00-153-4096
Turbine Aircraft Gas Turbin Case
Used on acft eng j57. matl ams 5645
00-153-8349
Compressor Rotor Turbine E Blade
00-153-8353
Aircraft Gas Turbine Compressor
00-155-4632
Compressor Rotor Turbine E Blade
00-155-4633
Aircraft Gas Turbine Compressor
00-156-8763
Compressor Rotor Turbi Blade Set
00-156-8911
Diffuser Turbine Engine Case
Used on aircraft engine model tf30-p-8.
00-156-9227
Antifriction Bearing Air Housing
Used on T56. 2.127" overall length
00-156-9440
Compressor Aircraft Gas Tu Rotor
Used on j-85 aircraft engine. original name compressor rotor, axial, turbine engine
00-156-9472
Centrifugal Compressor Turb Case
00-156-9474
Antifriction Bearing Air Housing
00-156-9477
Compressor Aircraf Vane Assembly
00-156-9485
Compressor Aircraf Vane Assembly
00-156-9777
Compressor Aircraf Vane Assembly
00-156-9782
Antifriction Bearing Air Housing
00-156-9816
Metallic Aircraft Gas Turbi Seal
Used on acft eng. 0.172" overall length id 0.725 in. min
00-157-0707
Turbine Aircraft Gas Turb Nozzle
Used on t-55 series engines. wcres, AMS5532, AMS5769
00-157-0897
Axial Compressor Turbine En Case
00-157-1054
Turbine Aircraft Ga Disk And Hub
Used on acft.eng. tf-41. original name disk
00-157-1055
Turbine Aircraft Gas Turbi Rotor
Used on acft.eng. tf-41.
00-157-1283
Fan Aircraft Gas Turbine E Blade
00-157-1346
Compressor Aircraft Gas Tur Case
Used on acft eng tf-41.
00-157-1538
Gearbox Turbine Engine Housing
00-157-1541
Heat Aircraft Gas Turbine Shield
00-157-1603
Combustion Aircraft Gas Chamber
00-157-1615
Combustion Aircraft Gas Chamber
00-157-1622
Combustion Aircraft Gas Chamber
00-157-1645
Axial Com Case And Vane Assembly
00-157-2348
Combustion Aircraft Gas Chamber
00-157-2374
Turbine Aircraft Gas Turbin Disk
36 holes, one on cl of ea groove, 2 tangs equally spaced, 2 slots equally spaced, 36 blades grooves equally spaced, 24 places equally spaced
00-157-2375
Turbine Aircraft Gas Turbin Disk
Used on t-53 series engines. 1.637" overall length steel, AMS4135, black chromic anodized finish, 6.570 in. min, 6.580 in. max o/a od, 1.637 in. nom o/a lg, 4.082 in. min, 4.087 in. max id, 34 blade grooves equally spaced on outer peripwery, 34 holes 0.094 in. min, 0.097 in. max dia by 0.095 in. min, 0.105 in. max depth equally spaced on groove centerlines anodize surface treated
00-157-2643
Fan Aircraft Gas Turbine E Blade
00-157-2655
Heat Aircraft Gas Turbine Shield
00-157-2777
Heat Aircraft Gas Turbine Shield
00-157-2781
Axial Com Case And Vane Assembly
00-157-2800
Axial Com Case And Vane Assembly
00-157-2984
Axial Compressor Turbine En Disk
00-157-2985
Axial Compressor Turbine En Disk
00-157-2986
Gearbox Turbine Engine Housing
00-157-2994
Lubricating Aircraft Gas Nozzle
00-157-2995
Lubricating Aircraft Gas Nozzle
00-157-3002
Compressor Aircraft Gas Turb Hub
Hub, compressor rotor, turbine engine
00-157-3100
Turbine Aircraft Gas Turb Nozzle
Nozzle, turbine, turbine engine
00-157-3347
Carrier Planetary Reduction Gear
Used on t-pt6a series engines. core rockwell c scale 30 min 40 max hardness rating; 5 holes equally spaced; 50 teeth; 10 holes equally spaced
00-157-3349
Compressor Component Air Support
Used on j-65 aircraft engine.
00-157-3605
Turbine Aircraft Gas Turbi Rotor
3.945" overall length 58 blades; 8.547 min 8.549 max in. o/a od; 1st end stepped hub; 1.12 min 1.1207 max od 1st step 1st end; 0.2 min 0.21 max lg 1st step 1st end; ext splines 2nd step 1st end; 38 teeth; 30 deg pressure angle; 1.2188 in. nom pitch dia 0.54 min 0.57 max in. lg 2nd step 1st end; 1.11 min 1.13 max od 3rd step 1st end; 0.07 min 0.08 max in. lg 3rd step 1st end; 1.3 min 1.3007 max in. od 4th step 1st end; 0.155 min 0.16 max in. lg 4th step 1st end; 1.82 min 1.83 max in. od 5th step 1st end; 6th step 1st end tapered:1.675 min 1. 685 max smallest od; 0.635 min 0.705 max in. lg 6th step 1st end; 1.77 min 1.825 max lg from 1st end to disk; 2nd end plain hub; 1.408 min. 1.412 max in. od hub 2nd end ; 0.495 min 0.515 max in. lg from 2nd end to disk; 4 holes 0.208 min 0.212 max in. dia; 0.125 min 0.145 max in. lg 5th step 1st end
00-157-3619
Compressor Aircraft Gas Tu Blade
Used on t-pt6a series engines. cadmium blade surface treated
00-157-3623
Compressor Aircraft Gas Tu Blade
Used on t-pt6a series engines. cadmium blade surface treated
00-157-3625
Turbine Engine Afterburner
Used on engine model j79. components include nozzel 1, turnbuckle 4, actuator 4, blanket 4, manifold 1, cap 5, bracket 4, gasket 2, washer 33, pulley 1, cover 2, clamp 14, strap 8, duct 1, rod 4, shaft 3, tube 10, bolt 149, pin 17, key 8, nut 101, tee 1
00-157-3633
Compressor Aircraft Ga Blade Set
Used on TF33. consisting of 2 ea blade, compressor rotor, turbine engine-titaniumalloy, AMS4928, 17.073 in. max lg, 3.920 in. max w, 0.985 in. max thk
