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NIIN Output Data

NIIN:
NSN:
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.

Reference/Part Number

Part Number CAGE Status RNCC RNVC DAC RNAAC MSDS SADC
200540020-1 98748 A 3 2 C ZZ

CAGE Information

Code Company
98748 AIR FORCE UNITED STATES DEPARTMENT O

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
CZDJ AIRCRAFT LOCATION REPAIR-HORIZONTAL STABILIZER TRAILING EDGE
ABNM THICKNESS 1.610 INCHES NOMINAL
CZEK AIRCRAFT MISSION DESIGN SERIES B-1B
ABHP OVERALL LENGTH 17.750 INCHES NOMINAL
MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4 T3 FED SPEC SINGLE MATERIAL RESPONSE
ABMK OVERALL WIDTH 2.300 INCHES NOMINAL
CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY OUTBOARD CLOSEOUT
MATT MATERIAL ALUMINUM ALLOY 2024

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