Part Number
Part Number:
NSN:
NIIN:
Item Name:
FRAME , REAR , AIRCRAFT GAS TURBINE
Definition:
A FRAME USED FOR AND PART OF THE REAR SECTION OF AN AIRCRAFT GAS TURBINE ENGINE. MAY INCLUDE STRUTS.
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 |
|---|---|---|
| AARX | INSIDE DIAMETER | 15.495 INCHES MINIMUM AND 15.535 INCHES MAXIMUM |
| ABKV | OUTSIDE DIAMETER | 16.995 INCHES MINIMUM AND 17.005 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | MAINFRAME COMPRESSOR SECTION |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,TURBINE |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-J85-54, FIG 13, IND 1 |
| AGAV | END ITEM IDENTIFICATION | ACFT.ENG. J85 |
| ABHP | OVERALL LENGTH | 4.517 INCHES MINIMUM AND 4.531 INCHES MAXIMUM |
| CZLB | NUMBER OF VARIABLE GUIDE VANES | 6 |
| MATT | MATERIAL | NICKEL ALLOY |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV AND AARX AND CZLB |