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Part Number:
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Item Name:
CASE , FAN , AIRCRAFT GAS TURBINE EN

Definition:

A CASE THAT IS AN INTEGRAL PART OF AN ENGINE, GAS TURBINE, AIRCRAFT, DESIGNED TO SURROUND AND PROTECT A FAN, AIRCRAFT GAS TURBINE ENGINE.

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
CZBJ ENGINE SECTION LOCATION FAN
APGF DESIGN TYPE AXIAL COMPRESSOR
MDCL MATERIAL DOCUMENT AND CLASSIFICATION AMS4150 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
MATT MATERIAL ALUMINUM ALLOY OVERALL
FEAT SPECIAL FEATURES 2ND STAGE; 1 PIECE EXTRUDED CASE REPLACED P/N 1288M61G01 AND REWORKED TO P/N 9397M40G02
ABMZ DIAMETER 95.930 INCHES MINIMUM AND 95.950 INCHES MAXIMUM
CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY ORIGINAL NAME CASE AND NOZZLE ASSEMBLY,TURBINE,AIRCRAFT
RDAL REFERENCE DATA AND LITERATURE T.O. 2J-TF39-4, FIG 38, IND 3
CRTL CRITICALITY CODE JUSTIFICATION AGAV
ABHP OVERALL LENGTH 23.433 INCHES MINIMUM AND 23.453 INCHES MAXIMUM
AGAV END ITEM IDENTIFICATION ACFT ENG TF39

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9397M40G01 , 9397M40G01 , 2840-01-167-2923 , 2840011672923 , 011672923