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9535-01-531-7083

Metal Sheet

9535015317083 015317083 AMS-QQ-A-250/4 AMS-QQ-A-250/4-O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48

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

9535-01-531-7083 SHEET,METAL 9535015317083 015317083

Managed by United States
NSN Created on 19 Jul 2005
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
AGTA Style A10 for 9535-01-531-7083 1/1
NSN 9535-01-531-7083 (Identification) 1/1

9535-01-531-7083 Stock and Availability Marketplace 9535-01-531-7083

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9535-01-531-7083 Related Documents Related Documents 9535-01-531-7083 5+ Documents (More...)

AMS-QQ-A-250/4 AMS-QQ-A-250/4-O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48 A ferrous or nonferrous product
-CD0-0,16X12X48 A ferrous -CD0-0,04X12X48 -O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48 9535015317068
Metal Sheet 9535015317083015317083AMS-QQ-A-250 /4-O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48 A
fsc-9535/ us 9535-01-620-6988 Metal Sheet 9535016206988 /us 9535-01 -620-6988 -O -0.160X12X48 AMS-QQ-A-250/4
Metal Sheet 9535015317083 015317083 AMS-QQ-A-250/4-O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48
A ferrous or nonferrous product with -O -0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48 A ferrous -CD0-0,04X12X48
AMS-QQ-A-250/4-O-0.040X12X48 AMS-QQ-A-250/4-CD0-0,04X12X48 A ferrous or nonferrous product with
us 9535-01-620-6988 Metal Sheet 9535016206988 016206988 /us 9535-01 -620-6988 -O -0.160X12X48 AMS-QQ-A-250/4
-CD0-0,1X12X48 A ferrous or nonferrous product with AMS-QQ-A-250/4- https//www.nsnlookup.com /fsg
-CDT3 004081733,AMS 4268 , AMS 4268 - AMS-QQ-A -250 /4 -CDT3 AMS-QQ-A https//www.nsnlookup.com
/fsg-95/fsc-9535/us 9535-01-531-7083 Metal Sheet 9535015317083 015317083 AMS-QQ-A-250/4-O-0.160X12X48
AMS-QQ-A-250/4-CD0-0,16X12X48 A ferrous or nonferrous product with -CD0-0,16X12X48 /us 9535-01 -620-
AMS-QQ-A-250/4-O0.100X12X48 AMS-QQ-A-250/4-CD0-0,1X12X48 A ferrous or nonferrous product with
-O0.100X12X48 https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-7083 Metal Sheet 9535015317083
015317083 AMS-QQ-A-250/4-O-0.160X12X48 AMS-QQ-A-250/4-CD0-0,16X12X48 A ferrous or nonferrous product

9535-01-531-7083 Demil Restrictions 9535-01-531-7083

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

9535-01-531-7083 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.

9535-01-531-7083 End Users End Users 9535-01-531-7083

Germany (ZG01)
Effective Date:
1 Jul 2005

9535-01-531-7083 Manufacturers Approved Sources 9535-01-531-7083

9535-01-531-7083 Technical Data Datasheet 9535-01-531-7083

Characteristic
Specifications
FIIG
A13100
Basic Shape Style [AGTA]
Solid
Cross-Sectional Thickness [ADVM]
0.1600 Inches Nominal
Fabrication Method [AARN]
Rolled
Heat Treatment [HEAT]
O-Annealed
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
Usage Design [ALBY]
Aircraft
Length [ABRY]
48.000 Inches Nominal
Special Features [FEAT]
Maximum Tensile Strength 32000 Pounds Per Square Inch; Maximum Yield Strength 14000 Pounds Per Square Inch
Width [ABGL]
12.000 Inches Nominal

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9535-01-531-7083 Freight Data Freight Information 9535-01-531-7083

9535-01-531-7083 has freight characteristics.. 9535-01-531-7083 has a variance between NMFC and UFC when transported by rail and the description should be consulted.