00-938-3684
Compressor Aircraft Gas Tur Vane
00-938-3685
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
00-938-3698
Compressor Aircraft Gas Turb Hub
Hub, compressor rotor, turbine engine
00-938-3699
Compressor Aircraft Gas Turb Hub
Hub, compressor rotor, turbine engine
00-938-3701
Turbine Aircraft Shroud Segment
Nickel alloy ams 5665; segment subtends 180 deg arc; 0.859 in. min 0.869 in. max w; 0.875 in. min 0.895 in. max h; honeycomb core nickel alloy ams 5540; 0.003 in. min 0.004 in. max thk stock which is brazed to shroud; color coded green
00-938-3702
Turbine Aircraft Shroud Segment
Znickel alloy ams 5665; segment subtends 180 deg arc; 0.859 in. min 0.869 in. max w; 0.875 in. min 0.895 in. max h; honeycomb core nickel alloy ams 5540; 0.003 in. min 0.004 in. max thk stock which is brazed to shroud; color coded red
00-938-3703
Turbine Aircraft Shroud Segment
Nickel alloy ams 5665; segment subtends 180 deg arc; 0.859 in. min 0.869 in. max w; 0.875 in. min 0.895 in. max h; honeycomb core nickel alloy ams 5540; 0.003 in. min 0.004 in. max thk stock which is brazed to shroud; color coded blue
00-938-3755
Gearbox Turbine Engine Housing
00-938-3756
Gearbox Turbine Engine Housing
00-938-3823
Compressor Aircraft Gas Tur Vane
00-938-3838
Exhaust Aircraft Gas Turbin Duct
Used on j52-p-6b.
00-938-3841
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
00-938-3842
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
00-938-3847
Combustion Chamber Turbine Case
00-938-3850
Fan Aircraft Gas T Vane Assembly
Vane assembly, stator, turbine engine
00-938-3851
Fan Aircraft Gas T Vane Assembly
Vane assembly, stator, turbine engine
00-938-3854
Turbine Turbine Engine Nozzle
00-938-3858
Gearbox Turbine Engine Housing
00-938-3860
Aircraft Gas Tu Turbine Assembly
00-938-3864
Turbine Aircraft Gas Turbi Rotor
Used on acft eng t56. fscap
00-938-3866
Turbine Turbine Eng Disk And Hub
00-938-3867
Turbine Turbine Engine Disk
00-938-3868
Turbine Aircraft Gas Turbin Disk
Used on acft eng t56. original name disk, turbine, turbine engine
00-938-3869
Turbine Aircraft Gas Turbin Disk
Used on acft eng t56. original name disk, turbine, turbine engine
00-938-4429
Combustion Chamber Aircraf Liner
Used on acft eng t56. 24.804" overall length
00-938-9846
Combustion Chamber Aircraft Case
Used on acft eng j57.
00-938-9850
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
00-938-9851
Compressor Aircraft Gas Tu Blade
Used on acft engine j60. greek ascaloy; 2.074 in. max lg
00-939-0254
Turbine Rotor Aircraft Gas Blade
00-939-1518
Diffuser Aircraft Gas Turbi Case
Used on tf-33 aircraft engine.
00-939-3395
Axial Compressor Turbine En Disk
00-939-3446
Lubricating Aircraft Gas Nozzle
00-939-3447
Lubricating Aircraft Gas Nozzle
Used on tf-30 aircraft engine. 0.930" overall length
00-939-3453
Air Aircraft Gas Turbine En Seal
Used on acft eng tf30. 0.977" overall length
00-939-3459
Compressor Blade Aircraft G Lock
Used on acft eng tf30.
00-939-3460
Compressor Blade Aircraft G Lock
Used on acft eng tf30.
00-939-3461
Compressor Blade Aircraft G Lock
Used on acft eng tf30.
00-939-3480
Heat Aircraft Gas Turbine Shield
Used on tf30 eng.
00-939-3481
Heat Aircraft Gas Turbine Shield
Used on tf30 eng.
00-939-5649
Bearing Aircraft Gas Tur Support
Used on acft eng j85.
00-939-5985
Lubricating Aircraft Gas Nozzle
Used on tf-30 aircraft engine. 2.573" overall length
00-939-8962
Antifriction Bearing Air Housing
00-939-9361
Air Aircraft Gas Turbine En Seal
Used on acft eng tf33.
00-939-9363
Compressor Aircraft Gas Tur Duct
Used on acft eng tf33. 1.895" overall length
00-940-8452
Turbine Aircraft Gas Turbi Rotor
Used on t63-a-700 and t63-a-720 engines. cres, EMS73634 fscm 73342, 44 blades, 7.170 in. min, 7.172 in. max o/a od, 1.319 in. min, 1.321 in. max o/a lg, 1st end hub, ext splines, 20 teeth, 30 deg pressure angle, 1.938 in.-24 ext thd located 0.090 in. nom distance from 1st end, 0.250 in. nom thd lg, 10 holes 0.200 in. nom dia equally spaced on od hub, 0.520in. nom c to c distance from 1st end to holes, 2nd end hub, ext splines, 20 teeth, 30 deg pressure angle, stepped id, 1.1585 in. min, 1.1590 in. max smallest id.flight safety critical aircraft part
00-940-8632
Air Aircraft Gas Turbine En Seal
00-940-8724
Turbine Aircraft Gas Turbi Rotor
Turbine rotor, turbine engine
00-940-8725
Turbine Aircraft Gas Turb Nozzle
Cres, AMS5382
00-940-8753
Oil Sump Aircraft Gas Tu Housing
00-941-0847
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
