01-344-5513
Exhaust Aircraft Gas Turbin Duct
01-344-5923
Combustion Aircraft Gas Chamber
Used on t700-ge-700 engine. 6.436" overall length
01-344-6035
Compressor Aircraft Gas Tu Rotor
Used on j-400 engine. rotor, compressor, gas turbine engine
01-344-6049
Engine Modification Kit
Used on f110-ge-400 engine.
01-344-6057
Turbine Aircraft Gas Turbi Rotor
Used on t700-ge-401 engine. dynamic balance rotor assy at 1500 rpm
01-344-7783
Labyrinth Aircraft Gas Seal Ring
Used on engine model j400.
01-344-9149
Compressor Aircraft Gas Tur Vane
Used on acft eng f100.
01-344-9151
Aircraft Gas Turbine Compressor
Used on f100pw0229 aircraft engine. 7th stage
01-344-9154
Compressor Aircraf Vane Assembly
Used on f100pw0229 acft engine. original name compressor, aircraft gas turbine engine t.o. 2j-F100-54, fig 95, ind 110 or fig 96, ind 94
01-344-9155
Aircraft Gas Turbine Compressor
Used on f100pw0229 acft engine. 8th stage
01-344-9156
Turbine Aircraft Nozzle Segment
Used on f108 aircraft engine. 4.000" overall length nozzle segment-lpt stg 1 material RENE77
01-344-9157
Turbine Aircraft Nozzle Segment
Used on f108 aircraft engine. nozzle segment-lpt stg 1 t.o. 2j-F108-4
01-345-1298
Turbine Aircraft Gas Turbin Disk
10.936" overall length disk, gas turbine engine internal involute spline data; no. of teeth 324, pitch 32/64, pressure angle 30 degrees, base circle dia. 8.758 in. min. dia., 10.097 in. max. pitch dia., 10.125 in. basic form dia., 10.162 in. max. dia., 10.183 in. dimensions over two 0.054 dia. pins - 10.048 in. max. external involute spline data, no. of teeth 264 on the basis of 344 pitch 32/64, pressure angle 30 degrees, base circle dia. 9.310 in. min. dia., 10.698 in. min. pitch dia., 1.750 in. basic, form dia. 10.715 in., splines in accordance with ansi B92.1, dimension over two 0.054 in. dia., pins = 10.835 in. max.
01-345-1941
Turbine Aircraft Shroud Segment
Used on seahawk helicopter s70b-2.
01-345-2584
Compressor Aircraft Gas Tu Rotor
Used on AH-64A. rotor, compressor, gas turbine engine
01-345-3061
Gas Turbine Engi Case And Stator
Used on f110-ge-400 engine.
01-345-4480
Gas Turbine Engine Case
Used on aircraft model a-4; a-6.
01-345-4481
Turbine Aircraft Gas Turbin Case
Used on j52 engine. case, gas turbine engine
01-345-4787
Air Aircraft Gas Turbine En Seal
Used on pacer dawn. 0.554" overall length tungsten surface treated
01-345-4788
Air Aircraft Gas Turbine En Seal
Used on pacer dawn. 0.170" overall length titanium surface treated
01-345-4789
Air Aircraft Gas Turbine En Seal
Used on pacer dawn. 7.973" overall length
01-345-4790
Compressor Aircraf Vane Assembly
Used on f100-pw0-229 acft eng/core mod. 2.675" overall length t.o. 2j-F100-54, fig 95, ind 118 or fig 96, ind 104
01-345-4791
Compressor Aircraf Vane Assembly
Used on f100-pw0-229 acft eng core mod. 2.675" overall length original name compressor, aircraft gas turbine engine t.o. 2j-F100-54, fig 95, ind 119 or fig 96, ind 105
01-345-4792
Compressor Aircraf Vane Assembly
Used on f100-pw0-229 acft eng/core mod. 2.675" overall length original name compressor, aircraft gas turbine engine t.o. 2j-F100-54, fig 95, ind 120 or fig 96, ind 106; use only on 4080084-01 thru -04, 4080302-01
01-345-4793
Aircraft Gas Turbine Compressor
Used on f100-pw0-229 acft eng/core mod. 3.227" overall length 7th stage
01-345-4794
Turbine Aircraft Gas Turb Nozzle
Used on pacer special.
01-345-4795
Turbine Aircraft Nozzle Segment
Used on f108 aircraft engine. 8.500" overall length nozzel seg assy-lpt stg 2 material rene 77
01-345-4796
Turbine Aircraft Gas Turbi Shaft
Used on pacer dawn. 11.006" overall length internal spline data: 39 teeth; pressure angle 20 degrees anodize shaft surface treated
01-345-4797
Heat Aircraft Gas Turbine Shield
Used on j400 engine.
01-345-4798
Lubricating Oil Aircraft Ga Tank
Used on j400 engine.
01-345-4819
Compressor Ai Synchronizing Ring
Used on pacer dawn. 5.120" overall length
01-345-4824
Aircraft Gas Hot Section Module
Used on f100-pw-100 acft eng. t.o. 2j-F100-4; provides additional thrust for the engine; this item has critical tolerance features.
01-345-4826
Aircraft Gas Hot Section Module
Used on f100-pw-100/200 aircraft eng. t.o. 2j-F100-4/14; extracts energy from exhaust gases to drive the inlet fan; 3rd
01-345-4838
Augmenter Exhaust Nozzle Support
Used on pacer dawn. 2.816" overall length used on the variable nozzle, actuator strut
01-345-4839
Augmenter Exhaust Nozzle Support
Used on pacer dawn. 2.816" overall length 0.750" overall width goes on the actuator strut; variable nozzle
01-345-6734
Heat Aircraft Gas Turbine Shield
Used on f404 engine.
01-345-8352
Aircraft Turbo-prop Engine
01-346-0610
Compressor Aircraft Gas Tu Rotor
Used on pacer dawn.
01-346-0611
Turbine Aircraft Gas Turb Nozzle
Used on f110 aircraft engine. orig name nozzle, turbine, turbine engine
01-346-0615
Antifriction Bearing Air Housing
Used on t-56 aircraft engine. t.o. 2j-T56-44; hydraulic pump drive; inner rear case assembly
01-346-0657
Metallic Aircraft Gas Turbi Seal
Used on acft eng tf33. 1.530" overall length
01-346-0823
Fan Aircr Case And Vane Assembly
Used on yj400-wr-404 engine. 0.924" overall width case
01-346-0891
Turbo-jet Engine
Used on j400-wr-404 engine,turbojet.
01-346-0928
Heat Aircraft Gas Turbine Shield
Used on j-52 engine.
01-346-1727
Gearbox Turbine Engine Housing
01-346-2765
Augmentor Aircraft Gas Turb Duct
Used on F100PW.
01-346-2766
Exhaust Aircraft Gas Turbin Duct
01-346-2790
Metallic Aircraft Gas Turbi Seal
Used on acft eng t-56.
01-346-4623
Air Aircraft Gas Turbine En Seal
01-346-5352
Turbine Aircraft Gas Turbin Case
Used on yj400-wr-404 engine. case, gas turbine engine
