01-448-6154
Combustion Aircraft Gas Chamber
Used on f100-pw-229 aircraft engine. original name chamber, combustion assy used on rear compressor; stage 1
01-448-6291
Compressor Aircraft Gas Tu Blade
01-448-6410
Air Aircraft Gas Turbine En Seal
Used on alliedsignal, t-55 mk714a aero engine.
01-448-6985
Compressor Aircraft Gas Tu Rotor
Used on f100-pw-229 aircraft gas turbine engine. original name rotor t.o. 2j-F100-54, fig 86, ind 1; location near the rear compressor drive turbine rotor
01-448-6986
Compressor Aircraf Vane Assembly
01-448-6990
Combustion Aircraft Gas Chamber
Used on f100-pw-229 aircraft gas turbine engine. t.o. 2j-F100-54, fig 86, ind 22; located near the rear compressor drive turbine rotor
01-448-6991
Compressor Aircraf Vane Assembly
01-448-6993
Compressor Aircraf Vane Assembly
01-448-6994
Combustion Aircraft Gas Chamber
Used on f100-pw-229 aircraft gas turbine engine. 8.258" overall length original name chamber, combustion, outer t.o. 2j-F100-54, fig 100, ind 23; combustion chamber assy; use only on p/n 4083194
01-448-6995
Compressor Aircraf Vane Assembly
01-448-6996
Combustion Aircraft Gas Chamber
Used on f100-pw-229 aircraft gas turbine engine. original name chamber, combustion, inner t.o. 2j-F100-54, fig 100, ind 35; combustion chamber assy; use only on p/ns 4083194, 4083560
01-448-7032
Air Aircraft Gas Turbine En Seal
Used on f100-pw-229 aircraft gas turbine engine. 1.475" overall length original name ring-air sealing, turbine assembly t.o. 2j-F100-54, fig 86, ind 4; location near the rear compressor drive turbine rotor
01-448-7033
Air Aircraft Gas Turbine En Seal
Used on f100-pw-229 aircraft gas turbine engine. 0.154" overall length 0.258" overall width original name brushseal, inner t.o. 2j-F100-54, fig 86, ind 19g; seal contains brush wire pack that has 2250-2650 wires per circumferential inch; use only on p/ns 4083194, 4083560
01-448-7034
Combustion Chamber Aircraf Liner
Used on acft eng f100pw229. 4.160" overall length liner segment combustion chamber duct, i id
01-448-7035
Air Aircraft Gas Turbine En Seal
Used on f100-pw-229 aircraft gas turbine engine. 0.258" overall length original name seal brush, combustion chamber, outer assembly t.o. 2j-F100-54, fig 86, ind 19f; use only on p/ns 4083194, 4083560,
01-448-7036
Combustion Chamber Aircraf Liner
Used on f100-pw-229 aircraft gas turbine engine. 6.157" overall length 1.456" overall width original name liner segment, combustion chamber t.o. 2j-F100-54, fig 100, ind 21; use only on p/n 4084089
01-448-7037
Combustion Chamber Aircraf Liner
Used on f100-pw-229 aircraft gas turbine engine. 6.157" overall length 1.456" overall width original name liner segment, combustion chamber duct t.o. 2j-F100-54, fig 100, ind 22; used only on p/ns 4084089
01-448-7038
Combustion Chamber Aircraf Liner
Used on f100-pw-229 aircraft gas turbine engine. 6.157" overall length 1.456" overall width original name liner segment, combustion chamber duct t.o. 2j-F100-54, fig 100, ind 20; use only on p/n 4084089
01-448-7511
Turbine Component Aircra Support
Used on f100-pw-229 aircraft gas turbine engine. 23.962" inside diameter 3.773" overall length 26.217" outside diameter original name support turbine duct use only on p/ns 4084517-700
01-448-7512
Compressor Aircraf Vane Assembly
