00-176-8819
Compressor Aircraft Gas Tur Vane
00-176-8936
Gearbox Turbine Engine Housing
Housing assembly, gearbox rear
00-176-9171
Diffuser Turbine Engine Case
Used on aircraft model tf30-p-408.
00-177-8356
Axial Compressor Turbine En Disk
00-177-8879
Accessory Drive Turbine Gearbox
Used on j79, j85, t58, t64 aircraft engines.
00-177-9220
Turbine Nozzle Turbine Engi Vane
00-177-9222
Turbine Nozzle Turbine Engi Vane
00-177-9568
Combustion Aircraft Gas Chamber
00-177-9569
Combustion Aircraft Gas Chamber
00-177-9572
Combustion Aircraft Gas Chamber
00-177-9573
Combustion Aircraft Gas Chamber
00-178-0161
Turbine Nozzle Turbine Engi Vane
00-178-0270
Turbine Rotor Aircraft Gas Blade
00-178-0733
Aircraft Gas Turbine Compressor
00-178-0841
Turbine Aircraft Gas Turb Nozzle
Used on t-53 series engines.
00-178-0904
Turbine Engine Afterburner
00-178-0932
Turbine Aircraft Gas Turbi Rotor
Used on j47/j73/j79/j85/j93/t58/t64 aircraft engines. fscap
00-179-5521
Lubricating Oil Aircraft Ga Tank
00-179-5536
Aircraft Turbo-shaft Engine
Shaft hp rating
00-179-5538
Turbine Turbine Case And Nozzle
00-179-5656
Combustion Aircraft Gas Chamber
00-180-0782
Accessory Drive Turbine Gearbox
Major components 196885 1, 196886 1, 197744 1, 212925 1, 218680 1, 218893 1, 218679 1, 677814 1
00-181-0196
Augmentor Aircraft Gas Turb Case
Case afterburner
00-184-4980
Component Mounting Aircraf Plate
Used on tf-30 aircraft gas turbine engine. 0.880" overall length 0.203" overall width original name boss, chamber, combustion
00-184-4982
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.100" overall length
00-184-4983
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.100" overall length
00-184-4986
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.100" overall length
00-184-5017
Combustion Aircraft Gas Chamber
Used on tf-30 aircraft engine.
00-184-5031
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 1.480" overall length
00-184-5042
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 1.480" overall length
00-184-5046
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 1.730" overall length
00-184-5050
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.295" overall length
00-184-5072
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.740" overall length
00-184-5077
Combustion Chamber Aircraf Liner
Used on tf-30 aircraft engine. 2.955" overall length
00-184-5157
Combustion Chamber Aircraf Liner
Used on tf-30 acft eng. t.o. 2j-tf-24; liner fits up in the combustion can securing the nozzlesin place
00-185-1068
Compressor Aircraft Gas Tur Vane
Used on acft eng tf-39. 1.265" overall length 0.945" overall width original name vane, compressor stator, turbine engine
00-185-2904
Metallic Aircraft Gas Turbi Seal
Used on tf-33 aircraft gas turbine engine. orig name seal assembly, bearing consists of 1 p/n 563709 seal face assy, 18 p/ns 476966; 1 spring p/n 658221; 2 seal ring holder p/n 4998266 ; 3 seal rings 563717, pins
00-185-3554
Combustion Chamber Aircraft Case
Used on acft eng j57. 6.353" overall length original name case, centrifugal compressor, turbine engine
00-185-5990
Air Aircraft Gas Turbine En Seal
Used on acft eng tf-39. t.o. 2j-TF39-4
00-185-6252
Compressor Aircraft Gas Tur Disk
Used on j-60 aircraft engine. 1.172" overall length special features at tapered od; 2nd end od 12.264-12.274; was disk, axial compressor, turbine engine cadmium disk surface treated
00-185-6255
Compressor Aircraft Gas Tur Disk
Used on j-60 aircraft engine. 0.999" overall length original name disk, axial compressor, turbine engine cadmium disk surface treated
00-185-6256
Compressor Aircraft Gas Tur Disk
Used on j-60 aircraft engine. 0.860" overall length special features at tapered od; 2nd end od 13.935-13.945; was disk, axial compressor, turbine engine cadmium disk surface treated
00-187-0669
Labyrinth Aircraft Gas Seal Ring
Used on t-56 aircraft engine. 0.740" overall length
00-188-2211
Airflow Aircraft Gas Turb Baffle
Used on acft eng. 0.190" overall length 0.040" material thickness radius 12.25 in. min
00-190-3358
Heat Aircraft Gas Turbine Shield
Used on acft eng tf 33. 4.440" overall length
00-190-3364
Heat Aircraft Gas Turbine Shield
Used on acft eng tf33. 4.440" overall length 0.005" material thickness
00-191-2502
Diffuser Turbine Engine Case
Used on t-pt6a series engines. steel AMS5510; 0.370 in. min, 0.470 in. max material thk.
00-191-9392
Turbine Aircraft Gas Turbin Disk
Used on t-53 series engines.
00-192-0327
Turbine Aircraft Gas Turb Nozzle
Used on acft eng t58. isteel, stage 3, 13.770 min in. 13.810 max in.outside dia, 0.340 min.min.; 0.346 max in.dia of 8 holes; fitting matl ams 5645 tube matl ams 5580, tube ends in elliptical shape, for sealing braze matl ams 4770;
00-192-0329
Fan Aircraft Gas Turbi Blade Set
