00-172-4277
Compressor Aircraft Gas Tur Vane
Used on acft eng tf-39. 1.191" overall length 0.951" overall width original name vane, compressor stator, turbine engine
00-172-4278
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
00-172-4279
Combustion Chamber Aircraft Case
Used on acft eng tf-39.
00-172-4295
Compresso Case And Vane Assembly
Used on acft.eng. tf39. original name case
00-172-4432
Combustion Chamber Aircraft Duct
Used on acft eng tf33. matl ams 5536
00-172-4437
Air Aircraft Gas Turbine En Seal
Used on acft eng j85.
00-172-6919
Air Aircraft Gas Turbine En Seal
00-172-7394
Compressor Aircraft Gas Tur Disk
Used on j-60 aircraft engine. original name disk, axial compressor, turbine engine
00-173-3302
Air Aircraft Gas Turbine En Seal
Used on acft eng tf-39.
00-175-0357
Axial Com Case And Vane Assembly
Mtg data, 16 bolt holes 0.180 in. min, 0.186 in. max dia, 5.1040 in.bolt circle dia, 5.540 in. o/a dia of case.
00-175-1387
Lubricating Aircraft Gas Nozzle
Irregular shape; 2.505 in. o/a lg.
00-175-3486
Component Mounting Aircraf Plate
Used on j-85 aircraft engine. 0.990" overall length
00-175-5499
Air Aircraft Gas Turbine En Seal
Used on acft eng tf-39. 5.480" overall length t.o. 2j-TF39-4
00-175-5537
Turbine Aircraft Gas Turb Nozzle
Major components 1 ea air seal 3900T98G01, 1 ea air deflector 3002T07P01, 29 ea airfoils;
00-175-8163
Turbine Aircraft Gas Turbi Rotor
Used on tf-33 aircraft engine.
00-176-3386
Compressor Aircraft Gas Tu Rotor
Used on acft eng tf-39. 47.991" overall length original name compressor rotor, axial, turbine engine
00-176-3579
Turbine Aircraft Gas Turb Nozzle
Used on t-53 series engines. brazing alloy ams 4776, 18 holes equally spaced, 10 tangs equally spaced, 0.490 in.min, 0.494 in.max, 5 places;
00-176-3691
Compressor Aircraf Vane Assembly
Cres AMS5504; rockwell c scale 20 min 28 max hardness of band; 13 vanes equally spaced
00-176-3692
Compressor Aircraf Vane Assembly
Cres AMS5504; rockwell c scale 26 min 34 max hardness of band; 7 vanes equally spaced
00-176-3694
Aircraft Gas Turbine Compressor
00-176-3734
Compressor Aircraft Gas Tur Disk
Used on tf-33 aircraft engine. 4.518" overall length original name disk, axial compressor, turbine engine
00-176-3739
Accessory Drive Turbine Gearbox
00-176-3745
Centrifugal Tur Compressor Rotor
Used on t-53 series engines. titanium alloy M3403, fscm 91547, shot peened AMS2430, 36 blades, 13.048 in. min, 13.051 in. max od, 4.8694 in. min, 4.8700 in. max id bore, 12 holes 0.337 in. min, 0.344 in. max dia on 5.440 in. nom bolt circle dia, 3 thd holes on 5.440 in. nom bolt circle dia, 0.250-28unf class 2b thd, thd holes countersunk 90 deg by 0.280 in. nom dia, 12 holes 0.154 in. min, 0.159 in. max dia 0.150 in. nom deep on 5.290 in. nom bolt circle dia.
