01-005-0284
Compressor Aircraft Gas Tur Vane
Used on engine,acft,turbofan,model no. f100pw100. 4.525" overall length original name vane, compressor stator, turbine engine
01-005-2763
Antifriction Bearing Air Housing
Used on j79 engine.
01-005-3050
Turbine Aircraft Gas Turbi Rotor
Used on engine turbojet,model no. j85ge-13 and j85ge-17a. fscap
01-005-3517
Turbine Aircraft Gas Turbin Disk
Used on engine model tf30-p-412,tf30-p-412a.
01-005-4196
Compressor Aircraft Gas Tur Vane
Used on engine,aircraft,model no. tf39-ge1a. 2.4483" overall length original name vane, compressor stator, turbine engine
01-005-4699
Compressor Aircraft Gas Tu Rotor
01-005-5477
Heat Aircraft Gas Turbine Shield
11.400" overall length
01-005-5889
Turbine Aircraft Gas Turbi Shaft
Used on tf41 engine. 35.585" overall length
01-005-7004
Gearbox Turbine Engine Housing
Used on engine,aircraft,turbojet,modelj69.
01-005-7012
Exhaust Aircraft Gas Turbin Cone
Used on engine,acft,turbofan,model f100pw100. 11.770" overall length
01-005-8172
Turbine Aircraft Gas Turbi Rotor
Used on acft eng j85ge21.
01-005-8701
Exhaust Aircraft Gas Turbin Cone
Used on engine,aircraft,turbofan,model no. f100pw100. 11.770" overall length
01-005-9994
Compressor Aircraft Ga Blade Set
Used on engine model tf 30.
01-006-0033
Compressor Stator Turbine E Vane
Used on tf30 engine.
01-006-1116
Compressor Aircraft Gas Tur Vane
Used on engine,aircraft,model no. tf39-ge-1a. 2.4483" overall length original name vane, compressor stator, turbine engine
01-006-1117
Turbine Aircraft Nozzle Assembly
Used on engine,aircraft,model t56.
01-006-1118
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. nom 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 dia 4th 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 tapered 30 deg, 0.310 in. nom lg 5th step 2nd end, 2.423 in. min, 2.431 in. max od 6th step 2nd end, 0.820
01-006-1299
Turbine Aircraft Gas Turbin Case
Used on tf-33 acft eng. 2.639" overall length originally case, turbine rotor, turbine engine
01-006-3028
Turbine Aircraft Gas Turbine Hub
Used on engine,aircraft,model no. j69t25. 1.610" overall length
01-006-3657
Thermal Aircr Insulation Blanket
01-006-4537
Turbine Aircraft Gas Turbi Rotor
Used on engine model t58.
01-006-7424
Fan Vane Aircraft Gas Tur Spacer
Used on engine,aircraft,turbofan,model no. tf39-ge1a. 0.840" overall length
01-006-7425
Fan Aircraft Gas T Vane Assembly
Used on engine,aircraft,turbofan,model no. tf39-ge1a.
01-007-4231
Compressor Ai Synchronizing Ring
Used on j-85 aircraft gas turbine eng. 0.525" overall length 19.120" outside diameter original name ring, actuating, inlet used on the inlet guide vane front frame assy
01-007-4233
Augmentor Aircraft Gas Turb Case
Used on engine,aircraft,model no. j85-ge-13.
01-007-4281
Turbine Aircraft Nozzle Assembly
01-007-4282
Compressor Aircraf Vane Assembly
01-007-5441
Turbine Rotor Aircraft Gas Blade
Used on t-53 series engine. blade, turbine rotor, turbine engine, nickel alloy M3602 FSCM91547, rockwell c scale 35 min, 40 max hardness, 1.6607 in. min, 1.6617 in. max o/a lg
01-007-5442
Turbine Rotor Aircraft Gas Blade
Used on j79 engine. 5.850" overall length 1.530" overall width 0.668" material thickness
01-007-8108
Accessory Drive Turbine Gearbox
Used on aircraft engine model t57-ge-16a.
