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Part Number

Part Number:
NSN:
NIIN:
Item Name:
PANEL , STRUCTURAL , AIRCRAFT

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
BWJF SIDE FOR WHICH DESIGNED LEFT SIDE
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
MDCL MATERIAL DOCUMENT AND CLASSIFICATION 1100-1 ASSN STD 1ST MATERIAL RESPONSE AND HIMS-4020-100 MFR REF 2ND MATERIAL RESPONSE
ABHP OVERALL LENGTH 19.250 INCHES MINIMUM AND 19.440 INCHES MAXIMUM
ABNM THICKNESS 0.115 INCHES MINIMUM AND 0.145 INCHES MAXIMUM

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