00-148-4098
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4099
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4101
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4102
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4106
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4110
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4111
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4112
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4113
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4114
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4115
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4116
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4117
Compressor Aircraft Gas Tur Vane
Used on tf-41 aircraft engine. original name vane, compressor stator, turbine engine
00-148-4120
Compressor Aircraft Gas Tu Blade
Used on tf-41 acft engine. original name blade, compressor rotor, turbine engine
00-148-6668
Aircraft Gas Turbine Compressor
Used on tf30-p412/412a engine.
00-148-7475
Combustion Aircraft Gas Chamber
Used on aircraft engine model tf30-p-408.
00-148-7476
Combustion Aircraft Gas Chamber
Used on aircraft engine model tf30-p-408.
00-148-7477
Combustion Aircraft Gas Chamber
Used on aircraft engine model tf30-p-408.
00-148-7503
Centrifugal Tur Compressor Rotor
Used on engine model j65-w-16a.
00-148-7914
Turbine Turbine Eng Disk And Hub
Used on t-55engine. cres M3702, fscm 91547, rockwell a scale 64.5 min, 69.0max hardness, tapered od disk, 9.494 in. min, 9.499 in. maxsmallest od, 9.909 in. min, 9.914 in. max largest od, 0.988 in.min, 0.991 in. max w disk, 56 blade grooves equally spaced onod, 4.499 in. nom o/a lg, 3.475 in.min, 3.485 in. max lg steppedhub, 2.548 in. -18 ns external thd 1st step, 2.5068 in. min, 2.5119 in. max pitch dia, 2.5589 in.min, 2.5593 in. max od 2ndstep, 2.750 in. min, 2.760 in. max od 3rd step, internal SPLINE42 teeth, 2.050 in. min, 2.055 in. max id, 2.1000 in. nom pitchdia, 30 deg pressure angle, 12 holes total through disklongitudinal to axis equally spaced on 3.380 in. nom boltcircle dia, 9 holes 0.313 in. min, 0.315 in. max dia, 9 holescountersunk both sides 60 deg by 0.350 in. min, 0.360 in. maxdia, 3 holes 0.2520 in. min, 0.2527 in. max dia, 3 holescountersunk both sides 90 deg by 0.270 in. nom dia
00-148-7919
Turbine Turbine Engine Disk
Used on t-55 series engines. cres, M3603, rockwell a scale 69 min, 73 max hardness, 11.430 in. min, 11.435 in. max od, 0.867 in. min, 0.870 in. max o/a lg, 3 holes through body, 0.2491 in. min, 0.2496 in. max dia holes, countersunk 60 deg by 0.290 in..min, 0.300 in. max dia both sides, holes equally spaced on 3.380 in. boltcircle dia, 9 holes through body, 0.350 in. min, 0.360 in. max dia holescountersunk 60 deg by 0.350 in. min, 0.360 in. max dia both sides, holesspaced on 3.380 in. nom bolt circle dia, 66 blade grooves equally spaced onouter periphery.
00-148-7944
Aircraft Gas Turbine Compressor
Used on aircraftmodel tf30-p-408.
00-148-7953
Axial Com Case And Vane Assembly
13 stage
00-148-9478
Exhaust Aircraft Gas Turbin Duct
Used on acft engine model tf30-p-408.
00-149-7965
Lubricating Aircraft Gas Nozzle
Anodize surface treated
00-149-8011
Gearbox Turbine Engine Housing
00-150-0141
Compressor Aircraft Gas Tu Rotor
Used on acft.eng. tf-41. original name compressor rotor, axial, turbine engine
00-150-1931
Heat Aircraft Gas Turbine Shield
00-150-1932
Heat Aircraft Gas Turbine Shield
Used on t-55engine. cres, ams 5510; 28 holes, 0.610 in. min., 0.620 in. max. dia
00-150-1936
Combustion Aircraft Gas Chamber
Used on t-55 series engines.
00-150-2366
Lubricating Aircraft Gas Nozzle
Aluminum alloy ams 4260 composition 356, temper-T6, anodized finish mil-a-8625, ty 1
00-150-5912
Turbine Aircraft Gas Turbi Rotor
Used on j79-10 aircraft engine. fscap
00-150-7225
Component Mounting Aircraf Plate
Used on tf39 aircraft engine. adapter assembly, starter
00-150-7229
Component Mounting Aircraf Plate
Used on tf39 aircraft engine.
00-150-7233
Fan Aircraft Gas T Vane Assembly
Used on acft eng tf-39.
00-150-7234
Compressor Blade Aircraft G Lock
Used on acft eng tf-39. 1.112" overall length 0.480" overall width original name lug, locking, compressor
00-150-7237
Compressor Blade Aircraft G Lock
Used on acft eng tf-39.
00-150-7241
Compressor Aircraft Gas Tu Rotor
Used on acft eng tf-39.
00-150-7246
Compressor Aircraft Gas Tu Blade
Used on acft eng tf-39. original name blade, compressor rotor, turbine engine
00-150-7247
Compressor Aircraft Gas Tu Blade
Used on acft eng tf-39. original name blade, compressor rotor, turbine engine
00-150-7344
Compressor Aircraft Gas Tu Rotor
00-150-7416
Compressor Aircraft Ga Blade Set
Used on TF33. nickel alloy, pwa 663, fscm 77445, consisting of two part no .516701 blades with dim. 3.878-3.910 in lg, 0.558-0.562 in. thk, 1.240-1.250 in. w
00-150-7424
Reduction Gear Aircraft Housing
00-150-7661
Compressor Aircraft Gas Tur Vane
00-150-7678
Compressor Aircraf Vane Assembly
00-150-7685
Turbine Rotor Turbine Engin Case
00-150-7804
Compresso Case And Vane Assembly
00-150-7807
Compressor Aircraft Gas Tur Vane
00-150-7866
Turbine Blade Set Turbine Rotor
00-150-7869
Axial Compressor Turbine En Disk
