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 |
|---|---|---|
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| MATT | MATERIAL | PLASTIC ARAMID |
| AGAV | END ITEM IDENTIFICATION | PACER SPECIAL |
| FEAT | SPECIAL FEATURES | HNUCLEAR HARDNESS CRITICAL ITEM & SMOOTHNESS CRITICAL ITEM; CORE MATL: NOMEX HONEYCOMB PER BMS8-124, CL IV, TY V, GR 3, THK TOLERANCE PLUS OR MINUS .006; OPPOSITE -006; DIMENSIONS LISTED ARE STOCK SIZE |
| ABHP | OVERALL LENGTH | 33.000 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-2 |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| ABNM | THICKNESS | 0.500 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | BONDED PART OUTBOARD TRAILING EDGE LOWER PANEL |
| ABMK | OVERALL WIDTH | 13.000 INCHES NOMINAL |