Part Number
Definition:
A METALLIC ITEM OF VARIOUS SHAPES DESIGNED TO REDUCE VIBRATION AND TO SECURE A COMPONENT PART OF AN ENGINE, GAS TURBINE, AIRCRAFT TO THE ENGINE CASE OR HOUSING AS MODIFIED. FOR MOUNTING ACCESSORIES TO THE OUTSIDE OF THE ENGINE, SEE PLATE, MOUNTING.
CAGE Information
| Code | Company |
|---|---|
| 33574 | EMPIRE MANUFACTURING CORP. DIV EMPIR |
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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| MATT | MATERIAL | STEEL COMP 410 OVERALL |
| CQFM | HARDNESS RATING | 30.0 ROCKWELL C MINIMUM OVERALL AND 38.0 ROCKWELL C MAXIMUM OVERALL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CZBJ | ENGINE SECTION LOCATION | DIFFUSER |