00-970-8921
Turbine Aircraft Gas Turb Nozzle
Nozzle, turbine, turbine engine
00-971-6279
Turbine Aircraft Gas Turb Nozzle
Cres AMS5532, 15.472 in.min, 15.502 in.max od, 4.207 in.min, 4.208 in.max id support, 24 holes 0.190 in.-32nf cl 2b thd through nozzle flange on 12.680 in.nom bolt circle dia, holes countersunk 90 deg by 0.220 in.nom dia, 6 holes 0.279 in.min, 0.291 in.max dia through support on 4.938 in.nom bolt circle dia, 15 holes 0.438 in.nom dia through support on 4.813 in.nom bolt circle dia, 3 holes 0.250 in.-28 unf cl 3b thd through support on 4.688 in.nom bolt circle dia, thd holes countersunk 90 deg 0.280 in.nom dia on vane trailing edge side;
00-971-6286
Axial Compressor Turbine En Case
00-971-6287
Turbine Rotor Aircraft Gas Blade
Blade, turbine, rotor turbine engine nickel alloy M3602 fscm 91547, rockwell c scale 35 min, 40 max hardness, 0.988 in. min, 0.991 in. max o/a w
00-971-6288
Turbine Rotor Aircraft Gas Blade
Blade, turbine, rotor turbine engine nickel alloy M3602 fscm 91547, rockwell c scale 35 min, 40 max hardness, 0.988 in. min, 0.991 in. max o/a w
00-971-9104
Compressor Aircraft Gas Turb Hub
Used on tf-33 aircraft engine. original name hub, compressor rotor, turbine engine
00-971-9106
Turbine Nozzle Turbine Engi Vane
00-972-3600
Turbine Aircraft Gas Turbi Rotor
Used on j-60 aircraft engine.
00-972-3601
Compressor Rotor Aircraft Spacer
Used on acft eng j60. 1.853" overall length
00-972-3602
Compressor Rotor Aircraft Spacer
Used on j-60 aircraft engine. 1.647" overall length 9.580" outside diameter do not use cadmium plated tools on this material, titanium
00-972-6899
Turbine Nozzle Aircraft Support
Used on acft eng. 24.120" inside diameter 1.435" overall length 25.900" outside diameter stiffener-turb nozzle, STG1
00-973-7713
Combustion Chamber Turbine Case
Used on j-57 aircraft engine.
00-974-8209
Combustion Chamber Turbine Case
00-975-0258
Turbine Aircraft Gas Turb Nozzle
2.983" overall length 15.525 min 15.54 max in. od; 5.588 min 5.59 max in. id support; 20 holes 0.19-32nf 3b thd through nozzle flange on 13.06 in. nom bolt circle dia; thd holes countersunk 90 deg by 0.22 in. nom dia; 3 holes 0.282 min 0.2825 max in. dia through nozzle flange on 13.06 in. nom bolt circle dia; 8 holes 0.34 in. nom dia through support on 6.16 in. nom bolt circle dia; 3 holes 0.19-32nf 3b thd through support on 6.16 in. nom bolt circle dia; thd holes countersunk 90 deg by 0.22 in. nom dia on vane trailing edge side
00-975-4414
Combustion Chamber Aircraf Liner
Used on acft eng j79, j85, t58, t64.
00-976-0044
Combustion Chamber Aircraf Liner
Used on acft eng j65. 21.860" overall length
00-976-1611
Compressor Aircraft Gas Tur Case
Used on tf-33 aircraft engine. t.o. 2j-TF33-4; goes on the 1st stage compressor outer
00-977-2120
Turbine Rotor Aircraft Gas Blade
Used on j85 aircraft engine.
00-977-3426
Compressor Vane Aircraft Damper
Used on acft eng j69.
00-977-6310
Fan Aircraft Gas Turbine En Case
Used on acft eng tf33.
00-977-6805
Augmentor Component Airc Support
Used on acft eng. 4.560" overall length fuel manifold hinge
00-977-7753
Lubricating Oil Aircraft Ga Tank
Used on acft eng tf33.
