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9535-01-531-6272

Metal Sheet

9535015316272 015316272 AMS-QQ-A-250/4-T3-0.150X12X48 AMS-QQ-A-250/4-CDT3-0,15X12X48 AMS-QQ-A-250/4

A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Includes corrugated and perforated items. For items 0.005 inch or .125mm thick and less. see FOIL, METAL. For silver items see SILVER SHEET. View more Metal Sheet

9535-01-531-6272 SHEET,METAL 9535015316272 015316272

Managed by United States
NSN Created on 15 Jul 2005
Data Last Changed
May 2023
NATO Update Count
6
NATO Data Quality
AGTA Style A10 for 9535-01-531-6272 1/1
NSN 9535-01-531-6272 (Identification) 1/1

9535-01-531-6272 Stock and Availability Marketplace 9535-01-531-6272

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9535-01-531-6272 Related Documents Related Documents 9535-01-531-6272 5+ Documents (More...)

AMS-QQ-A-250/4-T3-0.150X12X48 AMS-QQ-A-250/4-CDT3-0,15X12X48 AMS-QQ-A-250/4 A ferrous or nonferrous
/fsg-95/fsc-9535/us 9535-01-531-6272 Metal Sheet 9535015316272015316272 AMS-QQ-A-250/4-T3-0.150X12X48AMS-QQ-A
-O-0.063X12X48 AMS-QQ-A /us 9535-01-531-6272 Metal Sheet 9535015316272015316272 -T3-0.150X12X48 AMS-QQ-A
product with AMS-QQ-A-250/4 A /us 9535-01-531 https//www.nsnlookup.com / AMS-QQ-A -250 /4- https AMS-QQ-A
/fsc-9535/us 9535-01-531-7064 Metal Sheet 9535015317064 015317064 AMS-QQ-A-250/4-O-0.063X12X48 AMS-QQ-A
/us 9535-01-531-6272 Metal Sheet 9535015316272 015316272 -T3-0.150X12X48 AMS-QQ-A-250/4-CDT3-0,15X12X48
AMS-QQ-A-250/4-O-0.040X12X36 AMS-QQ-A-250/4-CD0-0,04X12X36 A ferrous or nonferrous product with
AMS-QQ-A-250/4-T351-0.375X6X36 AMS-QQ-A-250/4-CDT351-0,375X6X36 A ferrous or nonferrous product
https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-6272 Metal Sheet 9535015316272 015316272 -T3
-CDT351 https// AMS-QQ-A-250/4-T3-0.100X12X48 AMS-QQ-A AMS-QQ-A A AMS-QQ-A -250 /4- https AMS-QQ-A -
Sheet 9535015316272 015316272 -T3-0.150X12X48 AMS-QQ-A-250 https//www.nsnlookup.com /fsg-95/fsc-9535
/us 9535-01-531-6272 Metal Sheet 9535015316272 015316272 -T3-0.150X12X48 AMS-QQ-A-250/4-CDT3-0,15X12X48
AMS-QQ-A-250/4-T351-0.375X6X36 AMS-QQ-A-250/4-CDT351-0,375X6X36 A ferrous or nonferrous product
-CDT3-0,045X12X48 A ferrous or nonferrous product -CDT3- 0,045X12X48 AMS-QQ-A-250/4-T351-0.313X8X36
Metal Sheet 9535015316272 015316272 9535015316280015316280AMS-QQ-A-250/4-T351-0.375X6X36AMS-QQ-A

9535-01-531-6272 Demil Restrictions 9535-01-531-6272

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

9535-01-531-6272 is a Metal Sheet that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

9535-01-531-6272 End Users End Users 9535-01-531-6272

Germany (ZG01)
Effective Date:
1 Jul 2005

9535-01-531-6272 Manufacturers Approved Sources 9535-01-531-6272

9535-01-531-6272 Technical Data Datasheet 9535-01-531-6272

Characteristic
Specifications
FIIG
A13100
Basic Shape Style [AGTA]
Solid
Cross-Sectional Thickness [ADVM]
0.1500 Inches Nominal
Fabrication Method [AARN]
Rolled
Heat Treatment [HEAT]
T-3 Solution Heat Treated
End Item Identification [AGAV]
Fuselage F4f Jet Aircraft
Material Document And Classification [MDCL]
Qq-A-250/4 Fed Spec 1St Material Response
Material [MATT]
Aluminum Alloy 2024
Minimum Tensile Strength [CQBC]
64000 Pounds Per Square Inch
Minimum Yield Strength [CQHQ]
42000 Pounds Per Square Inch
Usage Design [ALBY]
Aircraft
Length [ABRY]
48.000 Inches Nominal
Width [ABGL]
12.000 Inches Nominal

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9535-01-531-6272 Freight Data Freight Information 9535-01-531-6272

9535-01-531-6272 has freight characteristics.. 9535-01-531-6272 has a variance between NMFC and UFC when transported by rail and the description should be consulted.