FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-018-4072, 2840-00-019-2216, 2840-00-019-2570

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
2840-00-018-4072
2840000184072
467298Bracket, Valve, Anti-IcingIII End Item Identification: Engine model TF33
General Characteristics Item Description: Cres, ams 5504, rockwell C30-38 hardness, 4.010 in. lg, 1.979 in. H, 3.250 in. W
III Fsc Application Data: Aircraft jet engine
United Technologies Corporation (52661, 77445)

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2840-00-018-4073
2840000184073
698999
822636
466009
Hub, Compressor, Aircraft gas TurbIII End Item Identification: Acft eng TF33
Criticality Code Justification: AGAV
Engine Section Location: Compressor
United Technologies Corporation (77445)

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2840-00-018-4074
2840000184074
452144Tube, Air Pressure, CIII End Item Identification: Acft ENGTF-33
Criticality Code Justification: Abhp and adav
Special Features: Matl ams 5570
Tube Bends Incorporated (33830)
Lewis & Saunders Inc. (21890)
Turbo Power & Marine System Inc. (11449)

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2840-00-018-4492
2840000184492
505683Support, ScIII End Item Identification: Eng J-57
Emhart Industries Inc. (05657)
United Technologies Corporation (77445)
Filtron Co. Inc. (81831)

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2840-00-018-4894
2840000184894
5001T81P01Shield, Electric ConnectorIII End Item Identification: Acft eng J85
General Characteristics Item Description: 5.300 min 5.420 max in. lg, 0.187 min 0.203 max in. dia of 2 holes
General Electric Company (99207)
Aero Metal Forms Inc. (3T761)
Scottsdale Tool and DIE (32482)

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2840-00-018-4895
2840000184895
3003T29P01Bracket Assy, ShieldIII End Item Identification: J85 eng
General Characteristics Item Description: Cres AMS5510 bracket 0.073 min, 0.087 max in. thk matl bracket assy consists of P/ns 3003T29P02, bracket and MK2031-3P anchor nut, fscm 75237
General Electric Company (99207)
General Electric Co. (24446)

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2840-00-018-9420
2840000189420
1-110-101-03Deflector, Turbine NozzleIII End Item Identification: T-53 series engines
General Characteristics Item Description: Cres, AMS5532, rockwell 30T SCALE.74.5 min, 81.5 max hardness, 9.517IN. nom od, 5.615 in. min, 5.620 in. max id flange, 1.060 in. nom O/a lg, 0.032 in. min, 0.040 in. max thk material
Honeywell International Inc. (99193)

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2840-00-019-1402
2840000191402
1C5408G1Anvil, Combustion Liner RepairGeneral Electric Co. (24446)
General Electric Company (07482)

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2840-00-019-1982
2840000191982
U527909Plate, CoverIII End Item Identification: Acft eng J79, J85, T58, T64
Criticality Code Justification: AGAV
Triumph Thermal Systems Inc. (78943)

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2840-00-019-2212
2840000192212
500259Cushion, Front Oil TankIII End Item Identification: Acft eng TF33
Criticality Code Justification: Matt and abhp and abmk and agav
Material: Rubber synthetic
United Technologies Corporation (77445)
Turbo Power & Marine System Inc. (11449)

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2840-00-019-2214
2840000192214
500239Bracket Assy, FrontIII End Item Identification: Acft eng TF33
General Characteristics Item Description: 12.790 in. lg, 0.339 min 0.349 max in. dia of 2 holes, 0.307 min 0.317 max in. dia of 1 hole, 0.375 min 0.381 max in. dia of 1 hole
United Technologies Corporation (77445)
Turbo Power & Marine System Inc. (11449)

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2840-00-019-2216
2840000192216
502336Elbow, Breather TubeIII End Item Identification: Acft eng TF33
Criticality Code Justification: Matt and abhp and adav and agav
Special Features: Matl ams 5646
United Technologies Corporation (77445)

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2840-00-019-2217
2840000192217
502334Connector-Tube, CaseIII End Item Identification: Acft eng TF33
General Characteristics Item Description: Steel ams 5646, 3.628 in. lg, 1.390 min 1.410 max in. H, 0.495 min 0.505 max in. dia of 1 hole, 0.348 min 0.358 max in. dia of 1 hole
United Technologies Corporation (77445)
Hamilton Sundstrand Corporation (73030)

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2840-00-019-2220
2840000192220
463382Seal, Air, Aircraft gas Turbine EnIII End Item Identification: Acft eng tf 33
Criticality Code Justification: AGAV
Overall Length: 6.999 inches minimum and 7.001 inches maximum
United Technologies Corporation (77445)

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2840-00-019-2223
2840000192223
500952Tank, Lubricating Oil, Aircraft GaCriticality Code Justification: Abhp and abmk
Engine Section Location: Compressor
Overall Length: 30.950 inches nominal
United Technologies Corporation (77445)

Quote

2840-00-019-2224
2840000192224
JA484642
484642
Shield, Heat, Aircraft gas TurbineEngine Section Location: Turbine
Material: Nickel alloy shield
Overall Length: 4.400 inches nominal
JET Avion Corporation (14236)
United Technologies Corporation (77445, 52661)

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2840-00-019-2561
2840000192561
6807738Clamp, ThermocoupleIII End Item Identification: Acft eng T56
General Characteristics Item Description: Steel ams 5510, 1.122 in. lg, 0.500 in. W, 0.028 min 0.036 max in. thk, 0.217 min 0.225 max in. dia of 2 holes
Allison Transmission Inc. (73342)
General Motors Corp. (24617)

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2840-00-019-2564
2840000192564
109R283G8
109R283G7
Case, Turbine, Aircraft gas TurbinIII End Item Identification: J79 eng
Criticality Code Justification: Abhp and agav
Overall Length: 13.095 inches minimum and 13.105 inches maximum
General Electric Company (07482)
General Electric Co. (24446)

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2840-00-019-2568
2840000192568
105B2199G1
105B3895G1
Bracket Assembly, AnIII End Item Identification: Eng J-47, J-79, T-58 and T-64
General Characteristics Item Description: Cres AMS5510;0.065 min, 0.077 max in. thk matl;assy consists of P/N 105B3895P2 spacer and P/N 105B3895P3 bracket
General Electric Co. (24446)
General Electric Company (07482)

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2840-00-019-2570
2840000192570
517D227G1Bracket Assembly, AmIII End Item Identification: En J-47, J-79, T-58 and T-64
General Characteristics Item Description: Major components consist of: bracket pn 517D227P2, nut pn R401P2, solid rivet pn AN123470; riveting conforms to ge spec M50T814R
General Electric Co. (24446)
General Electric Company (07482)

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