01-447-2508
Compressor Aircraft Gas Tu Rotor
Used on acft eng tf39 2j-tf39-4 f. 49 i. 1. rotor assembly, compressor
01-447-2509
Compressor Aircraft Gas Tu Blade
Used on tf-39 aircraft gas turbine engine. 1.472" overall length original name blade, compressor rotor modified blade has tungsten carbide wear coating on the midspan shrouds
01-447-2512
Compressor Aircraft Gas Tu Rotor
Used on acft eng tf39 2j-tf39-4 f.49 i.1. rotor assembly, compressor
01-447-2801
Airflow Aircraft Gas Turb Baffle
01-447-2846
Turbine Aircraft Gas Turbin Case
Used on acft eng f110ge129. 2.359" overall length cover, cooling air-high pressure turbine nozzle, outer used on the nozzle assembly
01-447-2847
Turbine Aircraft Nozzle Assembly
Used on acft eng f110ge129. 31.500" overall length nozzle assembly, high pressure turbine stator
01-447-2865
Turbine Aircraft Gas Turbin Disk
Used on acft eng f110ge100. 18.995" overall length disk, turbine, turbine engine
01-447-2868
Compressor Aircraft Disk And Hub
Used on f110-ge-129 aircraft gas turbine engine. 6.425" overall length original name spool, compressor rotor t.o 2j-F110-14, fig 67, ind 5; repl p/n 1559M63G02; hpcr stg 1-2 spool oil drain holes are enlarged 1.48 larger than the current elliptical holes to allow better drainage
01-447-3225
Compressor Aircraf Vane Assembly
Used on acft eng f100pw229. stator, compressor exit
01-447-3920
Component Mounting Aircraf Plate
Used on c-17a acft.
01-447-4158
Turbine Aircraft Gas Turbi Shaft
Used on f110-ge-110 aircraft gas turbine engine. original name shaft, turbine, aircraft gas turbine engine t.o. 2j-F110-4, fig 58, ind 38; similar to 1359M21P02 used on the F110-ge-100 but for the F110-ge-110 engine only
01-447-4554
Turbine Aircraft Nozzle Assembly
Used on f414 engine. 47.100" overall length 52.800" overall width
01-447-4809
Turbine Component Aircra Support
Used on c130 hercules aircraft.
01-447-4905
Turbine Aircraft Nozzle Assembly
Used on f100-pw-100/200/220e aircraft gas tubine engine. 2.820" overall length 2.036" overall width original name vane, turbine stator flow area 4.590-4.615 square inch area; t.o. 2j-F100-24, fig 109; replaces p/n 4064943cll, 4082943cll, 4084343cll
01-447-4909
Turbine Aircraft Nozzle Assembly
Used on f100-pw-100/200/220e aircraft gas turbine engine. 2.820" overall length 2.036" overall width original name vane, turbine stator t.o. 2j-F100-24, fig 109; flow area 4.615-4.639 square inch area
01-447-4915
Turbine Aircraft Nozzle Assembly
Used on f100-pw-100/200 aircraft gas turbine engine. 2.820" overall length 2.036" overall width original name vane, turbine stator t.o. 2j-F100-24, fig 109; flow area 4.664-4.689 square inch area
01-447-4917
Turbine Aircraft Nozzle Assembly
Used on f100-pw-100/200 aircraft gas turbine engine. 2.820" overall length 2.036" overall width original name vane turbine stator t.o. 2j-F100-24, fig 109; flow area 4.714-4.738 square inch area
01-447-4918
Turbine Aircraft Nozzle Assembly
Used on f100-pw-100/200 aircraft gas turbine engine. 2.820" overall length 2.036" overall width original name vane, turbine stator t.o. 2j-F100-24, fig 109; flow area 4.689-4.714 square inch area
01-447-5085
Metallic Aircraft Gas Turbi Seal
Used on pacer dawn. 0.040" overall length original name seal, wire
01-447-5097
Turbine Aircraft Gas Turb Nozzle
Used on coast guard hu25c aircraft. 1.300" overall length 0.850" overall width this item has a shape similar to a thimble with twentythree 0.040 inch diameter holes
01-447-6236
Turbine Aircraft Gas Turb Nozzle
Used on f404-ge-400 engine.
01-447-6237
Turbine Aircraft Gas Turb Nozzle
Used on f404-ge-400 engine.
01-447-6248
Turbine Aircraft Gas Turbin Disk
01-447-6533
Fan Aircraft Gas Turbine E Blade
Used on pacer dawn. nha disk p/n 3073436-4/-5; damper coating to be metco 73sf-ns
01-447-6534
Accessory Drive Turbine Gearbox
Used on pacer dawn.