00-176-3746
Axial Compressor Tu Disk And Hub
Used on t-53 series engines. 1 hole on ea blade groove, 2 holes equally spaced 0.065 in. min, 0.070 in. max dia, 8 holes equally spaced 0.120 in. nom dia, 10 holes equally spaced, 12 holes equally spaced 0.330 min, 0.337 max dia, 16 holes equally spaced, 34 places
00-176-3750
Axial Compressor Tu Disk And Hub
Cres, M3710 fscm 91547, passivated finish, P6402 fscm 91547, rockwell c scale 37 min, 44 max hardness, 4.577 in. min, 4.589 in. max o/a lg, 1st end tapered disk, 5.872 in. min, 5.882 in. max smallest od disk, 5.927 in. min, 5.937 in. max largest od disk, 1.121 in. min, 1.123 in. max lg disk, 31 blade grooves equally spaced on outer periphery of disk, 2nd end stepped hub, ext thd 2nd end, 1.750 in.-16 un series cl 3a thd, 0.356 in. min, 0.376 in. max lg thd, 1.645 in. min, 1.655 in. max od 1st step 2nd end, 0.150 in. nom lg 1st step 2nd end, ext splines 2nd step 2nd end, 45 teeth, 30 deg pressure angle, 1.9137 in. min, 1.9167 in. max od, 1.8750 in. nom pitch dia, 0.163 in. min, 0.173 in. max lg splines, 1.725 in. min, 1.735 in. max od 3rd step 2nd end, 0.120 in. nom lg 3rd step 2nd end, 1.9685 in. min, 1.9687 in. max DIA4th step 2nd end, 1.060 in. min, 1.062 in. max lg 4th step 2nd end, 2.220 in. nom od 5th step 2nd end, 30 deg taper by 0.310 in. nom lg 5th step 2nd end, 2.4360 in. min, 2.4365 in. max od 6th st
00-176-3751
Turbine Aircraft Gas Turbi Shaft
Used on ah-1,uh-1,ov-1 turbine engine,external spline data, full fillet-side bearing fit,number of teeth-50,diametral pitch-24/48,pressure angle 30.
00-176-3752
Compressor Aircraft Gas Tu Blade
Used on ah-1 turbine engine.
00-176-3756
Compressor Aircraft Gas Tu Blade
Used on t-53 series engines.
00-176-3758
Compressor Aircraft Ga Blade Set
Used on t-53 series engines. cres, AMS5745, rockwell c scale 35 min, 44 max hardness, packaged in pairs w/0.10 grams max weight variance
00-176-3759
Compressor Aircraft Ga Blade Set
Used on t-53 turbine engine.
00-176-3773
Compressor Aircraft Ga Blade Set
Used on t-53 series engines. cres, AMS5745, rockwell c scale 35 min, 44 max hardness, packaged in pairs w/0.50 grams max weight variance
00-176-3780
Compressor Aircraft Gas Tu Blade
Used on t-53 series engines.
00-176-3782
Compressor Aircraft Gas Tu Blade
Used on t-53 series engines.
00-176-3788
Compressor Aircraft Ga Blade Set
Used on t-53 series engines. cres, AMS5745, rockwell c scale 35 min, 44 max hardness, packaged in pairs w/0.10 grams max weight variance
00-176-3789
Compressor Aircraft Ga Blade Set
Used on t-53 series engines. cres, AMS5745, rockwell c scale 35 min, 44 max hardness, packaged in pairs w/0.10 grams max weight variance
00-176-3791
Compressor Aircraft Gas Tu Blade
Used on t-53 series engines.
00-176-3812
Turbine Aircraft Gas Turbi Shaft
00-176-3813
Gearbox Turbine Engine Housing
00-176-3915
Turbine Nozzle Turbine Engi Vane
00-176-4046
Axial Com Case And Vane Assembly
00-176-8478
Exhaust Aircraft Gas Turbin Cone
Used on engine,t-63.
00-176-8479
Exhaust Aircraft Gas Turbin Cone
Used on engine,t-63.
00-176-8496
Heat Aircraft Gas Turbine Shield
00-176-8683
Compressor Aircraf Vane Assembly
00-176-8753
Turbine Aircraft Gas Turbi Rotor
Used on t-53 series engines. consists of ring assembly 1; blade 66; disc 2. flight safety critical aircraft part
00-176-8777
Fan Aircraft Gas Turbine En Vane
Nickel alloy
00-176-8778
Fan Aircraft Gas Turbine En Vane
Nickel alloy
00-176-8795
Fan Aircraft Gas Turbine En Vane
Nickel alloy
00-176-8806
Fan Aircraft Gas Turbine En Vane
Nickel alloy
00-176-8818
Compressor Aircraft Gas Tur Vane
