Part Number
Definition:
A PREFORMED ITEM OF VARIOUS SHAPES, AND CONTOURS, WHICH MAY HAVE A SANDWICH OR HONEYCOMB CORE BONDED TO A METALLIC OR NONMETALLIC FACING MATERIAL. IT IS USED TO ENCLOSE INTEGRAL PORTIONS OF THE FUSELAGE OR TO FORM PARTITIONS OR SECTIONS WITHIN A WING, EMPENNAGE, FUSELAGE, NACELLE OR CREW COMPARTMENT. IT MAY HAVE MOUNTING PROVISIONS SUCH AS PREDRILLED HOLES TO FACILITATE INSTALLATION, BUT WILL HAVE NO ITEMS ATTACHED TO IT EXCEPT BRACKET (S) OR OTHER SECURING DEVICES TO ACCOMMODATE ITS OWN MOUNTING OR SUPPORT. IT MAY BE MOUNTED BY MEANS OF FASTENERS, BONDING OR WELDING. EXCLUDES PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.
CAGE Information
| Code | Company |
|---|---|
| 81205 | THE BOEING COMPANY 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 | 21.000 INCHES NOMINAL |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| CZDJ | AIRCRAFT LOCATION | ACCESS PANEL-SURGE TANK, BOND PART |
| MATT | MATERIAL | PLASTIC ARAMID |
| FEAT | SPECIAL FEATURES | GNUCLEAR HARDNESS CRITICAL ITEM & SMOOTHNESS CRITICAL ITEM; CORE MATL: NOMEX HONEYCOMB PER BMS8-124 CL IV, TY V, GR 5, THK TOLERANCE PLUS OR MINUS .006; OPPOSITE -002; DIMENSIONS LISTED ARE STOCK SIZE |
| AGAV | END ITEM IDENTIFICATION | PACER SPECIAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-2 |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| ABNM | THICKNESS | 0.500 INCHES NOMINAL |
| ABHP | OVERALL LENGTH | 30.000 INCHES NOMINAL |