01-007-8375
Turbine Aircraft Gas Turbi Rotor
Part of T64-ge-7 engine
01-007-9113
Turbine Aircraft Nozzle Assembly
01-008-0562
Augmentor Component Aircra Liner
Used on engine,aircraft,turbofan,model no. f100-pw-100. 1.990" overall length matl ams 5596
01-008-0563
Combustion Chamber Aircraf Liner
Used on engine,acft,turbofan,model no. f100-pw-100.
01-008-1548
Combustion Chamber Aircraf Frame
Used on engine,aircraft,turbofan,model no. t34-ge-100.
01-008-1550
Heat Aircraft Gas Turbine Shield
Used on engine,aircraft,turbofan,model no. tf39-ge-1a.
01-008-1628
Turbine Aircraft Gas Turbin Disk
Used on engine,aircraft,model no. j85-ge-17. original name disk, turbine, turbine engine
01-008-4442
Compressor Aircraft Gas Tur Vane
Used on tf33 aircraft engine. 2.230" overall length compressor stator 13 stage, asst of
01-008-5729
Compressor Aircraft Gas Tur Case
Used on ah-1, uh-1, ov-1 tubine engine, rotary wing aircraft. housing assy, first compressor, sub-assy
01-008-5730
Combustion Chamber Aircraft Case
Used on ah-1, uh-1, ov-1 tubine engine, rotary wing aircraft. housing assy, impellar
01-008-5731
Combustion Chamber Aircraft Case
Used on ah-1, uh-1, ov-1 tubine engine, rotary wing aircraft. housing, combustion chamber assy
01-008-5732
Axial Com Case And Vane Assembly
Housing assembly encases the following; vane assy-second stage; vane assyfirst stage; vane assy-exit guide; vane assy-fourth stage; and vane assy-third stage; t-53 series engines
01-008-5733
Exhaust Aircraft Gas Turbin Cone
Used on ah-1, uh-1, ov-1 tubine engine, rotary wing aircraft.
01-008-5734
Antifriction Bearing Air Housing
Used on t-53 series engines.
01-008-5982
Turbine Aircraft Gas Turbi Rotor
Used on t-53 series engines. 62 blades, 13.397 in. min, 13.399 in. max od. flight safety critical aircraft part
01-008-5983
Turbine Aircraft Gas Turbi Rotor
Used on t-53 series engines. 66 blades, 12.120 in. min, 12.122 in. max od, counterclockwise rotation. flight safety critical aircraft part
01-008-5984
Combustion Aircraft Gas Chamber
Icres, AMS5536, rockwell 15t scale 83 min., 92.5 max. hardness, 15.500 in. nom. o/a od; 2.480 in. nom. o/a lg.; 0.040 in. min., 0.044 in. max. thk material, 88 slots 0.020 in. min., 0.030 in. max. w on od breaking into 88 holes 0.094 in. nom. dia equally spaced on od; 0.640in. nom. distance from end to hole centers; 11.712 in. nom. od inner wall; 50 louvers equally spaced on inner wall, 0.390 in. nom. effective lg. louver; 0.0795 in. nom. inside h louver
01-008-5985
Turbine Aircraft Gas Turb Nozzle
5.588 in.min, 5.590 in.max id support, 3 holes 0.2820 in.min, 0.2825 in.max dia through nozzle flange on 13.060 in.nom bolt circle dia, 20 holes 0.263 in.min, 0.270 in.max dia on 13.060 in.nom bolt circle dia, countersunk 60 deg to 0.325 in.nom dia on vane trailing edge side, 8 holes 0.340 in.nom dia through support on 6.160 in.nom bolt circle dia, 3 holes 0.190 in.-32 unf cl 3b thd through support 6.160 in.nom bolt circle dia, thd holes countersunk 90 deg to 0.220 in.nom dia on vane trailing edge side, 2.993 in.min, 2.998 in.max length;
01-008-5986
Turbine Aircraft Ga Disk And Hub
Used on t53 series engine.
01-008-7887
Turbine Rotor Aircraft Gas Blade
Blade, turbine, rotor turbine engine cres, M3612 fscm 91547, rockwell c scale 34 min, 40 max hardness, 0.988 in. min, 0.991 in. max o/a w
