Part Number
Part Number:
NSN:
NIIN:
Item Name:
RIB , STIFFENER , AIRCRAFT
Definition:
A VERTICAL, RELATIVELY SHORT, RIB LOCATED IN A FUSELAGE, NACELLE, POD, AND THE LIKE. IT FOLLOWS THE PERIPHERY AND PROVIDES ADDITIONAL RIGIDITY. IT MAY JOIN VARIOUS COMPONENTS SUCH AS STRINGERS, LONGERONS, AND THE LIKE. IT IS SUPPLEMENTARY TO THE FRAMES AND BLUKHEADS. SEE ALSO RIB (1), AIRFOIL.
CAGE Information
| Code | Company |
|---|---|
| 43999 | BOEING COMPANY THE DBA BOEING DIV DE |
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 14.500 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | RIB, LEADING EDGE |
| FEAT | SPECIAL FEATURES | -013 OPP -014; RIB--QQ-A-250/12 AL BARE SH ALY 7075-0 |
| ABMK | OVERALL WIDTH | 9.750 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| ABPX | MATERIAL THICKNESS | 0.063 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | LEADING EDGE, NO. 1 FLAP |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B1-B ACFT |