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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
76823 NORTHROP GRUMMAN SYSTEMS CORPORATION

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
ABHP OVERALL LENGTH 48.000 INCHES NOMINAL
CZEK AIRCRAFT MISSION DESIGN SERIES T-38
MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATT MATERIAL ALUMINUM ALLOY 7075
ABNM THICKNESS 0.025 INCHES NOMINAL
ABMK OVERALL WIDTH 24.000 INCHES NOMINAL

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