Non-Aircraft Gas Turbines, Jet Engines and Components: 713088-1C, 72034, 7-2041
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 713088-1C 7130881C | 2835-01-032-8911 | Bellows, Flexible Co | Arrowhead Products Corporation (70628) | ||
| 713813 | 2835-00-108-4196 | Blade, Turbine Rotor, Nonaircraft | Special Features: Nickel alloy | United Technologies Corporation (77445) | |
| 713814 | 2835-00-108-2356 | Blade, Turbine Rotor, Nonaircraft | Special Features: Nickel alloy | United Technologies Corporation (77445) | |
| 713815 | 2835-00-108-1943 | Blade, Turbine Rotor, Nonaircraft | Special Features: Nickel alloy | United Technologies Corporation (77445) | |
| 7138342 | 2835-01-503-5532 | Stiffener, Flat | III End Item Identification: 3930-01-486-2151 | JLG Industries Inc. (1YHH8) Trak International (3Y949) | |
| 7138843 | 2835-01-503-5548 | Stiffener, Flat | III End Item Identification: 3930-01-486-2151 | JLG Industries Inc. (1YHH8) Trak International (3Y949) | |
| 714266 | 2835-01-003-5719 | Lead Assembly, Turbi | Unison Industries LLC (59501) | ||
| 714266 | 2835-01-004-7313 | Cable Assembly, Power, Electrical, | Special Features: Four connectors, no. 16 awg conductor size, 19 strand per conductor, overbraid to be nickel and welded to connector backshells, shield to be copperand electrically isolated from other shields, overbraid and connector backshells | Unison Industries LLC (59501) | |
| 714792 | 2835-00-142-8543 | Cone, Exhaust, Nonaircraft gas Tur | Material: Steel overall Hardness Rating: 24.0 rockwell C minimum and 35.0 rockwell C maximum overall | United Technologies Corporation (77445) | |
| 715J408 PIECE 27 715J408PIECE27 | 2835-01-181-5110 | Nozzle, Lubricating, Nonaircraft g | Material: Steel cone | Northrop Grumman Systems Corporation (90099) | |
| 71664 | 2835-00-731-6319 | Spacer, Exhaust Door | General Characteristics Item Description: Stainless steel, 0.440 in. od, 0.220 in. id, 0.737 in. lg | Teledyne Technologies Inc. (03104) | |
| 71885 | 2835-01-212-2940 | Kit, Seal | Eaton Corporation (77842) | ||
| 71A160014-1001 71A1600141001 | 2835-01-453-1533 | Duct, Exhaust, Nonaircraft gas Tur | End Item Identification: Used on 71A160019 part of GR-7 and T10 aircraft engine bay vent | Boeing Company, The (76301) | |
| 71A160014-1003 71A1600141003 | 2835-01-478-4257 | Duct, Exhaust, Nonaircraft gas Tur | End Item Identification: AV8B, GRMK5, TAV8B, and harrier GR7/T10 aircrafts Material: Glass fiber and plastic phenolic duct Engine Section Location: Exhaust | Boeing Company, The (76301) | |
| 72016 | 2835-00-869-1850 | Spacer set, Bearing | Honeywell International Inc. (99193) | ||
| 72018 | 2835-00-707-8284 | Block, Governor Drive | General Characteristics Item Description: Matl:sae 1113 steel rod per QQ-5-633, good to medium machine finish all over;dim.: 0.480 in. min and 0.510 max lg, 0.5630 in. min and 0.5640 in. max od | Alliedsignal Inc. (72599) Honeywell International Inc. (70210) | |
| 7202701407 | 2835-01-228-5841 | Housing, Gearbox, Turbine Engine | Daimler AG (D8046) | ||
| 72028 | 2835-00-040-2959 | Fan Assembly, Oil Cooler | General Characteristics Item Description: Assembly consists of P/N 75470-3 fan 1EA, P/N 72062-5 fan al alloy 61ST6 cond T spec QQ-A-325 1EA, P/N 75471 hub steel 4130 MIL-S-6758 a/W steel EMS-626 1EA;3.010 in. min 3.020 in. max od, 0.3755 in. min 0.3758 in. max id | Honeywell International Inc. (99193) | |
| 72032 | 2835-00-033-1774 | Carrier Assembly | General Characteristics Item Description: Assembly consists of P/N 72033 sleeve gear brg 1EA;P/N 72034 pressed insert 4EA;P/N 72057 carrier 1EA;PN S8152B2-0-180 pin 1EA | Alliedsignal Inc. (72599) Honeywell International Inc. (70210,99193) | |
| 72034 | 2835-00-033-1776 | Insert, Bearing Carrier | III Fsc Application Data: Compressor section, GTC85-71 and GTGE85-70A | Alliedsignal Inc. (72599) Honeywell International Inc. (70210,99193) | |
| 7-2041 72041 | 2835-01-073-8030 | Blade, Compressor, Nonaircraft gas | END Item Identification: 2350-01-087-1095;2350-01-136-8738 Special Features: Mounted on compressor rotor of turbine engine to create air flow in compressor section Part Name Assigned BY Controlling Agency: Blade, compressor rotor, turbine engine | Doncasters Inc. (25818) |