FSC 2840 Aircraft Prime Moving Gas Turbines and Jet Engines and: 2840-00-011-5623, 2840-00-012-0021, 2840-00-012-7025
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
2840-00-011-5623 2840000115623 | 577166 | Cover, Turbine Stator Vane | III 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) | |
2840-00-011-5951 2840000115951 | 625879 | Patch, Combustion | United Technologies Corporation (77445) | ||
2840-00-011-9952 2840000119952 | 572081 | Stop, Power Lever Cr | United Technologies Corporation (77445) | ||
2840-00-012-0017 2840000120017 | 589426 | Mount, Ignition EXC1 | United Technologies Corporation (77445) | ||
2840-00-012-0021 2840000120021 | 538992 | Stiffener, Combustio | United Technologies Corporation (77445) | ||
2840-00-012-0023 2840000120023 | 572195 | Piston, Anti-Icing | United Technologies Corporation (77445) | ||
2840-00-012-0827 2840000120827 | 407682 | Boss, Diffuser Case | III 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) | |
2840-00-012-0835 2840000120835 | 611659N9 | Blade set, Turbine R | Curtiss-Wright Controls Inc. (0AHP5) | ||
2840-00-012-3269 2840000123269 | PK242 | Cover, Shipping, Oil Vent | General 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) | |
2840-00-012-3271 2840000123271 | PK425 | Cover, Shipping, Engine Mount | General 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) | |
2840-00-012-3276 2840000123276 | PK1841 PK4471 PK257 | Cover, Shipping, Propeller Shaft | General 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) | |
2840-00-012-3277 2840000123277 | PK255 | Cover, Shipping, Tachometer Mount | III 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) | |
2840-00-012-3279 2840000123279 | PK251 | Cover, Shipping, Starter-Generator | III 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) | |
2840-00-012-3283 2840000123283 | 1-060-030-01 | Vane, Inlet Guide | III End Item Identification: Engine T-53 General Characteristics Item Description: Cres AMS5510, rockwell 30 T scale 76 max hardness | Honeywell International Inc. (99193) | |
2840-00-012-4184 2840000124184 | 446117 474619 | Bracket Assembly, Case, Diffuser | General 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) | |
2840-00-012-4325 2840000124325 | 6842746 | Prop Brake Assy, Cone | III End Item Identification: Acft eng T56 Criticality Code Justification: AGAV | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) General Motors Corp. (24617) | |
2840-00-012-4659 2840000124659 | 2-160-293-04 | Lever, Interstage Air Bleed | III 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) | |
2840-00-012-5039 2840000125039 | 628449 | Manifold Assembly, Main Bearing | General Characteristics Item Description: Thd internal tubefitting on each end | United Technologies Corporation (77445) | |
2840-00-012-6005 2840000126005 | S6135-20634-4 | Housing, Gearbox, Turbine Engine | End Item Identification: H-3 | Sikorsky Aircraft Corporation (78286) | |
2840-00-012-7025 2840000127025 | 6843829 | Housing, Reduction Gear, Aircraft | Criticality Code Justification: AGAV Engine Section Location: Accessory gearbox Overall Length: 17.364 inches nominal | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) |