00-573-8199
Compressor Aircraft Gas Tu Rotor
Used on aircraft engine tf41-a-2.
00-573-9738
Compressor Aircraft Gas Tu Blade
00-573-9740
Compressor Aircraft Gas Tu Blade
Blade, compressor rotor, turbine engine
00-573-9750
Heat Aircraft Gas Turbine Shield
00-573-9960
Antifriction Bearing Air Housing
Used on tf41 aircraft engine. t.o. 2j-TF41-r; gearbox cover; outer rear breather shaft; 11 pockets; use w/6860047
00-573-9981
Air Aircraft Gas Turbine En Seal
00-574-1679
Turbine Aircraft Nozzle Assembly
00-574-1685
Turbine Aircraft Nozzle Assembly
00-574-1695
Turbine Aircraft Nozzle Assembly
Used on engine,aircraft,turbofan,model f100pw100.
00-574-8641
Heat Aircraft Gas Turbine Shield
Used on j-69 aircraft engine.
00-575-1364
Antifriction Bearing Air Housing
Used on t-56 aircraft engine.
00-575-2170
Compressor Aircraft Gas Tu Blade
00-575-2222
Compressor Aircraft Gas Tu Blade
00-575-2224
Compressor Aircraft Gas Tu Blade
00-575-2225
Compressor Aircraft Gas Tu Blade
00-575-6688
Heat Aircraft Gas Turbine Shield
Used on j-75 aircraft engine.
00-575-8917
Heat Aircraft Gas Turbine Shield
Used on j-57 aircraft engine.
00-582-1471
Turbine Rotor Turbine Engin Case
Flange, cres AMS5645, body, cres AMS5510, rockwell b scale 90 max hardness, 125 microinch aa surface finish, 7.165 in. nom o/a lg, 19.240 in. nom od flange, tapered body, 18.279 in. min, 18.280 in. max largest od body, 16.730 in. min, 16.731 in. max smallest od body, tapered id, 16.560 in. min, 16.561 in. max smallest id countersunk 0.015 in. nom lg by 45 deg, 18.000 in. min, 18.001 in. max largest id countersunk 0.060 in. nom lg by 45 deg, 42 holes 0.271 in. min, 0.291 in. max dia through flange equally spaced on 18.740 in. nom bolt circle dia, 3 holes 0.190 in.-32 nf series cl 3b thd through flange on 18.740 in. nom bolt circle dia, thd holes countersunk 90 deg by 0.220 in. nom dia on back surface of flange, 3 thd holes, 0.250 in.-28 unf series cl 3b thd, through flange on 18.740 in. nom bolt circle dia, thd holes countersunk 90 deg by 0.280 in. nom dia on back surface of flange, 14 holes 0.256 in. min, 0.261 in. max dia through body equally spaced on outer periphery, 2.264 in. min, 2.274 in. ma
00-583-2529
Turbine Aircraft Gas Turbin Disk
00-583-2967
Bleed Turbine Engine Valve
Used on f-14 acft.
00-583-5484
Seal Aircraft Gas Turbin Housing
Used on engine,aircraft,turbofan,model f100pw100.
00-585-8555
Air Aircraft Gas Turbine En Seal
00-586-2970
Heat Aircraft Gas Turbine Shield
00-586-5846
Gearbox Turbine Engine Housing
Used on j-47,j-79,t-58 and t-64 aircraft engine.
00-587-3622
Gearbox Turbine Engine Housing
Used on t-53 series engines. c/o component qty, 13, 2 holes equally spaced;
00-587-3936
Accessory Drive Turbine Gearbox
Used on t-53 series engines.
00-587-8719
Thermal Aircr Insulation Blanket
00-588-3475
Turbine Aircraft Nozzle Assembly
Used on tf-30 aircraft engine.
00-588-5802
Turbine Aircraft Gas Turbi Shaft
00-588-5822
Augmentor Component Aircra Liner
Used on acft eng. 18.180" overall length liner, tailpipe phase 2 large
00-588-5823
Augmentor Component Aircra Liner
Used on acft eng. 11.160" overall length exhaust nozzle shell
00-588-7857
Heat Aircraft Gas Turbine Shield
Used on j-57 aircraft engine.
00-588-9285
Accessory Drive Turbine Gearbox
00-588-9324
Compressor Aircraft Gas Tu Rotor
Compressor rotor, axial, turbine engine
00-588-9341
Lubricating Aircraft Gas Nozzle
Used on j-75 aircraft engine.
00-588-9373
Antifriction Bearing Air Housing
Used on j-47,j-79,t-58 and t-64 aircraft engine.
00-589-4975
Afterburner Turbine Flameholder
Used on j-57 aircraft engine.
00-589-6760
Turbine Aircraft Gas T Blade Set
Used on J57.
00-589-6761
Compressor Aircraft Ga Blade Set
Used on j-57 aircraft engine.
00-589-6764
Turbine Aircraft Gas T Blade Set
Used on j-57 aircraft engine. blade set, turbine engine
00-589-6776
Compressor Aircraft Ga Blade Set
Used on J57. cres, ams 5616, hardness rockwell c 32-38, 5.399 in. MIN5.468 in. max lg, 1.743 in. min 1.753 in. max w, 3 blades required
00-589-6779
Compressor Aircraft Ga Blade Set
Used on J57.
00-589-6780
Compressor Aircraft Ga Blade Set
Used on J57.
00-589-8996
Component Mounting Aircraf Plate
Used on acft eng j-65. 16.230" overall length plate, oil pressure pump gear bearing
00-590-6927
Heat Aircraft Gas Turbine Shield
Used on j-75 aircraft engine.
00-590-6955
Compressor Aircraft Gas Tur Disk
Used on j-75 aircraft engine. was disk, axial compressor, turbineengine
00-590-7515
Lubricating Aircraft Gas Nozzle
Used on j-75 aircraft engine.
00-591-0731
Heat Aircraft Gas Turbine Shield
00-591-0741
Turbine Turbine Eng Disk And Hub
Cres, M3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. min, 3.815 in. max o/a lg, 9.820 in. nom od disk, 1.394 in.min, 1.397 in. max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. min, 2.840 in. max od 1st step 1st end, 0.700 in. nom lg 1st step 1st end, 3.320 in. nom dia 2nd step 1stend, 0.603 in. min, 0.607 in. max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 deg pressure angle, 2.8750 in.nom pitch dia, 0.380 in. min, 0.420 in. max lg splines, 0.681 in.min, 0.738 in. max lg 2nd step 2nd end, stepped bore, 3.805 in. min, 3.815 in. max o/a lg bore, 2.5576 in. min, 2.5579 in. max dia 1ststep 1st end, 0.950 in. nom lg 1st step 1st end, 2.566 in. min, 2.576 in. max dia 2nd step 1st end, 0.600 in. nom lg 2nd step 1stend, 2.2133 in. min, 2.2137 in. max dia 1st step 2nd end, 0.275 in.min, 0.295 in. max lg 1st step 2nd end, 2.425 in. min, 2.435 in. maxdia 2nd step 2nd end, 0.165 in. min, 0.205 in. max lg 2nd step 2ndend, internal splines 3rd s
00-592-4068
Turbine Turbine Engine Nozzle
