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 |
---|---|
0R2X7 | HUESTON INDUSTRIES INC |
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 |
---|---|---|
CZEK | AIRCRAFT MISSION DESIGN SERIES | F-15A/B/C/D |
CZDJ | AIRCRAFT LOCATION | DAMPING PAD,STANDOFF |
ABMK | OVERALL WIDTH | 2.690 INCHES MINIMUM AND 2.880 INCHES MAXIMUM |
MATT | MATERIAL | ALUMINUM ALLOY 1100 AND PLASTIC EPOXY |
BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
ABHP | OVERALL LENGTH | 19.250 INCHES MINIMUM AND 19.440 INCHES MAXIMUM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 1100-1 ASSN STD 1ST MATERIAL RESPONSE AND HIMS4020-100 MFR REF 2ND MATERIAL RESPONSE |
ABNM | THICKNESS | 0.115 INCHES MINIMUM AND 0.145 INCHES MAXIMUM |