01-321-4455
Compressor Aircraft Gas Tur Vane
Used on f100pw0229 aircraft engine. 4.721" overall length t.o. 2j-F100-54; 4-9th stages; 58units per assy; rear compressor, variable inlet nickel vane surface treated
01-321-4456
Air Aircraft Gas Turbine En Seal
Used on f100 aircraft engine. 1.836" overall length
01-321-4457
Air Aircraft Gas Turbine En Seal
Used on f100pw0229 aircraft engine. 2.636" overall length 0.060" material thickness t.o. 2j-F100-54
01-321-4458
Air Aircraft Gas Turbine En Seal
Used on f100pw0229 engine. 2.062" overall length 0.060" material thickness t.o. 2j-F100-54
01-321-4459
Aircraft Gas Turbine Compressor
Used on f100pw0229 acft engine. 6.712" overall length 2j-F100-54; includes stages 10-12; 2nd end dia. 20.906
01-321-5571
Compressor Component Air Support
Used on f100pw0229 aircraft engine. 0.778" overall length
01-321-5572
Compressor Component Air Support
Used on f100pw0229 aircraft engine. 0.778" overall length
01-321-7855
Turbine Aircraft Shroud Segment
Used on acft eng f100pw0229.
01-321-7856
Turbine Aircraft Shroud Segment
Used on acft eng f100pw0229.
01-321-7857
Turbine Aircraft Shroud Segment
Used on acft eng f100pw0229.
01-321-7858
Turbine Aircraft Gas Turbin Case
Used on acft eng f100pw0229.
01-321-7861
Turbine Aircraft Nozzle Assembly
Used on acft eng f100pw0229. fan exit guide vanes
01-321-7917
Air Aircraft Gas Turbine En Seal
Used on acft engine f100pw229.
01-322-0256
Metallic Aircraft Gas Turbi Seal
Used on t700-ge-701. seal, metallic, special material AMS5596, N07718 nickel alloy 718; stk thk prior to forming 0.009 in min, 0.011 in max; outside DIA13.959 in min, 13.971 in max; free height 0.222 in min, 0.232 in max
01-322-1721
Gearbox Turbine Engine Housing
Used on f16-aircraft (f100-pw-200). purchase description identification: 77445-t. o. 2j-F100 (v) -512
01-322-2051
Turbine Aircraft Shroud Segment
Used on f100pw0229 aircraft engine. 0.532" overall length 3.825" overall width 0.050" material thickness t.o. 2j-F100-54; 35 holes eq sp 0.520-0.540
01-322-3277
Metallic Aircraft Gas Turbi Seal
Used on acft eng f100pw0229.
01-322-4293
Metallic Aircraft Gas Turbi Seal
Used on acft eng j-52.
01-322-4570
Turbine Aircraft Shroud Segment
Used on f110ge100 acft eng. 1.661" overall length 0.335" overall width
01-322-4571
Turbine Aircraft Shroud Segment
Used on f110ge100 aircraft engine. 1.661" overall length 0.331" overall width
01-322-4572
Turbine Aircraft Shroud Segment
Used on f110ge100 aircraft engine. 1.661" overall length 0.328" overall width
01-322-4573
Turbine Aircraft Shroud Segment
Used on f110ge100 aircraft engine. 1.661" overall length 0.324" overall width
01-322-4574
Turbine Aircraft Shroud Segment
Used on f110ge100 aircraft engine. 1.661" overall length
01-322-4746
Turbine Aircraft Shroud Segment
Used on acft eng f110ge100.
01-322-4747
Turbine Aircraft Shroud Segment
Used on acft eng f110ge100.
01-322-4748
Turbine Aircraft Shroud Segment
Used on acft eng f110ge100.
01-322-4749
Turbine Aircraft Shroud Segment
Used on acft eng f110ge100.
01-322-4752
Turbine Aircraft Shroud Segment
Used on f100pw0229 aircraft engine. 0.855" overall length
01-322-4754
Turbine Aircraft Gas Tur Fairing
Used on f110 ge 129 acft engine. 4.890" overall length section is 110 deg. of the full case
01-322-4755
Turbine Aircraft Gas Tur Fairing
Used on f110 ge 129 acft engine. 4.890" overall length 0.068" material thickness section is 140 deg. of full case
01-322-4756
Turbine Aircraft Gas Turbin Case
Used on f110ge129 acft eng. 4.890" overall length 0.068" material thickness section is 110 deg. of the full case
01-322-4757
Compressor Aircraft Gas Tu Blade
Used on f110ge129 aircraft engine. 3.798" overall length blade is dovetail
01-322-4758
Compressor Aircraft Gas Tur Disk
Used on f110ge129 aircraft engine. 11.953" overall length spline data: no. of teeth 50; pitch dia. 5.102; pressure angle 14 deg. 30 min.; o/a dia. 5.040
01-322-4759
Compressor Aircraft Gas Tu Rotor
Used on f110ge129 aircraft engine. 6.143" overall length includes 1-2 stages
01-322-4760
Compressor Aircraft Gas Tu Rotor
Used on f110ge129 aircraft engine. 14.506" overall length includes 4-9 stages
01-322-4761
Aircraft Gas Turbine Compressor
Used on f100pw0229 aircraft engine.
01-322-4763
Gearbox Turbine Engine Housing
Used on acft eng f110ge129. 14.845" overall length
01-322-4764
Heat Aircraft Gas Turbine Shield
Used on pacer special.
01-322-4765
Heat Aircraft Gas Turbine Shield
Used on pacer special.
01-322-4766
Heat Aircraft Gas Turbine Shield
Used on pacer special.
01-322-4797
Compressor Aircraft Ga Blade Set
Used on F100. t.o. 2j-F100-54; 46 units per assy; 2nd stage; goes on the front compressor rotor
01-322-4798
Compressor Aircraft Ga Blade Set
Used on F100. t.o. 2j-F100-54; 42 units per assy; 3rd stage; goes on the front compressor rotor
01-322-5347
Turbine Aircraft Gas Turbin Case
Used on acft eng f110ge129.
01-322-5349
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
01-322-5350
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
01-322-5351
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
01-322-5352
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
01-322-5353
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
01-322-5354
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100. 11 vanes per assembly; needs 2 units per assembly
01-322-5355
Compressor Aircraf Vane Assembly
Used on acft eng f110ge100.