Used on f100-pw-220 aircraft gas turbine engine. 4.717" overall length 2.036" overall width original name vane, turbine statorassembly 4.639-4.664 square inch flow area
01-448-7518
Compressor Aircraf Vane Assembly
Used on acft eng f100pw100. 4.615" overall length vane turbine stator, 3 stage, assembly of
01-448-7526
Combustion Chamber Aircraf Liner
Used on acft eng f100pw229 core. 4.276" overall length liner segment combustion chamber duct, 2 id
01-448-7539
Turbine Aircraft Gas Turbin Disk
Used on f100-pw-229 aircraft gas turbine engine. 1.809" overall length t.o. 2j-F100-54, fig 99, ind 42; use only on p/ns 4084517-700
01-448-7540
Turbine Aircraft Gas Turbin Case
Used on f100-pw-229 aircraft gas turbine engine. 5.809" overall length nt.o. 2j-F100-54, fig 89, ind 71; use only on p/n 4084522-800, -801, -802, 4082654-803,
01-448-7553
Combustion Chamber Aircraf Liner
Used on acft eng f100pw229 core. 4.276" overall length liner segment combustion chamber duct, 2 id
01-448-7554
Combustion Chamber Aircraf Liner
Used on acft eng f100pw229 core. 4.276" overall length liner segment combustion chamber duct, 2 id
01-448-7793
Aircraft Gas Cold Section Module
Used on pacer dawn. support module structure
01-448-7799
Combustion Aircraft Gas Chamber
Used on pacer dawn. combustion chamber
01-448-7807
Turbine Rotor Aircraft Gas Blade
Used on pacer dawn. blade turbine rotor
01-448-8347
Augmentor Flameholder Air Gutter
Used on f110-ge-400 for f14b/d.
01-448-9591
Turbine Blade Aircraft Retainer
01-449-0752
Compressor Blade Aircraft G Lock
Used on acft eng f100-pw-229. nickel alloy iaw ams 5596
01-449-0769
Air Aircraft Gas Turbine En Seal
Used on acft eng f100-pw-229.
01-449-1573
Combustion Chamber Aircraf Liner
Used on f100-pw-229 aircraft gas turbine engine. 9.660" overall length original name liner, augmentor combustion chamber assy t.o. 2j-F100-54, fig 65, ind 25; service repair for p/ns 4079666-01, 4080412-01, 4081214-01, 4083169-01, 4083180-01, 4083181-01
01-449-1759
Air Aircraft Gas Turbine En Seal
Used on ctcp85-180l apu.
01-449-2297
Turbine Blade Aircraft Retainer
01-449-2828
Air Aircraft Gas Turbine En Seal
Used on acft eng f100-pw-229.
01-449-2830
Air Aircraft Gas Turbine En Seal
Used on acft eng f100-pw-229.
01-449-2875
Exhaust Nozzle Control Parts Kit
Used on ch47d chinook helicopter.
01-449-3295
Compressor Aircraft Gas Tur Case
Used on f-16 aircraft.
01-449-3521
Compresso Case And Vane Assembly
Used on f110-ge-400 for f14b/d.
01-449-4089
Combustion Chamber Aircraf Liner
01-449-4491
Turbine Aircraft Gas Turbin Disk
Used on f110-ge-400 for f14b/d.
01-449-4493
Turbine Aircraft Gas Turbin Disk
Used on f110-ge-400 for f14b/d.
01-449-4495
Fan Aircraft Gas Turbine En Disk
Used on acft engine f110-ge-400 for f14b/d.
01-449-4496
Augmentor Flameholder Air Gutter
Used on f110-ge-400 for f14b/d.
01-449-6222
Compressor Case Aircraft Ga Plug
Application is C17 acft eng
01-449-6573
Turbine Aircraft Gas Turbin Disk
Used on acft eng f118ge100. 18.995" overall length tracking purposes only F118 used
01-449-6666
Augmenter Exhaust Aircraf Nozzle
Used on f110-ge-400(for f14b/d).
01-449-6929
Air Aircraft Gas Turbine En Seal
Used on f100-pw-100 acft gas turb eng. 1.575" overall length 0.945" overall width 0.020" material thickness original name seal, turbine stator use only on p/n nha 4083716-01
