Part Number
Part Number:
NSN:
NIIN:
Item Name:
STIFFENER , AIRCRAFT
Definition:
AN ITEM, GENERALLY A STRIP, DESIGNED TO STRENGTHEN AND RESIST LOADS BY ATTACHMENT TO VARIOUS COMPONENTS SUCH AS SKINS, RIBS, PYLONS, AND THE LIKE.
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 |
|---|---|---|
| ABMK | OVERALL WIDTH | 2.240 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | HORIZONTAL STABILIZER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| FEAT | SPECIAL FEATURES | MANUFACTURER SUGGESTED NAME:TEE, RIB; MATL:AL BARE PLATE ALLOY, 7075-T7351; N/A: L2102104; OPPOSITE -005 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEJ | AIRCRAFT STATION NUMBER | STA67.286 |
| ABHP | OVERALL LENGTH | 9.740 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| ABPX | MATERIAL THICKNESS | 1.320 INCHES NOMINAL |