Part Number
Definition:
A SINGLE STATIONARY ITEM DESIGNED FOR THE PURPOSE OF DIRECTING AIR AT THE PROPER ANGLE AND VELOCITY TO A ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT HAS PROVISIONS FOR ATTACHING TO A CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE AN INNER SUPPORT SHROUD.
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 |
|---|---|---|
| ABMZ | DIAMETER | 17.040 INCHES MINIMUM AND 17.050 INCHES MAXIMUM |
| CZCJ | STAGE NUMBER | 1 |
| ABHP | OVERALL LENGTH | 1.997 INCHES MINIMUM AND 2.023 INCHES MAXIMUM |
| CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| MATT | MATERIAL | STEEL OVERALL |
| ABKW | OVERALL HEIGHT | 2.515 INCHES MINIMUM AND 2.555 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,TURBOJET,MODEL NO. J85-GE-21 |
| FEAT | SPECIAL FEATURES | T.O. 2J-J85-94; TO BE RENAMED NOZZLE ASSY,TURBINE,GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |