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National Stock Number (NSN) Output Data

NSN:
NIIN:
Item Name:
PLATE , STRUCTURAL , AIRCRAFT

Definition:

A FLAT OR PREFORMED ITEM OF METALLIC OR NONMETALLIC MATERIAL. IT MAY VARY IN SHAPE AND ITS SURFACE MAY BE SMOOTH AND/OR SERRATED. ITS THICKNESS IS SMALL IN COMPARISON TO BOTH ITS LENGTH AND WIDTH. IT IS DESIGNED TO BE MOUNTED UPON A SURFACE OR BETWEEN TWO SURFACES. ITS PRIMARY FUNCTION IS TO STRENGTHEN, JOIN, OR SEPARATE AIRCRAFT STRUCTURAL PARTS. EXCLUDES PLATE, MENDING; SHIM; AND SPACER, PLATE.

Reference/Part Number

Part Number CAGE Status RNCC RNVC DAC RNAAC MSDS SADC
4P23206-101A 9U679 A 5 2 E ZZ
4P23206-101A 59213 A 5 2 E ZZ
4P23206-101A 17772 A 5 2 E ZZ
4P23206-101A 29183 A 5 2 E ZZ
4P23206-701A 98897 A 3 2 5 SE
4P23206-101A 8R034 A 5 2 E ZZ
4P23206-101A 51563 A 5 2 E ZZ
4P23206-101A 15992 A 5 2 E ZZ

CAGE Information

Code Company
15992 AEROPARTS MANUFACTURING & REPAIR INC
9U679 CPI AEROSTRUCTURES INC. DBA CPI AERO
59213 AERO COMPONENTS INC
17772 AERO ENGINEERING & MANUFACTURING COM
29183 G. S. E. DYNAMICS INC.
98897 LOCKHEED MARTIN CORPORATION DBA LOCK
8R034 KENT ASSOCIATES INC.
51563 ROHR INC DBA GOODRICH AEROSTRUCTURES

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
ABMK OVERALL WIDTH 27.000 INCHES NOMINAL
ABMK OVERALL WIDTH 27.000 INCHES NOMINAL
MATT MATERIAL ALUMINUM ALLOY
ABHP OVERALL LENGTH 85.000 INCHES NOMINAL
ABPX MATERIAL THICKNESS 0.063 INCHES NOMINAL
AGAV END ITEM IDENTIFICATION ACFT MODEL C5

Similar Parts

4P23206-101A , 4P23206101A , 1560-00-153-9314 , 1560001539314 , 001539314 , 4P23206-101A , 4P23206-101A , 4P23206-101A , 4P23206-101A , 4P23206-701A , 4P23206-101A , 4P23206-101A , 4P23206-101A ,