Part Number
Part Number:
NSN:
NIIN:
Item Name:
FRAME , AIRCRAFT
Definition:
A PRINCIPAL TRANSVERSE STRUCTURAL MEMBER OF THE FUSELAGE, HULL, NACELLE, POD, AND THE LIKE. IT FOLLOWS THE PERIPHERY AND PROVIDES SHAPE AND SUPPORT BY ATTACHMENT TO THE LONGITUDINAL MEMBERS OR SKIN.
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | MATL: ST0170LB0027 PLATE, ALLOY 2124-T851; N/A: -001; FINISH: 10AC; DIMENSIONS LISTED ARE STOCK SIZE |
| CZDJ | AIRCRAFT LOCATION | VERTICAL STABILIZER TIP |
| ABMK | OVERALL WIDTH | 8.800 INCHES NOMINAL |
| ABHP | OVERALL LENGTH | 23.500 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| CZEJ | AIRCRAFT STATION NUMBER | STA YUS319.000 |
| MATT | MATERIAL | ALUMINUM ALLOY 2124 |
| ABPX | MATERIAL THICKNESS | 1.920 INCHES NOMINAL |