01-447-7235
Heatshield Aircraft Ga Stiffener
Used on acft eng f100.
01-447-7286
Augmenter Exhaust Nozzle Support
Used on acft eng f100.
01-447-7298
Augmenter Exhaust Nozzle Support
Used on acft eng f100.
01-447-7792
Aircraft Gas Hot Section Module
Used on f100-pw-100 aircraft gas turbine engine. used on the lpt turbine; assy consists of p/n 4068948, case; 4076465, casc; 4024675, ball end; 4028005, seal assy; 4067082, bearing option; 4032915, gasket; 4033932, seal ring holder; 4034066, seat; 4034245, support assy; 4034246, support; 4034247, gasket; 4035982, spacer; NAS1398C4A2, rivet; 4048683, plug assy; 4042778, ring assy; 4075518, plate; 4023115, nut option; MS9741-08, bolt; ST2179-02, bolt; MS9226-04, wire; 4053130, bolt; 4001684, ring; 4001687, washer; 4057845, lug; 4057846, bolt; 4006745, gasket; 4006747, insert; 4007021, washer; 4011362, seal ring; 4021784, seat; 4022304, nut; 4022305, washer; 4072216-701, rotor & stator assy
01-447-7793
Compressor Aircraf Vane Assembly
Used on acft eng f100pw100. 4.639" overall length vane-turbine stator, 3 stage, assembly of function
01-447-7801
Turbine Engine Parts Kit
Used on acft eng f110-ge-129. fixture, storage-high presure turbine nozzle assembly kit consist of high pressure turbine nozzle assembly, fixture, high pressure turbine nozzle
01-447-8547
Aircraft Gas Hot Section Module
01-447-8978
Turbine Aircraft Gas Turbi Shaft
Used on f118-ge-100 aircraft gas turbine engine. t.o. 2j-F110-4, fig 58, ind 38; this item is to be used strictly on the F118 engine
01-448-0656
Diffuser Aircraft Gas Turbi Case
Used on f100-pw-229 aircraft gas turbine engine. 13.940" overall length
01-448-0985
Turbine Aircraft Gas Turbin Case
Used on acft eng f100pw100. case assembly of turbine, rear
01-448-1008
Turbine Aircraft Gas Turbin Case
Used on f100-pw-100 aircraft gas turbine engine. 6.784" overall length original name case, turbine rear
01-448-3147
Compressor Aircraft Gas Tu Rotor
Used on f101-ge-102 aircraft gas turbine engine. 28.000" overall length fracture critical item; stgs 1
01-448-3442
Turbine Aircraft Gas Turbi Rotor
Used on acft eng pacer dawn. turbine rotor assembly hpt
01-448-3873
Accessory Drive Turbine Gearbox
Used on pacer dawn. 26.470" overall length gearbox outline, accessory drive height of gearbox is 11.204 max from bottom to center of top mounting holes
01-448-3928
Accessory Drive Turbine Gearbox
Used on pacer dawn. gearbox assembly accessory drive
01-448-4901
Aircraft Gas Hot Section Module
Used on acft eng f100pw229. core engine module
01-448-4903
Fan Aircr Case And Vane Assembly
Used on acft eng f100pw220. inlet case
01-448-4904
Compressor Aircraf Vane Assembly
Used on acft eng f100pw220. 4.590" overall length vane turbine stator, 3 stage, assembly of
01-448-4924
Air Aircraft Gas Turbine En Seal
Used on acft eng f100pw229. 15.073" overall length seal air, turbine, 1 stage
01-448-4926
Air Aircraft Gas Turbine En Seal
Used on acft eng f100pw229. 18.967" overall length ring air sealing, turbine, 2stage, assembly of
01-448-5028
Augmenter Exhaust Aircraf Nozzle
Used on f110-ge-400 for f14b/d.
01-448-5557
Air Aircraft Gas Turbine En Seal
Used on pacer dawn. original name seal assembly, station
01-448-5701
Compressor Aircraft Gas Tur Vane
Used on acft eng f117.
01-448-5704
Compressor Aircraft Gas Tur Vane
Used on acft eng f117.
01-448-5790
Combustion Chamber Aircraft Case
Used on j69-t-25a aircraft gas turbine engine. 7.450" overall length original name shell assembly, complete outer combustor t.o. 2j-J69-44, fig 16; repl p/n 723688-102; contains swirl vane p/n 713163
