Part Number
Definition:
A FLEXIBLE COVERING, FABRICATED FROM APPROPRIATE INSULATING MATERIALS, DESIGNED TO REDUCE THERMAL RADIATION IN THE HOT SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT. SEE ALSO SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE.
CAGE Information
Code | Company |
---|---|
03350 | GENERAL ELECTRIC COMPANY DBA GE STRU |
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 |
---|---|---|
FEAT | SPECIAL FEATURES | MATERIAL IS STEEL,CORROSION RESISTING & SHEET FIBER, CERAMIC; LAYER THICKNESS 0.004 IN. |
ABMK | OVERALL WIDTH | 10.260 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 10.880 INCHES NOMINAL |
ABJH | TEMP RATING | 2000.0 DEG FAHRENHEIT |
ABPX | MATERIAL THICKNESS | 1.630 INCHES NOMINAL |