Part Number
Part Number:
NSN:
NIIN:
Item Name:
CASE , FAN , AIRCRAFT GAS TURBINE EN
Definition:
A CASE THAT IS AN INTEGRAL PART OF AN ENGINE, GAS TURBINE, AIRCRAFT, DESIGNED TO SURROUND AND PROTECT A FAN, AIRCRAFT GAS TURBINE ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 07482 | 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 |
|---|---|---|
| CZBJ | ENGINE SECTION LOCATION | FAN |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4150 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| MATT | MATERIAL | ALUMINUM ALLOY OVERALL |
| FEAT | SPECIAL FEATURES | 2ND STAGE; 1 PIECE EXTRUDED CASE REPLACED P/N 1288M61G01 AND REWORKED TO P/N 9397M40G02 |
| ABMZ | DIAMETER | 95.930 INCHES MINIMUM AND 95.950 INCHES MAXIMUM |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE AND NOZZLE ASSEMBLY,TURBINE,AIRCRAFT |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4, FIG 38, IND 3 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABHP | OVERALL LENGTH | 23.433 INCHES MINIMUM AND 23.453 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |