NIIN Output Data
NIIN:
NSN:
Item Name:
RIB , AIRFOIL
Definition:
A PRINCIPAL CHORDWISE RIB THAT GIVES CROSS-SECTIONAL SHAPE, STRENGTH AND RIGIDITY TO A PORTION OF A WING, STABILIZER, AND THE LIKE. SEE ALSO RIB (1), STIFFENER, AIRCRAFT
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 215-70200-301 | 80378 | A | 3 | 2 | 2 | SB |
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 |
|---|---|---|
| ABMK | OVERALL WIDTH | 6.400 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
| BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
| CZDJ | AIRCRAFT LOCATION | INBD LEADING EDGE LANDING FLAP |
| ABHP | OVERALL LENGTH | 8.000 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| FEAT | SPECIAL FEATURES | HEAT TREAT TO COND T42; AGE TO COND T62 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | A-7 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |