01-010-3129
Metallic Aircraft Gas Turbi Seal
Used on engine,aircraft,turbofan,model no. f100-pw-100. 7.850" overall length matl ams 5540
01-010-3755
Antifriction Bearing Air Housing
Used on acft eng. matl ams 5062
01-010-5616
Compressor Aircraft Gas Tur Case
Used on engine,acft,model j85ge5-13.
01-010-5841
Combustion Aircraft Gas Chamber
01-010-5941
Component Mounting Aircraf Plate
Rockwell 30t scale 76 max hardness, 0.840 in. nom lg, 0.420 in nom w, 0.240 in nom o/a h, 0.040 in nom shoulder located on one end, 0.040 in nom h shoulder, 0.220 in nom dia hole located on shoulder end, 0.210 in nom distance to hole center from edge along lg, 0.020 in nom distance to hole center from edge along w, 0.047 in min, 0.062 in max dia hole through corner on shoulder end, 25 deg min, 35deg max angle of corner hole on ll edge, 0.093 in min, 0.125 in from corner, 0.093 in min, 0.125 in max distance to corner hole center from corner, 0.093 in min, 0.125 in max distance to hole center from bottom edge along h, 0.165 in on end oppsite shoulder, 0.176 in min, 0.196 in max radius of slot end, 69 deg min, 79 deg max angle chamfer of slot w/shoulder of slot radius on side w/shoulder, 85 deg min, 95 deg max angle chamfer of slot radius on side oppsite shoulder
01-010-5949
Turbine Aircraft Gas Turbi Rotor
66 blades; 12.935 in. min 12.937 in. max od
01-010-8306
Combustion Aircraft Gas Chamber
01-011-5045
Antifriction Bearing Air Housing
Surface, phosphate ams 2481; 5.5635 in. o/a lg.; 6.312 in. min., 6.313 in. max. o/a dia.; flange located on one end; rockwell c scale 23 max hardness; 1.380 in. min., 1.390 in. max. o/a lg.; 6.440 in. o/a dia.; 0.420 in. w of face; 1st step 0.670 in. min., 0.690 in. max. lg.; 3.800 in. od; 2nd step 0.140 in. min., 0.150 in. max. lg; 4.901 in. min., 4.903 in. max. od; 3rd step 0.140 in. lg.; 5.000 in. od; bore, 3.140 in. id; 0.820 in. min., 0.830 in. max. dp; counterbore, 4.620 in. id; 0.560 in. dp; flange located on opposite end; rockwell c scale 23 max. hardness; 1.430 in. o/a lg; 6.060 in. o/a dia.; 0.320 in. w of face; 1st step 0.780 in. min., 0.790 in. max. lg.; 3.800 in. od; 2nd step 0.180 in. min., 0.200 in.max. lg.; 4.901 in. min., 4.903 in. max. od; 3rd step 0.130 in. min., 0.140 in. max. lg.; 5.000 in. od; bore, 3.140 in. id; 0.780 in. min., 0.790 in. max. dp; counterbor, 4.620 in. id; 0.460 in. dp; each flang, 15 holes 0.440 in. dia.
01-012-4153
Compressor Aircraft Gas Tu Rotor
01-012-6471
Turbine Aircraft Gas Turbin Disk
Used on engine,aircraft,turbofan,model no. f100-pw-100. disk, gas turbine engine
01-012-7548
Lubricating Oil Aircraft Ga Tank
Used on aircraft model sh-3h.
01-013-0481
Air Aircraft Gas Turbine En Seal
Used on engine,aircraft,turbofan,model no. f100-pw-100.
01-013-1339
Aircraft Turbo-shaft Engine
Shaft hp rating
01-013-1599
Air Aircraft Gas Turbine En Seal
Used on engine,aircraft,turbofan,model no. f100/pw/100. 0.185" overall length 0.135" overall width t.o. 2j-F100-14, fig 134, ind 1
01-013-1703
Turbine Aircraft Gas Turbin Disk
Used on engine,aircraft,turbofan,model no. tf39-ge-1a. 0.505" overall length original name disk, turbine, turbine engine
01-013-1706
Turbine Aircraft Gas Turb Nozzle
Used on engine,aircraft,turbojet,model no. j85-ge-21. 2.028" overall length t.o. 2j-J85-94; to be renamed nozzle assy, turbine, gas turbine engine
01-013-1967
Turbine Aircraft Gas Turb Nozzle
Used on engine,aircraft,turbojet,model no. j85-ge-21. 1.997" overall length t.o. 2j-J85-94; to be renamed nozzle assy, turbine, gas turbine engine
01-013-4707
Turbine Rotor Aircraft Ga Spacer
Used on engine,acft,turbofan,model no.tf39-ge-1a.
