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NSN 1560-01-528-1016, 1560015281016
PANEL,STRUCTURAL,AIRCRAFT

Federal Supply Classification
FSC 1560 - Airframe Structural Components
National Item Identification Number
NIIN 015281016
Codification Country
United States
Item Name Code
INC 35987
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Hazardous Material Indicator Code
(P) There is no information in the HMIRS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product.
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DLMS® Summary

National Stock Number 1560-01-528-1016

National Stock Number (NSN) 1560-01-528-1016, or NIIN 015281016, (panel,structural,aircraft) was assigned March 3, 2005 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are no manufacturer part numbers associated to this NSN.

This part number has not been procured by the US Government in over 5 years.

This NSN is somewhat common among different platforms, belonging to 2 different weapons systems.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Jul 12, 2012, this NSN's acquisition method was noted as: Suitable for competitive acquisition for the first time. (Potential sources shall include dealers/distributors.) The Government has unlimited rights to the technical data, and the data package is complete. Valid AMCs: 1 and 2.

This NSN is assigned to Item Name Code (INC) 35987. [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.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no information in the HMIRS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product. NSN 1560015281016 does not contain precious metals.

This NSN is associated to Schedule B 8803909060: other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites). The Schedule B End Use is listed as parts for military-type goods. NAICS classification category 336419: other guided missile and space vehicle parts and auxiliary equipment manufacturing.

This information was last updated on .


Technical Characteristics

III MATERIAL
(MATT) ALUMINUM ALLOY 2024
END ITEM IDENTIFICATION
(AGAV) C-2A AND E-2A
AIRCRAFT LOCATION
(CZDJ) WING CENTER SECTION TRAILING EDGE
AIRCRAFT MISSION DESIGN SERIES
(CZEK) C-2A
OVERALL LENGTH
(ABHP) 46.000 INCHES NOMINAL
OVERALL WIDTH
(ABMK) 6.000 INCHES NOMINAL
PART NAME ASSIGNED BY CONTROLLING AGENCY
(CXCY) INAVY:STRIP
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE
MATERIAL
(MATT) ALUMINUM ALLOY 2024
RELATIONSHIP TO SIMILAR EQUIPMENT
(RTSE) 71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE
SIDE FOR WHICH DESIGNED
(BWJF) BOTH SIDES
SPECIAL FEATURES
(FEAT) SURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409.
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION
(STDC) MIL-STD-130 MIL STD SINGLE TREATMENT RESPONSE
SURFACE TREATMENT
(SFTT) PRIMER EPOXY
THICKNESS
(ABNM) 0.250 INCHES NOMINAL

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