NIIN Output Data
Definition:
A RIGID ITEM DESIGNED TO MAINTAIN A PREDETERMINED SPACE BETWEEN TWO VANE, FAN, AIRCRAFT GAS TURBINE ENGINE IN A VANE ASSEMBLY OR VANE SEGMENT, FAN, AIRCRAFT GAS TURBINE ENGINE. THEY ALSO MAINTAIN THE PROPER ANGLE OF THE VANE FOR PROPER AIR PASSAGE. THEY MAY BE POSITIONED AT THE OUTER OR INNER EDGE OF THE VANE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 6021T38G02 | 99207 | A | 3 | 2 | 2 | SB |
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 3.965 INCHES MINIMUM AND 3.986 INCHES MAXIMUM |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND AGAV |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT ENGINE, TF34-GE-100 |