01-013-5152
Front Aircraft Gas Turbine Frame
Used on engine,aircraft,turbojet model no. j85-ge-5k.
01-013-5153
Turbine Aircraft Gas Turbin Disk
Used on engine,afct,turbofan,model no. tf39-ge-1a. 2.340" overall length
01-013-5154
Combustion Chamber Aircraft Case
Used on engine,acft,turbofan,model no. f100-pw-100.
01-013-5155
Fan Aircraft Gas Turbine En Duct
Used on f-100-p-100.
01-013-6460
Axial Compressor Turbine En Disk
Used on j57-p engine.
01-013-9227
Turbine Rotor Aircraft Gas Blade
Used on acft eng tf41. 2.8110" overall length
01-013-9896
Turbine Aircraft Gas Turbi Shaft
Used on engine,aircraft,turbofan,model no. tf39-ge-1a. 7.329" overall length
01-014-2755
Combustion Chamber Aircraf Liner
Used on engine,acft,turbofan,model no. f39-ge-1a.
01-014-4053
Compressor Aircraft Gas Tur Disk
Used on j57 jet engine.
01-014-4054
Compressor Aircraft Gas Tur Disk
Used on j57 jet engine.
01-014-4473
Compressor Aircraft Gas Tu Rotor
Used on engine,acft,turbofan,model no. tf39-ge-1a.
01-014-4474
Compressor Aircraft Gas Tu Blade
Used on engine,acft,turbofan,model no. tf39-ge-1a. original name blade, compressor rotor, turbine engine
01-014-4475
Compressor Aircraft Gas Tu Blade
Used on engine,acft,turbofan,model no. tf39-ge-1a. original name blade, compressor rotor, turbine engine
01-014-4476
Compressor Aircraft Gas Tu Blade
Used on engine,acft,turbofan,model no. tf39-ge-1a. original name blade, compressor rotor, turbine engine
01-014-6069
Compressor Vane Assembly Spacer
01-014-8431
Combustion Chamber Aircraf Liner
Used on acft eng j79. 12.030" overall length
01-015-0480
Compressor Aircraft Gas Tu Blade
Used on engine,acft,turbofan,model no. tf39-ge-1a. original name blade, compressor rotor, turbine engine
01-015-1751
Combustion Chamber Aircraf Liner
Used on j-79 aircraft turbine engines. 12.030" overall length used on -7b, -11a, -11b
01-015-2432
Air Aircraft Gas Turbine En Seal
Used on engine model j79.
01-016-1793
Seal Aircraft Gas Turbin Housing
Used on acft eng j75. matl ams 5613
01-016-2043
Gearbox Turbine Engine Housing
Used on acft eng tf-33.
01-016-3163
Turbine Engine Afterburner
Used on aircraft model f-4.
01-016-3181
Compressor Stator Turbine E Vane
Used on j57-p-16 engine.
01-016-3182
Compressor Stator Turbine E Vane
Used on engine model j57.
01-016-3184
Compressor Stator Turbine E Vane
Used on engine model j57.
01-016-3193
Compressor Aircraft Gas Tur Disk
Used on j57 jet engine.
01-016-3194
Compressor Aircraft Gas Tur Disk
Used on j57 jet engine.
01-016-3195
Turbine Aircraft Gas Turbin Disk
Used on engine model j57-p. steel PWA768 fscm 77445, nickel-cadmium plated AMS2416-4, 75 blade slots
01-016-3196
Turbine Aircraft Gas Turb Nozzle
Used on engine model tf34-ge-2.
01-016-3197
Compressor Aircraf Vane Assembly
Used on j65-w-16a engine.
01-016-3896
Turbine Aircraft Gas Turbi Rotor
Used on engine,acft,turbofan,model no. f100-pw-100.
01-016-5752
Combustion Aircraft Gas Chamber
Used on engine,acft,turbofan,model no. f100-pw-100.
