Aircraft Prime Moving; And Components Gas Turbines And Jet Engines FSG 28 — FSC 2840

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NSN

NIIN

Name

Details

2840-01-040-1901

01-040-1901

Compressor Rotor Aircraft Spacer

Used on acft engine tf-33. 2.298" overall length 19.322" outside diameter

2840-01-040-4252

01-040-4252

Diffuser Aircraft Gas Turbi Case

Used on aircraft engine,j85-ge-21a.

2840-01-041-0198

01-041-0198

Turbine Aircraft Gas Turbi Rotor

30 blades equally spaced on outer periphery; tapered od, 7.51 min 7.512 max in. largest od; 10 slots equally spaced on outer periphery; 1.159 min 1.1595 max in. id

2840-01-041-2255

01-041-2255

Air Aircraft Gas Turbine En Seal

Used on f100-pw-100/200 acft engines. ring assembly t.o. 2j-F100-14, fig 130, ind 20

2840-01-041-8616

01-041-8616

Aircraft Gas Tu Turbine Assembly

Used on acrft engine tf39-ge1a.

2840-01-041-8649

01-041-8649

Turbine Rotor Aircraft Gas Blade

Used on aircraft engine,tf39-ge1a.

2840-01-041-9526

01-041-9526

Compressor Aircraft Gas Tu Blade

Used on engine model tf34-ge-100a/f.

2840-01-041-9541

01-041-9541

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9542

01-041-9542

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9543

01-041-9543

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9544

01-041-9544

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9550

01-041-9550

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2. blade, compressor rotor, turbine engine

2840-01-041-9552

01-041-9552

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2. blade, compressor rotor, turbine engine

2840-01-041-9558

01-041-9558

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2. blade, compressor rotor, turbine engine

2840-01-041-9560

01-041-9560

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9561

01-041-9561

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9562

01-041-9562

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9565

01-041-9565

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9566

01-041-9566

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9567

01-041-9567

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9568

01-041-9568

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9569

01-041-9569

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9570

01-041-9570

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9571

01-041-9571

Compressor Aircraft Gas Tu Blade

Used on aircraft engine model tf34-ge-2.

2840-01-041-9572

01-041-9572

Compresso Case And Vane Assembly

Used on aircraft engine model tf34.

2840-01-041-9573

01-041-9573

Turbine Case And Nozzle Assembly

Used on aircraft engine model tf34-ge-2. original name case

2840-01-041-9574

01-041-9574

Turbine Aircraft Gas Turb Nozzle

Used on aircraft engine model tf34-ge-2.

2840-01-042-3090

01-042-3090

Augmentor Component Airc Support

Used on acft engine no. tf-30-p3-9. 0.480" overall length 39.982" outside diameter

2840-01-042-3091

01-042-3091

Augmentor Component Aircra Liner

Used on acft engine no. tf-30. 0.740" overall length

2840-01-042-3948

01-042-3948

Accessory Aircraft Gas T Support

Used on aircraft engine,tf34-ge-100. original name beam, mount used on the ignition exciter

2840-01-042-4034

01-042-4034

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 2.188" overall length original name vane, compressor stator, turbine engine

2840-01-042-4036

01-042-4036

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 2.188" overall length original name vane, compressor stator, turbine engine

2840-01-042-4037

01-042-4037

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.955" overall length original name vane, compressor stator, turbine engine

2840-01-042-4040

01-042-4040

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.955" overall length original name vane, compressor stator, turbine engine

2840-01-042-4041

01-042-4041

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.955" overall length original name vane, compressor stator, turbine engine

2840-01-042-4042

01-042-4042

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.749" overall length original name vane, compressor stator, turbine engine

2840-01-042-4044

01-042-4044

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.749" overall length original name vane, compressor stator, turbine engine

2840-01-042-4045

01-042-4045

Compressor Aircraft Gas Tur Vane

Used on acft engine tf41. 1.749" overall length original name vane, compressor stator, turbine engine

2840-01-042-4048

01-042-4048

Turbine Case And Nozzle Assembly

Used on acft engine tf41. original name case

2840-01-042-6458

01-042-6458

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6459

01-042-6459

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6460

01-042-6460

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6461

01-042-6461

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6462

01-042-6462

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6463

01-042-6463

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6464

01-042-6464

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel, ams 5382, fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia

2840-01-042-6465

01-042-6465

Axial Com Case And Vane Assembly

Used on aircraft engine model t400-cp-401. steel AMS5382 fscm 81343, 2.090 in. min, 2.105 in. max, o/a lg, 10.210 in. o/a dia.

2840-01-042-6466

01-042-6466

Turbine Aircraft Nozzle Assembly

Used on aircraft engine model t400-cp-401.

2840-01-042-6467

01-042-6467

Turbine Aircraft Nozzle Assembly

Used on aircraft engine model t400-cp-401.

2840-01-042-6468

01-042-6468

Turbine Aircraft Nozzle Assembly

Used on aircraft engine model t400-cp-401.

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