Part Number
Definition:
A RIGID ITEM DESIGNED TO MAINTAIN A PREDETERMINED SPACE BETWEEN TWO VANE, FAN, AIRCRAFT GAS TURBINE ENGINE IN A VANE ASSEMBLY OR VANE SEGMENT, FAN, AIRCRAFT GAS TURBINE ENGINE. THEY ALSO MAINTAIN THE PROPER ANGLE OF THE VANE FOR PROPER AIR PASSAGE. THEY MAY BE POSITIONED AT THE OUTER OR INNER EDGE OF THE VANE.
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 |
---|---|---|
MATT | MATERIAL | ALUMINUM ALLOY |
MATT | MATERIAL | ALUMINUM ALLOY |
FEAT | SPECIAL FEATURES | 0.880 IN. H; 4.207 IN. W |
ABHP | OVERALL LENGTH | 3.986 INCHES NOMINAL |