1560-01-592-9362 STIFFENER,AIRCRAFT 1560-01-593-1735 FUSELAGE

National Stock Number:
1560-01-592-9405

Federal Supply Class:
1560

National Item Identification Number:
015929405

Description:
WEB,STRUCTURAL COMPONENT,AIRCRAF

Detail:
AN ITEM DESIGNED AS A PRINCIPAL MEMBER OF VARIOUS PRIMARY STRUCTURES WITHIN AN AIRCRAFT. IT PROVIDES STRENGTH, RIGIDITY AND THE LIKE WHILE MAINTAINING THE PROPER DIMENSIONAL DISTANCES AS REQUIRED. IT MAY INCLUDE HOLES FOR MOUNTING AND/OR JOINING TO OTHER ITEMS TO FORM AN ASSEMBLY.


Manufacturer Information:
L3223760-02800518C. F. ROARK WELDING & ENGINEERING COMPANY, INCORPORATED
L3223760-02806DM5INFINITY FABRICATION, INC.
L3223760-0280BT76PRO-FAB, LLC
L3223760-0280C7H8D-J ENGINEERING INC
L3223760-0280P657CAMNETICS MANUFACTURING CORPORATION
L3223760-02814248HARLOW AEROSTRUCTURES, LLC
L3223760-0281P642VOLUMATIC INC
L3223760-0281QJK4FMW, INC.
L3223760-02829183G. S. E. DYNAMICS, INC.
L3223760-02829957NORDAM GROUP LLC, THE
L3223760-0282V045MALONES CNC MACHINING INC
L3223760-02838281STARPLEX SCIENTIFIC
L3223760-0283L665C. E. MACHINE CO., INC.
L3223760-02843999THE BOEING COMPANY
L3223760-02859213AERO COMPONENTS, LLC
L3223760-0286AUZ3NORTHROP GRUMMAN TECHNICAL SERVICES, INC.


Techincal Specification:
AIRCRAFT LOCATIONUNDERWING FAIRING
AIRCRAFT MISSION DESIGN SERIESB-1B
CRITICALITY CODE JUSTIFICATIONFEAT
OVERALL LENGTH10.700 INCHES NOMINAL
OVERALL WIDTH4.300 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5 FED STD SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS0.050 INCHES NOMINAL
MATERIALALUMINUM ALLOY 2024
PART NAME ASSIGNED BY CONTROLLING AGENCYWEB
SPECIAL FEATURESHARDNESS CRITICAL ITEM;OPPOOSITE -027


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