General Electric Co. (24446)

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2840-00-070-0505
2840000700505
4001T49P01Shroud, Front Frame, Aircraft gasIII End Item Identification: Acft eng J85
Criticality Code Justification: AGAV
Engine Section Location: Compressor
Orenda Aerospace Corporation (35013)
Kerns Manufacturing Corp. (93596)
General Electric Company (99207)

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2840-00-070-0509
2840000700509
4002T27G01
4002T27P01
Support Assy, DrainGeneral Electric Company (99207)
General Electric Co. (24446)

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2840-00-070-0510
2840000700510
4002T43P01Shield, Heat, Aircraft gas TurbineCriticality Code Justification: AGAV
Engine Section Location: Turbine
Material: Steel comp 321 shield
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0511
2840000700511
4002T55P01Cover, Sump, Front FrIII End Item Identification: Eng J-85
General Characteristics Item Description: Aluminum ams 4150 or ams 4260, anodize MIL-A-8625, 3.780 in. min, 0.380 in. max dia
General Electric Company (99207)
General Electric Co. (24446)

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2840-00-070-0512
2840000700512
4002T59P01
37B201542P105
37C311043P101
Bar, Snubber, AfterburnerIII End Item Identification: J-85 aircraft engine
General Characteristics Item Description: Steel ams 5570, 10.460 in. min, 10.540 in. max lg, 0.040 in. min, 0.050 in. max W, 0.187 in. od
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0513
2840000700513
4002T59P02
4002T58P02
37C311043P104
37B201542P106
Bar, Snubber, AfterburnerIII End Item Identification: Acft model J85
General Characteristics Item Description: Tubing 0.187 in. od X 0.015-0.025IN. wall materiel ams 5570, 0.060- 0.070 in. outside width of tubing section
General Electric Co. (24446)
General Electric Company (99207)
D & D Machinery and Sales Inc. (1Y128)

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2840-00-070-0514
2840000700514
37B201542P107
4002T59P03
37C311043P106
Bar, Snubber, AfterburnerIII End Item Identification: Acft model J85
General Characteristics Item Description: Tubing 0.187 in. od X 0.015-0.025IN. wall materiel ams 5570, 0.090- 0.100 in. outside width of tubing section
D & D Machinery and Sales Inc. (1Y128)
Hydromach Inc. (1FG56)
B-C-D Metal Products Inc. (04602)

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2840-00-070-0515
2840000700515
37C311043P108
37B201542P108
4002T59P04
Bar, Snubber, AfterburnerIII End Item Identification: Acft model J85
General Characteristics Item Description: Tubing 0.187 in. od X 0.015-0.025IN. wall materiel ams 5570, 0.120- 0.130 in. outside width of tubing section
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0517
2840000700517
4002T92P01Support, IdentificationIII End Item Identification: Eng J-85
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0524
2840000700524
5000T65P01Shield, Heat, Air ImpIII End Item Identification: Eng J-85
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0525
2840000700525
5000T81P01Vane, Variable, FrontIII End Item Identification: J-85 aircraft engine
Criticality Code Justification: TEXT
General Characteristics Item Description: Consists of stem P/N 5000T81P02, covering, vane P/N 5000T81P03, spindle P/N 5000T81P04, baffle, fwd P/N 5000T81P05, divider P/N 5000T81P06, assembly P/N 5000T81P07
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0526
2840000700526
5001T27P01Duct, Leakage, STAGE8III End Item Identification: Eng J-85
General Characteristics Item Description: Consists of flange P/N 5001T27P02, elbow, half P/N 5001T27P03, elbow, half P/N 5001T27P04, duct, half P/N 5001T27P05, duct, half P/N 5001T27P06, tube P/N 5001T27P07, ferrule P/N 5001T27P08
General Electric Co. (24446)
General Electric Company (99207)

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2840-00-070-0535
2840000700535
4001T07P01Tube Assy, AfterburnIII End Item Identification: Eng J-85
General Electric Company (99207)
General Electric Co. (24446)

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2840-00-070-0539
2840000700539
5611-017Housing and StatorIII Fsc Application Data: Gas turbines and jet engines, aircraft
Kemtron Electron Products Inc. (92703)
IMC Magnetics Corp. (99743)

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