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Part Number:
NSN:
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Item Name:
CASE AND VANE ASSEMBLY , COMPRESSO

Definition:

A CASE (3), COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE AND A VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.

CAGE Information

Code Company
58828 CFM INTERNATIONAL INC. DBA CFM THE P

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 HIGH PRESSURE COMPRESSOR
APGF DESIGN TYPE AXIAL COMPRESSOR
AGAV END ITEM IDENTIFICATION F108-GE-100 AIRCRAFT GAS TURBINE ENGINE
FEAT SPECIAL FEATURES ETHE COMPRESSOR REAR STATOR IS A BOLTED QUANDRANT DESIGN CONSISTING OF 4 PINCHLESS CASING QUARTERS, 3 STAGES OF FIXED VANE SEGMENTS AND VANE SHROUDS; ENGINE SERIES 710626 -14 AND 41 APPLY; SB 72-215
RDAL REFERENCE DATA AND LITERATURE T.O. 2J-F108-14, FIG 1, IND 60E
CRTL CRITICALITY CODE JUSTIFICATION FEAT
CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY STATOR ASSEMBLY,COMPRESSOR REAR

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