Part Number
Definition:
(ALL EXCEPT USA) FOR USA INC 61676 CANCELED REPLACED BY CASE(3), GAS TURBINE ENGINE: INC 40956, FIIG A107, APPL KEY D. A CASE DESIGNED TO SURROUND A COMPRESSOR ROTOR, AXIAL, TURBINE ENGINE. EXCLUDESCASE AND VANE ASSEMBLY, AXIAL COMPRESSOR, TURBINE ENGINE.
CAGE Information
Code | Company |
---|---|
99207 | 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 |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 19.924-19.928 IN. LG,13.780-13.800 IN. OD ONE END,17.220-17.240 IN. OD OTHER END |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 19.924-19.928 IN. LG,13.780-13.800 IN. OD ONE END,17.220-17.240 IN. OD OTHER END |
ZZZV | FSC APPLICATION DATA | AIRCRAFT JET ENGINE,T64 |