01-444-7680
Turbine Rotor Aircraft Gas Blade
01-444-7692
Air Aircraft Gas Turbine En Seal
Used on tf-39 aircraft gas turbine engine. 2.370" overall length t.o 2j-TF39-4, fig 62, ind 35; ecp 369; dcn 97-37; honeycombed; replaces p/n 9083M60G06; do not grp per ecp/dcn, whole new configuration; once the old config is repl by the tcto kits with the new p/n, the old config is thrown away; interstage seal; not i&s able
01-444-7693
Turbine Aircraft Gas Turb Nozzle
Used on tf-39 aircraft gas turbine engine. 2.013" overall length t.o. 2j-TF39-4, fig 62 ind 22; boroscope location; repl p/n 9022M16G26; whole new config based on ecp 369, dcn 97-37; new matl
01-444-7699
Turbine Aircraft Gas Turbin Case
Used on acft eng tf39. 46.500" overall length material is inconel 718 with a thermo barrier coating on inner dia. original drawing name case, turbine mid frame. this item is part of the HT90 mod for the TF39 eng
01-444-7700
Turbine Rotor Aircraft Gas Blade
01-444-7701
Turbine Rotor Aircraft Gas Blade
Used on acft eng tf39. 5.388" overall length 1.347" overall width this item is part of the HT90 modfor the TF39 engine, external coating platinum aluminide, original drawing name blade, high pressure turbine rotor stage 2, lead
01-444-7756
Turbine Aircraft Gas Turbi Rotor
01-444-7757
Turbine Aircraft Gas Turbi Shaft
01-444-7758
Turbine Aircraft Gas Turbi Shaft
01-444-8084
Bleed Turbine Engine Valve
Used on guided missile, sidewinder aim-9l.
01-444-8747
Seal Aircraft Gas Turbin Support
Used on tf-39, c-5 acft.
01-444-8896
Gas Turbine Aircraft Engine
Used on falcon 50 aircraft.
01-444-8998
Turbine Aircraft Gas Turb Nozzle
Used on acft eng tf39. 1.873" overall length 3.110" overall width original drawing name, nozzle, high pressure turbine-stage 1 machining HT90-b, this is part of the HT90 mod. for the TF39 engine
01-444-9004
Turbine Aircraft Gas Turb Nozzle
Used on acft eng tf39. 1.873" overall length 3.110" overall width original name on drawing, nozzle, high pressure turbine-stage 1 machining HT90-b, this is part of the HT90 mod for the TF39 engine
01-444-9273
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9275
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9283
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9290
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9294
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9297
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-444-9305
Thermal Aircr Insulation Blanket
Used on acft eng f404. 23.400" overall length
01-444-9307
Thermal Aircr Insulation Blanket
Used on acft eng f404.
01-445-0387
Turbine Aircraft Gas Turbi Frame
Used on tf-39 aircraft gas turbine engine. 13.165" overall length 16.160" outside diameter dcn 97-4, cid 407635; item introduces a new turbine mid frame assembly incorporating a tbc mid frame
01-445-1204
Fan Aircraft Gas Turbine En Vane
Used on t56 acft engine.
01-445-1205
Fan Aircraft Gas Turbine En Vane
Used on t56 acft engine.
01-445-1206
Fan Aircraft Gas Turbine En Vane
Used on t56 acft engine.
01-445-1207
Fan Aircraft Gas Turbine En Vane
Used on t56 acft engine.
01-445-1881
Turbine Aircraft Nozzle Assembly
01-445-1882
Turbine Aircraft Gas Turb Nozzle
01-445-2786
Turbine Aircraft Nozzle Assembly
Used on acft eng f100. 4.615" overall length drawing name vane, turbine stator, 3 stage, assy of, length given is the flow area of the nozzle only
01-445-2787
Turbine Aircraft Nozzle Assembly
Used on acft eng f100. 4.590" overall length drawing name vane, turbine stator, 3 stage, assy of; length is for flow area of nozzle
01-445-2810
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.714-4.738
01-445-2811
Turbine Rotor Aircraft Gas Blade
Used on f100-pw-100 aircraft gas turbine engine. 6.771" overall length t.o. 2j-F100-14, fig 130, ind 9; interim blade replaces p/n 4067004
01-445-2812
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.615-4.639
01-445-3695
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132; flow area 4.639-4.664
01-445-3714
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.639-4.664
01-445-3715
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.615-4.639
01-445-3716
Turbine Aircraft Nozzle Assembly
Used on acft eng f100pw100. 4.689" overall length drawing name vane, turbine stator, 3 stage, assy of; length is flow area of nozzle
01-445-4013
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.664-4.689
01-445-4015
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.590-4.615
01-445-4017
Air Aircraft Gas Turbine En Seal
01-445-4396
Turbine Aircraft Nozzle Assembly
Used on acft engf100pw100. 4.615" overall length drawing name vane, turbine stator, 3 stage, assembly of
01-445-4399
Turbine Aircraft Nozzle Assembly
Used on acft eng f100pw100. 4.664" overall length drawing name vane turbine stator, 3 stage, assy of
01-445-4406
Turbine Aircraft Nozzle Assembly
Used on acft eng f100pw100. 4.639" overall length orignal drawing name vane, turbine stator, 3rd stage assembly of
01-445-5358
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132, flow area 4.714-4.738
01-445-5374
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width t.o. 2j-F100-14, fig 132; flow area 4.689-4.714
01-445-5422
Turbine Aircraft Gas Turbi Rotor
Used on t700 engine.
01-445-5423
Turbine Aircraft Gas Turbi Rotor
Used on t700 engine. matched assy high pressure turbine low stress rotor
01-445-5768
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width original name vane, turbine stator t.o. 2j-F100-14; 4.615-4.639 sq. in area; dcn 97-13 EC96NA072
01-445-5770
Turbine Aircraft Gas Turb Nozzle
Used on f100-pw-100 aircraft gas turbine engine. 2.246" overall length 2.036" overall width original name vane, turbine stator t.o. 2j-F100-14; 4.664-4.689 sq. in. area; dcn 97-13 EC96NA072
