01-438-4175
Heat Aircraft Gas Turbine Shield
Used on c130j hercules fixed wing aircraft.
01-438-4177
Heat Aircraft Gas Turbine Shield
Used on c130j hercules fixed wing aircraft.
01-438-6189
Turbine Aircraft Gas Turbin Duct
Used on f100-pw-229 aircraft gas turbine engine. 4.080" overall length 1.597" overall width 2nd stage segment
01-438-6547
Compressor Aircraft Gas Tur Vane
Used on pacer dawn. 8.736" overall length 0.723" overall width 2nd end width 0.295-0.305; variable inlet guide vane
01-438-6874
Heat Aircraft Gas Turbine Shield
Used on fixed wing aircraft, hercules model c-130j.
01-438-6905
Heatshield Aircraft Ga Stiffener
01-438-8397
Compressor Aircraft Gas Tu Rotor
Used on f118-ge-100 aircraft gas turbine engine. 6.143" overall length original name spool, compressor rotor t.o. 2j-F110-14, fig 67, ind 5 under p/n 1559M63G02; includes stage 2; also consists no. 1 disk
01-438-8398
Compressor Aircraft Gas Tu Rotor
Used on f101-ge-102 aircraft gas turbine engine. 6.143" overall length original name spool, compressor rotor t.o. 2j-F110-14, fig 67, ind 5 under p/n 1559M63G02; includes stage 2; also consists no. 1 disk
01-438-8399
Compressor Aircraft Gas Tu Rotor
Used on f110-ge-129 aircraft gas turbine engine. 6.143" overall length original name spool, compressor rotor t.o. 2j-F110-14, fig 67, ind 5 under p/n 1559M63G02; includes stage 2; also consists no. 1 disk
01-438-8400
Compressor Aircraft Gas Tu Rotor
Used on f110-ge-100 aircraft gas turbine engine. 6.143" overall length original name spool, compressor rotor t.o. 2j-F110-14, fig 67, ind 5 under p/n 1559M63G02; includes stage 2; also consists no. 1 disk
01-438-9420
Turbine Aircraft Nozzle Segment
01-438-9874
Air Aircraft Gas Turbine En Seal
01-439-1231
Compressor Aircraft Gas Tur Vane
Used on pacer dawn. 0.723" overall length material titanium alloy per ems 54924
01-439-1259
Turbine Aircraft Gas Turb Nozzle
Used on acft eng f108. vane-hpt nozzle
01-439-1262
Turbine Aircraft Nozzle Segment
Used on acft eng f108. 4.000" overall length nozzle segment-hpt stator material rene
01-439-1684
Turbine Aircraft Gas Turb Nozzle
Used on t700-ge-701cengine.
01-439-2638
Turbine Aircraft Nozzle Assembly
Used on f-16 acft.
01-439-2639
Turbine Aircraft Nozzle Assembly
Used on f-16 acft.
01-439-2641
Turbine Aircraft Nozzle Assembly
Used on f-16 acft.
01-439-2710
Airflow Deflector
Used on f100-pw-229 aircraft gas turbine engine. 3.511" overall length 2.955" overall width used on the combustion chamber; matl spec pwa 1475; 2nd end width 2.020
01-439-4580
Air Transfer Aircraft Gas Scroll
Used on helicopter agusta a109.
01-439-4724
Combustion Chamber Aircraf Liner
01-439-5513
Inlet Guide V Synchronizing Ring
Used on f100-pw-100/200/220 aircraft gas turbine engine. used on the inlet fan module
01-439-6376
Front Aircraft Gas Turbine Frame
Used on acft eng f110-ge-100.
01-439-6377
Turbine Aircraft Nozzle Assembly
Used on acft eng pacer special.
01-439-9183
Turbine Aircraft Gas Turbin Case
Used on ah-64 turbine engine, rotary wing aircraft.
01-439-9448
Aircraft Engine Built-up Unit
Used on cp140/cp140a aurora acft.
01-440-1697
Turbine Blade Aircraft Tu Damper
Used on f100-pw-229 aircraft gas turbine engine. 0.565" overall length t.o. 2j-F100-54, fig 99, ind 21; repl p/n 4074864 once tcto has been accomplished; retaining plate damper is symmetrical in shape
01-440-2599
Compresso Case And Vane Assembly
Used on pacer special.
01-440-4276
Turbine Aircraft Gas Turbin Case
Used on f16 aircraft.
01-440-4297
Aircraft Turbo-prop Engine
01-440-4351
Combustion Aircraft Gas Chamber
01-440-4352
Turbine Engine Afterburner
Used on f110-ge-129 aircraft gas turbine engine. ECPFI120; p/n 9547M23G10 is the same as the 9547M23G07 except the G10 deletes 5 damper ring links
01-440-5597
Compressor Aircraft Gas Tu Rotor
Rotor, compressor, gas turbine engine
01-440-5672
Air Aircraft Gas Turbine En Seal
Used on acft eng f100.
01-440-5673
Seal Aircraft Gas Turbin Support
01-440-5674
Air Aircraft Gas Turbine En Seal
Used on acft eng f100.
01-440-5700
Air Aircraft Gas Turbine En Seal
01-440-5701
Air Aircraft Gas Turbine En Seal
Used on f100-pw-229 acft gas turbine eng. 0.144" overall length original name seal-brush, turbine seal brush; 2250-2650 wires per circumferential inch; dia of seal brush 13.954-13.962; width of bristles 0.070 at overal dia.; seal brush bristles are waxed using spec PWA36702 as reqd
01-440-7223
Augmenter Exhaust Aircraf Nozzle
Used on f110-ge-400(for f14b/d).
01-440-7417
Exhaust Aircraft Gas Turbi Frame
Used on f100-pw-229 aircraft gas turbine engine. 11.156" inside diameter 6.301" overall length 31.120" outside diameter original name case, turbine exhaust, assy assy includes p/n 4077273 case; p/n 4071465 case; p/n 4072398 nut option; p/n xm rivets
01-440-7795
Aircraft Gas Turbine En Diffuser
01-440-8030
Gearbox Turbine Engine Housing
Used on f110-ge-129 aircraft gas turbine engine. 14.845" overall length 8.000" overall width
01-440-8578
Turbine Aircraft Gas Turbin Disk
Used on f100-pw-229 aircraft gas turbine engine.
01-440-8579
Air Aircraft Gas Turbine En Seal
Used on f100-pw-229 aircraft gas turbine engine. brush seal
01-441-0108
Turbine Aircraft Gas Turbin Duct
Used on f100-pw-229 aircraft gas turbine engine. originally submitted as support
01-441-0120
Gearbox Turbine Engine Housing
Used on f110-ge-129 aircraft gas turbine engine. 14.845" overall length 8.000" overall width
01-441-0121
Fan Aircraft Gas Tu Vane Segment
Used on f100-pw-229 aircraft gas turbine engine. 4.196" overall length 2.666" overall width originally submitted vane, turbine stator 7 of these are needed to complete the assembly under p/n 4083403
01-441-1604
Fan Aircraft Gas Tu Vane Segment
Used on f100-pw-229 aircraft gas turbine engine. 4.196" overall length 2.666" overall width originally submitted as vane, turbine stator 1 needed for nozzle assembly p/n 4083403
01-441-3072
Compressor Aircraft Gas Tur Vane
