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NSN 1560-00-073-2769, 1560000732769
COVER,ACCESS,AIRCRAFT

Federal Supply Classification
FSC 1560 - Airframe Structural Components
National Item Identification Number
NIIN 000732769
Codification Country
United States
Item Name Code
INC 51575
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 1560-00-073-2769

National Stock Number (NSN) 1560-00-073-2769, or NIIN 000732769, (cover,access,aircraft) was assigned January 1, 1963 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There is only one manufacturer part number associated with this NSN. None of the associated part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by 2 suppliers. Today, 2 suppliers are listed as Active suppliers for this NSN. Of the active suppliers, there are no suppliers that are deemed design controlled or valid supply parts.

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

This NSN is assigned to Item Name Code (INC) 51575. [AN ACCESS COVER WHICH IS AN INTEGRAL PART OF THE AIRFRAME STRUCTURE OF AN AIRCRAFT. EXCLUDES COVER, ACCESS.]. 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 1560000732769 does not contain precious metals.

This information was last updated on .


Technical Characteristics

DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG LENGTH
(ADPA) 5.365 INCHES MINIMUM AND 5.370 INCHES MAXIMUM
DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH
(ADPB) 0.745 INCHES MINIMUM AND 0.755 INCHES MAXIMUM
DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH
(ADPD) 0.933 INCHES MINIMUM AND 0.943 INCHES MAXIMUM
DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG LENGTH
(ADPC) 0.192 INCHES MINIMUM AND 0.202 INCHES MAXIMUM
END ITEM IDENTIFICATION
(AGAV) F-5 AIRCRAFT
BODY THICKNESS
(ADPR) 0.063 INCHES NOMINAL
CROSS-SECTIONAL SHAPE STYLE
(AAGR) FLAT
FSC APPLICATION DATA
(ZZZV) WING,AIRFRAME
LENGTH
(ABRY) 5.730 INCHES MINIMUM AND 5.750 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) QQ-A-250/5,T3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL
(MATT) ALUMINUM ALLOY 2024
PERIPHERAL SHAPE STYLE
(ABMW) RECTANGLE, TWO HOLES
WIDTH
(ABGL) 2.610 INCHES MINIMUM AND 2.625 INCHES MAXIMUM
SURFACE TREATMENT
(SFTT) ANODIZE

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