01-374-0876
Turbine Component Aircraft Liner
Used on acft eng f110ge129. 5.480" overall length
01-374-1205
Turbine Aircraft Gas Turbin Case
Used on tf-34 engine. case, gas turbine engine
01-374-1232
Antifriction Bearing Air Housing
Used on t-56 engine.
01-374-1547
Combustion Chamber Aircraf Liner
01-374-1552
Turbine Aircraft Gas Turbi Shaft
01-374-1946
Gearbox Turbine Engine Housing
Used on ah-64a. 15.050" overall length
01-374-2482
Compressor Aircraft Gas Tu Blade
Used on f100pw229. 1.468" overall length 0.758" overall width
01-374-3986
Turbine Engine Parts Kit
01-374-3987
Turbine Engine Parts Kit
01-374-4000
Turbine Component Aircra Support
Used on t55-l-712f engine. support, power turbine, turbine engine
01-374-4001
Turbine Component Aircra Support
Used on t55-l-712f/hma.
01-374-4687
Combustion Aircraft Gas Chamber
Used on tf30-p-414a engine. posted louvers, thermal barrier coating, revised louver cooling
01-374-4833
Compressor Blade Aircraft G Lock
Used on f100pw229 acft eng core. 1.411" overall length 0.701" overall width 0.071" material thickness 44 units per assy; 1 per 2 statorvanes
01-374-8488
Compressor Aircraft Gas Tu Blade
Used on f100pw0229 aircraft engine/core. 1.598" overall length 0.810" overall width blade attachment is dovetail; t.o. 2j-F100-54; 2 units per assy; use only on 4079287-01, 4080405-01, 4080720-01, 4080812-01, and 4080884-01
01-374-8489
Turbine Rotor Aircraft Gas Blade
2.642" overall length 2.065" overall width 0.085" material thickness blade, turbine engine
01-374-8490
Compressor Aircraf Vane Assembly
Used on f100pw0229 aircraft engine/core. 6.769" overall length t.o. 2j-F100-54; includes 11
01-374-8491
Compresso Case And Vane Assembly
Used on f100-pw-229 acft engine;softened coating pwa 279 the vane. t.o. 2j-F100-54, fig 88, ind 46; includes stgs 10-12; use only on 4068722-807
01-374-8498
Turbine Engine Afterburner
Used on engine f110-ge400.
01-374-9396
Turbine Aircraft Gas Turbine Hub
Used on f16 aircraft engine.
01-374-9593
Compressor Blade Aircraft G Lock
Used on f100-229. 0.489" overall length
01-374-9594
Compressor Blade Aircraft G Lock
Used on f100pw229. 0.445" overall length
01-375-1407
Turbine Aircraft Gas Turbin Case
Used on pacer special. 2.060" overall length
01-375-1408
Compressor Aircraft Gas Tu Blade
Used on f100pw100/200/220 acft engines. t.o. 2j-F100-14
01-375-1409
Fan Aircraft Gas Turbine E Blade
Used on f100pw100/200/220 acft engines. t.o. 2j-F100-14
01-375-1410
Turbine Rotor Aircraft Gas Blade
Used on acft eng f100pw229/fdt.
01-375-1411
Fan Aircr Case And Vane Assembly
Used on pacer dawn. 1st stage case
01-375-1413
Turbine Aircraft Nozzle Segment
Used on f100pw220 aircraft engine. original name nozzle assembly, turbine, aircraft gas turbine engine t.o. 2j-F100-24, fig 133, ind 32; 1.769-1.787 sq in total area; 1 unit per assy; has borescope hole for inspection
01-375-1414
Turbine Aircraft Nozzle Segment
Used on f100pw220 aircraft engine. original name nozzle assembly, turbine, aircraft gas turbine engine t.o. 2j-F100-4; 1.805-1.823 sq. in. total area between individual vanesin segment to allow frequency work forairflow, 1unit per assy; has borescopehole for inspection
01-375-1415
Turbine Aircraft Nozzle Segment
Used on f100pw220 aircraft engine. original name nozzle assembly, turbine, aircraft gas turbine engine t.o. 2j-F100-4; 1.823-1.842 sq. in. total area between individual vanesin segment to allow frequency work forairflow, 1 unit per assy; has borescope hole for inspection
01-375-1416
Turbine Aircraft Nozzle Segment
Used on acft eng f100pw220. original name nozzle assembly, turbine, aircraft gas turbine engine spacing between vanes 1.734 min. 1.751 max. square"
01-375-1417
Turbine Aircraft Nozzle Segment
Used on acft eng f100pw220. original name nozzle assembly, turbine, aircraft gas turbine engine 1.751-1.769 sq. in. area; t.o. 2JF100-24, fig 133, ind 32
01-375-1474
Compressor Aircraft Ga Blade Set
Used on F100. t.o. 2j-F100-14; used on the 1st stg compressor rotor; copper-nickel coating
01-375-1475
Compressor Aircraft Ga Blade Set
Used on F100. t.o. 2j-F100-14; used on the rearfan case; 2nd stage disk
01-375-1497
Combustion Chamber Aircraf Liner
Assembly consists of a ferrule nozzle, a retainer, a doubler, a swirl cup comb, a baffle outer, a dome liner, a baffle inner, a plate swirl cup, a weld wire, a dummy swirl cup,
01-375-1498
Turbine Component Aircra Support
Used on f110-129 acft engine.
01-375-2102
Augmentor Component Airc Support
Used on tf-30 aircraft engine. 39.595" inside diameter 0.930" overall length 39.819" outside diameter
01-375-2458
Turbine Aircraft Shroud Segment
Used on t64 engine. mfr describes as shroud segment, turbine-stage 2
01-375-6452
Component Mounting Aircraf Plate
01-375-6469
Compressor Aircraft Gas Tu Rotor
Used on engine model t700. rotor, compressor, gas turbine engine
01-375-9660
Turbine Aircraft Shroud Segment
01-375-9738
Turbine Aircraft Gas Turbi Shaft
01-376-1008
Air Aircraft Gas Turbine En Seal
0.100" material thickness matl ams 5536 ribbon thk .0027-.0033; hex across flats 0.052 in to 0.072 in
01-376-1009
Air Aircraft Gas Turbine En Seal
0.110" material thickness material ams 5536 ribbon thk .0027-.0033; hex across flats 0.052in to 0.072in
01-376-1087
Turbine Blade Aircraft Tu Damper
Damper, turbine blade, turbine engine material ams 5538 ; damper, blade-stg 2 turbine.
01-376-1572
Compressor Aircraf Vane Assembly
Used on f100-229.
01-376-3595
Turbine Blade Aircraft Tu Damper
01-376-3859
Combustion Aircraft Gas Chamber
Used on b0-150 c helicopter.
01-377-0307
Component Mounting Aircraf Plate
0.140" material thickness
01-377-2362
Turbine Aircraft Gas Turb Nozzle
Used on acft eng f110 ge129.
01-377-2418
Turbine Aircraft Gas Turb Nozzle
Used on acft eng f101. nozzle assembly, shroud, seals
