FSC 2835 Non-Aircraft Gas Turbines, Jet Engines and Components: 2835-00-234-5682, 2835-00-240-6165, 2835-00-285-2672
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2835-00-234-5682 2835002345682 | 968886-1 | Nozzle, Turbine, Nonaircraft gas T | III End Item Identification: GTCP85-180/180L Special Features: First flange 12.235 in. min and 12.275 in. max od; second flange 11.745 in. min and 11.785 in. max od; 0.993 in. min and 1.008 in. max lg; 23 vanes each having 1 hole 0.302 in. min and 0.314 in. max by 0.615 in. min and 0.625 in. max Engine Section Location: Turbine | Honeywell International Inc. (99193) | |
| 2835-00-239-6534 2835002396534 | 710117 | Chamber, Combustion, Nonaircraft g | Special Features: 4 bosses equally spaced holes Overall Length: 12.680 inches minimum and 12.700 inches maximum | United Technologies Corporation (77445) | |
| 2835-00-240-6165 2835002406165 | 669J603PC45 667J692PC12 912C356H11 | Weight, Counterbalance | Northrop Grumman Systems Corporation (90099) Westinghouse Electric Corp. (79500) | ||
| 2835-00-241-7924 2835002417924 | 9102M35P01 | Blade, Steam Turbine | General Electric Company (07482) | ||
| 2835-00-242-1468 2835002421468 | 968808-2 | Plinum half Assembly | III End Item Identification: Part of compressor inlet on apu GTCP165-1 for C5A aircraf | Honeywell International Inc. (99193) | |
| 2835-00-244-5133 2835002445133 | 651078-1 | Modification kit, Engine | BE Aerospace Consumables Management (04795) Honeywell International Inc. (59364, 99193) | ||
| 2835-00-245-0474 2835002450474 | 694097 | Nozzle, Lubricating, Nonaircraft g | Special Features: Tubing matl. steel per MIL-T-6736; plug steel per MIL-S-6758; plug BORE0.035IN. dia; plug 0.250 in. min and 0.310 in. max long; optional matl for tubing MIL-T-6737; for plug QQ-S-763 Overall Length: 3.520 inches minimum and 3.530 inches maximum | Alliedsignal Inc. (72599) Honeywell International Inc. (99193, 70210) | |
| 2835-00-245-3025 2835002453025 | 26442-0-3 26442-3 | Diffuser and Sleeve | III End Item Identification: T-62T-11 gas tubrine engine for the H-46 series helicopters | Hamilton Sundstrand Corporation (55820, 99167) | |
| 2835-00-250-0466 2835002500466 | 696D102G2 | Seal, Metallic, Nonaircraft gas Tu | III End Item Identification: J79 engine III Part Name Assigned By Controlling Agency: Seal, honeycomb - turbine, stage 3 | General Electric Company (07482) | |
| 2835-00-255-3145 2835002553145 | 6172D90 395-063-021 | Housing, Liner | Reference Number Differentiating Characteristics: Magnetic permeability shall be less than 1.2 before fabricationand not greater than 2.0 after fabrication as measured in a 200OERSTED field by permeability indicator specified in military SPECMIL-I-17214 | Triumph Gear Systems Inc. (82402) Dresser-Rand Holdings LLC (12570) | |
| 2835-00-255-3148 2835002553148 | 395-599-202 | Bar, Locking | Reference Number Differentiating Characteristics: Magnetic permeability shall be less than 1.2 before fabricationand not greater than 2.0 after fabrication as measured in a 200OERSTED field by permeability indicator specified in military SPECMIL-I-17214 | Dresser-Rand Holdings LLC (12570) | |
| 2835-00-256-0374 2835002560374 | 969080-1 | Duct, Exhaust, Nonaircraft gas Tur | End Item Identification: 6115-00-420-8486 generator set, A/M32A-60A | Honeywell International Inc. (99193) | |
| 2835-00-256-0375 2835002560375 | 976016-1 5-830212 | Insulation Blanket, Thermal, Aircr | Thermal Structures Inc. (54787) Honeywell International Inc. (99193) | ||
| 2835-00-257-5080 2835002575080 | 395-527-202 | Lifting Attachment, | Dresser-Rand Holdings LLC (12570) | ||
| 2835-00-258-3990 2835002583990 | 2488595 | Socket, Balljoint | General Characteristics Item Description: 1.1942 in. min, 1.947 in. max, od, 0.437 in. min, 0.438 in. max, H | Goodrich Corporation (99551) | |
| 2835-00-258-8903 2835002588903 | RU41838A | Pipe Assembly, Fuel | Rolls-Royce Airlines (K0680) | ||
| 2835-00-258-8909 2835002588909 | RU9241 | Ball, Control rod | Rolls-Royce Airlines (K0680) | ||
| 2835-00-260-2819 2835002602819 | N202613 N205229 | Pipe Assy, Special | Goodrich Control Systems LTD T/A (K4358) | ||
| 2835-00-283-2411 2835002832411 | 968019-2 968019-3 968019-4 | Shroud Segment, Turbine, Nonaircra | Special Features: Aluminum alloy, QQ-A-250, 6061 TEMPER;12 holes 0.210 in min, 0.220 in max; finish per airesearch spec EMS52401, type 2, class a, all surfaces 125 microinch finish III Part Name Assigned By Controlling Agency: Shroud assembly, compressor Engine Section Location: Compressor | Honeywell International Inc. (99193) | |
| 2835-00-285-2672 2835002852672 | 42801-0 | Rotor Assy | Hamilton Sundstrand Corporation (55820) |