Part Number
Part Number:
NSN:
NIIN:
Item Name:
FAIRING , AIRCRAFT
Definition:
A SECONDARY STRUCTURE WHOSE FUNCTION IS TO REDUCE DRAG BY PROVIDING A STREAMLINED SURFACE OR COVERING.
CAGE Information
| Code | Company |
|---|---|
| 80378 | TRIUMPH AEROSTRUCTURES, LLC DBA TRIU |
Federal Supply Class
Title
AIRFRAME STRUCTURAL COMPONENTS
Inclusions:
INCLUDES FLIGHT CONTROL SURFACES; INTERNAL AND EXTERNAL AUXILIARY FUEL TANKS; EXHAUST SYSTEMS; PYLONS, TRIM TABS; AIRCRAFT.
Exclusions:
EXCLUDES FITTED COVERS; HELICOPTER ROTOR BRAKE SYSTEM COMPONENTS; AIRCRAFT LOOSE EQUIPMENT AND ALTERNATE MISSION CONFIGURATION EQUIPMENT STORED ON BOARD THE AIRCRAFT.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| CZEJ | AIRCRAFT STATION NUMBER | X210 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 12.900 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | WEDGE NOZZLE PANEL |
| FEAT | SPECIAL FEATURES | MANUFACTURER SUGGESTED NAME: FLEX SEAL: U/A: GAP SEAL BLADE FAIRING; SMOOTHNESS CRITICAL ITEM; MATL: TI PL; AB-1 COND A; OPPOSITE -014; N/A DAA3640M070; U/O 05001-05002, 05004-05021, 04003 |
| ABMK | OVERALL WIDTH | 10.800 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | PACER SPECIAL |
| ABPX | MATERIAL THICKNESS | 0.250 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-2 |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| MATT | MATERIAL | TITANIUM |