Part Number
Definition:
A CYLINDRICAL SHAPED ITEM OR A SEGMENT THEREOF DESIGNED TO DIRECT AIR INTO OR AROUND A CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. THE INTERNAL IAR IS DIVIDED AND DIRECTED TO THE BURNING CHAMBER(S). THE EXTERNAL AIR IS USED FOR COOLING PURPOSES.
CAGE Information
Code | Company |
---|---|
52661 | UNITED TECHNOLOGIES CORPORATION DBA |
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 | T.O. 2J-TF30-24; SUPPORTS THE COMBUSTION CANS,KEEPS THEM IN LINE AND HELPS ALIGN THE DUCT,COMBUSTION CHAMBERTO ATTACH TO THE CANS |
AGAV | END ITEM IDENTIFICATION | ACFT.ENG. TF30 |
ABHP | OVERALL LENGTH | 5.657 INCHES NOMINAL |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMBUSTION CHAMBER |