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 |
|---|---|
| 33827 | BAE SYSTEMS INTEGRATED DEFENSE SOLUT |
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 |
|---|---|---|
| SFTT | SURFACE TREATMENT | PRIMER ZINC CHROMATE AND ALUMINUM AND ZINC AND PAINT |
| AARN | FABRICATION METHOD | COMPOSITE AND LAMINATED |
| MATT | MATERIAL | ALUMINUM ALLOY AND GLASS FIBER AND RESIN SYNTHETIC |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | AC-130U |
| ABMK | OVERALL WIDTH | 17.900 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | COVER SUBASSY,FRONT,ALLTV TURRET |
| FEAT | SPECIAL FEATURES | CARBON FIBRE ALSO P/O MATERALS LIST W/ FIBRE GLASS TO FORM COMPOSITE |
| ABHP | OVERALL LENGTH | 26.682 INCHES NOMINAL |