FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-011-5623, 2840-00-012-0021, 2840-00-012-7025

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
2840-00-011-5623
2840000115623
577166Cover, Turbine Stator VaneIII End Item Identification: TF30 eng
General Characteristics Item Description: Nickel alloy AMS5536;1.335 min, 1.375 max in. LG;0.022 min, 0.028 max in. thk;for use on 1ST stage stator
United Technologies Corporation (77445)

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2840-00-011-5951
2840000115951
625879Patch, CombustionUnited Technologies Corporation (77445)

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2840-00-011-9952
2840000119952
572081Stop, Power Lever CrUnited Technologies Corporation (77445)

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2840-00-012-0017
2840000120017
589426Mount, Ignition EXC1United Technologies Corporation (77445)

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2840-00-012-0021
2840000120021
538992Stiffener, CombustioUnited Technologies Corporation (77445)

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2840-00-012-0023
2840000120023
572195Piston, Anti-IcingUnited Technologies Corporation (77445)

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2840-00-012-0827
2840000120827
407682Boss, Diffuser CaseIII End Item Identification: Acft eng J52
General Characteristics Item Description: Stainless steel, ams 5613;2.192 in. lg, 4 mounting holes
United Technologies Corporation (77445)

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2840-00-012-0835
2840000120835
611659N9Blade set, Turbine RCurtiss-Wright Controls Inc. (0AHP5)

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2840-00-012-3269
2840000123269
PK242Cover, Shipping, Oil VentGeneral Characteristics Item Description: Plastic, yellow ana bulletin 166 no. 505 or C. g. s. b. 1-GP-12 no. 5-1, 2.160 in. min, 2.240 in. max lg, 1.400 in. min, 1.480 in. max W, 0.125 in. nom thk, 2 holes 0.220 in. min, 0.240 in. max dia, 5000 psi min compression strength, fuel and oil res, 150 deg F heat res
Canadian Commercial Corporation (98247)
Pratt and Whitney Canada Inc. (00198)

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2840-00-012-3271
2840000123271
PK425Cover, Shipping, Engine MountGeneral Characteristics Item Description: Plastic, yellow ana bulletin 166 no. 505 or C. g. s. b. 1-GP-12 no. 5-1, 4.000 in. min, 4.080 in. max lg, 2.450 in. min, 2.530 in.max W, 0.375 in. thk, 0.375 in. min, 0.415 in. max radius corners, 4 holes 0.405 in. min, 0.425 in. max dia, 3.250 in. C to C distance between holes along the lg, 1.600 in. C to C distance between holes along the W, 5000 psi min compression strength, fuel and oil res, 150 deg F heat res
Pratt and Whitney Canada Inc. (00198)

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2840-00-012-3276
2840000123276
PK1841
PK4471
PK257
Cover, Shipping, Propeller ShaftGeneral Characteristics Item Description: Plastic, yellow fed std 595 no. 13655 or C. g. s. b. 1-GP-12 no. 5-1, 5 holes 0.575 in. min, 0.625 in. max dia on 4.250 in. bolt circle dia, 5000 psi min compression strength, fuel and oil res, 150 deg F heat res
Pratt and Whitney Canada Inc. (00198)

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2840-00-012-3277
2840000123277
PK255Cover, Shipping, Tachometer MountIII End Item Identification: Engine PT6A
General Characteristics Item Description: Plastic, yellow ana bulletin 166 no. 505 or C. g. s. b. 1-GP-12 no. 5-1, 2.436 in. min, 2.516 in. max lg, 2.436 in. min, 2.516 in. max W, 0.250 in. nom thk, 0.280 in. min, 0.320 in. max radius corners, 4 holes 0.280 in. min, 0.300 in. max dia on 2.653 in. bolt circle dia, 5000 psi min compression strength, fuel and oil res, 150 deg F heat res
Canadian Commercial Corporation (98247)
Pratt and Whitney Canada Inc. (00198)

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2840-00-012-3279
2840000123279
PK251Cover, Shipping, Starter-GeneratorIII End Item Identification: Engine PT6A
General Characteristics Item Description: Plastic, yellow ana bulletin 166 no. 505 or C. g. s. b. 1-GP-12 no. 5-1, 4.236 in. min, 4.316 in. max lg, 4.236 in. min, 4.316 in. max W, 0.375 in. nom thk, 0.350 in. min, 0.390 in. max radius corners, 4 holes 0.340 min, 0.360 in. max dia on 5.000 in. bolt circle dia, 5000 psi min compression strength, fuel and oil res, 150 deg F heat res
Pratt and Whitney Canada Inc. (00198)

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2840-00-012-3283
2840000123283
1-060-030-01Vane, Inlet GuideIII End Item Identification: Engine T-53
General Characteristics Item Description: Cres AMS5510, rockwell 30 T scale 76 max hardness
Honeywell International Inc. (99193)

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2840-00-012-4184
2840000124184
446117
474619
Bracket Assembly, Case, DiffuserGeneral Characteristics Item Description: Cres, ams 5504, bracket material, consisting of three partno. 393798 spacers, one part no. 474618 bracket with dim. 0.085-0.101IN. thk, 2.565 in. lg, rockwell C30-38 hardness
III Fsc Application Data: Aircraft jet engine, TF33
United Technologies Corporation (77445, 52661)

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2840-00-012-4325
2840000124325
6842746Prop Brake Assy, ConeIII End Item Identification: Acft eng T56
Criticality Code Justification: AGAV
Allison Transmission Inc. (73342)
Rolls-Royce Corporation (63005)
General Motors Corp. (24617)

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2840-00-012-4659
2840000124659
2-160-293-04Lever, Interstage Air BleedIII End Item Identification: Engine T-55
General Characteristics Item Description: Aluminum alloy AMS4260, anodic film AMS2470, rockwell b scale 27 min, 60 max hardness, 2.540 in. nom lg, 0.330 in. min, 0.340 in. max W
Honeywell International Inc. (99193)
U S Army Aviation and Missile (81996)

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2840-00-012-5039
2840000125039
628449Manifold Assembly, Main BearingGeneral Characteristics Item Description: Thd internal tubefitting on each end
United Technologies Corporation (77445)

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2840-00-012-6005
2840000126005
S6135-20634-4Housing, Gearbox, Turbine EngineEnd Item Identification: H-3
Sikorsky Aircraft Corporation (78286)

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2840-00-012-7025
2840000127025
6843829Housing, Reduction Gear, AircraftCriticality Code Justification: AGAV
Engine Section Location: Accessory gearbox
Overall Length: 17.364 inches nominal
Allison Transmission Inc. (73342)
Rolls-Royce Corporation (63005)

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