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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 32.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 19.000 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| ABPX | MATERIAL THICKNESS | 0.080 INCHES NOMINAL |
| BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| FEAT | SPECIAL FEATURES | P/O -011 FRAME ASY; U/O ACFT 1 & SUBQ; MATL: AL CLAD SH, ALY 2024-0; HEAT TREAT PER ST0111L0009 TO TEMP T62; FINISH 10AB02 |
| CZDJ | AIRCRAFT LOCATION | LOWER OUTBOARD FUSELAGE |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| CZEJ | AIRCRAFT STATION NUMBER | YF512.000 |