Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE

2840-01-105-9540 A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.

Part Alternates: 2840-01-105-9540, 01-105-9540, 2840011059540, 011059540

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 01-105-9540

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Technical Data | NSN 2840-01-105-9540

Characteristic Specifications
ENGINE SECTION LOCATION COMPRESSOR
STAGE NUMBER 7
OVERALL LENGTH 1.562 INCHES MINIMUM AND 1.567 INCHES MAXIMUM
SPECIAL FEATURES ORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ACFT ENG TF 41
MANUFACTURERS CODE 63005
DESIGN CONTROL REFERENCE 6897248

Restrictions/Controls & Freight Information | NSN 2840-01-105-9540

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Category Code Description
No Freight Information