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Part Number

Part Number:
NSN:
NIIN:
Item Name:
BLADE , COMPRESSOR , AIRCRAFT GAS TU

Definition:

AN ITEM MOUNTED ON A DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE COMPRESSOR SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT.

CAGE Information

Code Company
07482 GENERAL ELECTRIC COMPANY DBA GE DIV

Federal Supply Class

Title

GAS TURBINES AND JET ENGINES, AI

Inclusions:

INCLUDES COMPRESSOR AND TURBINE ROTORS; BLADES; COMBUSTION CHAMBER; ACCESSORY GEAR BOX; AFTERBURNER; EXHAUST CONE; RESERVOIRS, HYDRAULIC; TANK, OIL.

Exclusions:

EXCLUDES OIL, AIR, ANTI-ICING, AND HYDRAULIC REGULATORS, VALVES, AND PUMPS SPECIALLY DESIGNED FOR GAS TURBINES AND JET ENGINES (FSC 2995); CONTROL ASSEMBLIES, PUSH-PULL (FSC 2995); ENGINE MOUNTED CONTROL ASSEMBLIES (FSC 2995); FUEL SYSTEM COMPONENTS (FSC 2915); ENGINE ELECTRICAL SYSTEM COMPONENTS (FSC 2925); ENGINE COOLING SYSTEM COMPONENTS (FSC 2935); ENGINE AIR/OIL CLEANER/FILTER/STRAINERS (FSC 2945).

Characteristics (Decoded)

MRC Requirements Statement Clear Text Reply
ABHP OVERALL LENGTH 1.910 INCHES NOMINAL
CZBJ ENGINE SECTION LOCATION HIGH PRESSURE COMPRESSOR
CZCJ STAGE NUMBER 12
FEAT SPECIAL FEATURES ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
MATT MATERIAL STEEL BLADE
ABMK OVERALL WIDTH 0.989 INCHES NOMINAL
APGF DESIGN TYPE COMPRESSOR
ABKW OVERALL HEIGHT 0.941 INCHES NOMINAL
CRTL CRITICALITY CODE JUSTIFICATION AGAV
AGAV END ITEM IDENTIFICATION ACFT ENG TF39

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