00-978-3000
Turbine Rotor Aircraft Ga Spacer
Used on acft eng tf33.
00-978-3010
Antifriction Bearing Air Housing
Used on acft eng tf33. 4.130" overall length
00-978-9956
Turbine Turbine Case And Nozzle
00-979-0880
Augmentor Component Aircra Liner
Used on acft eng j85.
00-979-6357
Heat Aircraft Gas Turbine Shield
00-979-6383
Antifriction Bearing Air Housing
Used on j-47,j-79,t-58,t-64 acft eng.
00-979-6631
Compressor Aircraft Gas Tur Vane
Used on tf-33 aircraft engine. original name vane, compressor stator, turbine engine
00-979-7518
Turbine Aircraft Gas Turbi Rotor
62 blades; 13.139 in. min 13.141 in. max od
00-979-7790
Thermal Aircr Insulation Blanket
Insulation blanket, thermal, turbine engine 29.250 in. dia, 9.750 in. lg
00-979-7792
Thermal Aircr Insulation Blanket
Insulation blanket, thermal, turbine engine 20.875 in. id, 9.438 in. lg
00-979-7794
Thermal Aircr Insulation Blanket
Insulation blanket, thermal, turbine engine 29.250 in. dia, 9.750 in. lg
00-979-8414
Metallic Aircraft Gas Turbi Seal
Used on t-53 series engine.
00-979-8418
Compressor Aircraft Gas Tu Rotor
Impeller, titanium alloy M3400, cage 91547, rockwell c scale 36 max hardness, coupling, steel AMS6371, rockwell c scale 26 min, 32 max hardness, black oxide finish AMS2485, 36 blades equally spaced
00-979-8432
Axial Compressor Tu Disk And Hub
Titanium alloy, M3400 fscm 91547, rockwell c scale 36 max hardness, painted finish, P6441 fscm 91547, 2.351 in. nom o/a lg, tapered od disk, 7.274 in. min, 7.284 in. max largest od disk, 7.146 in. min, 7.156 in. max smallest od disk, 0.677 in. min, 0.682 in. max lg disk, 38 blade grooves equally spaced on outer periphery, 2 hubs, 1st end 4.430 in. min, 4.440 in. max od hub, 1.202 in. min, 1.212 in. max distance from 1st end to disk, 2nd end 4.421 in. min, 4.422 in. max od hub, 0.453 in. min, 0.466 in. max distance from 2nd end to disk, 4.082 in. min, 4.087 in. max dia bore
00-979-9713
Augmentor Component Airc Support
Used on j-47,j-79,t-58 and t-64 aircraft engine. ring-middle, flameholder
00-980-0304
Antifriction Bearing Air Housing
Used on t-55 engines.
00-980-0740
Compressor Aircraft Gas Turb Hub
Used on acft eng tf33.
00-980-2658
Turbine Blade Aircraft Tu Damper
Used on acft eng tf33.
00-980-2666
Air Aircraft Gas Turbine En Seal
Used on tf-33 aircraft engine.
00-980-2669
Compressor Aircraft Gas Turb Hub
Used on tf-33 aircraft engine. 14.533" overall length original name hub, compressor rotor, turbine engine
00-980-2674
Compressor Aircraft Ga Blade Set
Used on acft eng tf33.
00-980-2675
Air Aircraft Gas Turbine En Seal
Used on acft eng tf33.
00-980-6265
Turbine Aircraft Gas Turbin Case
Used on t-56 aircraft engine.
00-980-9469
Turbine Aircraft Gas Turbin Case
Used on t-53 series engines. 7.867" overall length case, gas turbine engine
00-981-1761
Propeller Turbine Engine Shaft
Shaft, propeller, turbine engine
00-981-1762
Propeller Turbine Engine Shaft
Shaft, propeller, turbine engine
00-981-1804
Compressor Aircraft Gas Tur Vane
Used on tf-33 aircraft engine. 1.809" overall length compressor stator half 5 stage, assy of
00-981-1805
Turbine Aircraft Gas Turbi Rotor
Used on tf-33 aircraft engine.
