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9535-01-531-7078

Metal Sheet

9535015317078 015317078 AMS-QQ-A-250/4-O0.125X12X48 AMS-QQ-A-250/4 AMS-QQ-A-250/4-CD0-0,125X12X48

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

9535-01-531-7078 SHEET,METAL 9535015317078 015317078

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 9535-01-531-7078 1/1
NSN 9535-01-531-7078 (Identification) 1/1

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9535-01-531-7078 Related Documents Related Documents 9535-01-531-7078 5+ Documents (More...)

AMS-QQ-A-250/4-O0.125X12X48 AMS-QQ-A-250/4 AMS-QQ-A-250/4-CD0-0,125X12X48 A ferrous or nonferrous product
/fsg-95/fsc-9535/us 9535-01-531-7078 Metal Sheet 9535015317078015317078 AMS-QQ-A-250/4-O0.125X12X48AMS-QQ-A
NumberManufacturerStatusAMS-QQ-A-250/4 0U583 - Sae International (Active) Incomplete Reference RNCC 3 RNVC 1 DAC E AMS-QQ-A-250/4
Updated Every Day /fsg-95/fsc-9535/us 9535-01-115 https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-7078
Metal Sheet 9535015317078 015317078 -O0.125X12X48 AMS-QQ-A-250/4 AMS-QQ-A-250/4-CD0-0,125X12X48
Metal Sheet 9535015317078015317078 AMS-QQ-A-250/4-O0.125X12X48AMS-QQ-A NumberManufacturerStatusAMS-QQ-A
-CDT351-0,25X12X48 https//www.nsnlookup.com / fsg-95/fsc-9535/us 9535 -01-209-4197 Metal AMS-QQ-A-250/4
-250/4-CDT351-0,25X12X48 A ferrous or nonferrous -CDT351-0,25X12X48 AMS-QQ-A -CDT3 -CDT3 AMS-QQ-A-250/4
Metal Sheet 9535015317078 015317078 -O0.125X12X48 AMS-QQ-A-250/4 AMS-QQ-A-250/4-CD0-0,125X12X48
https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-7078 Metal Sheet 9535015317078 015317078
-O0.125X12X48 AMS-QQ-A-250/4 AMS-QQ-A-250/4-CD0-0,125X12X48 A ferrous or nonferrous product with cross-sectional
-9535/us 9535-01-531-7078 Metal Sheet 9535015317078015317078 AMS-QQ-A-250/4-O0.125X12X48AMS-QQ-A NumberManufacturerStatusAMS-QQ-A
https//www.nsnlookup.com https/ A AMS-QQ-A-250/4- /fsc AMS-QQ-A-250/4-O-0.050X6X36 AMS-QQ-A AMS-QQ-A
-O-0.050X6X36 AMS-QQ-A-250/4-CD0-0,05X6X36 A - /fsc AMS-QQ-A-250/4-O-0.050X6X36 AMS-QQ-A-250 /4
- /fsc - /fsc AMS-QQ-A-250/4-O-0.050X6X36 AMS-QQ-A-250 / A - /fsc AMS-QQ-A-250/4-O-0.050X6X36 AMS-QQ-A

9535-01-531-7078 Demil Restrictions 9535-01-531-7078

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

9535-01-531-7078 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.

9535-01-531-7078 End Users End Users 9535-01-531-7078

Germany (ZG01)
Effective Date:
1 Jul 2005

9535-01-531-7078 Manufacturers Approved Sources 9535-01-531-7078

9535-01-531-7078 Technical Data Datasheet 9535-01-531-7078

Characteristic
Specifications
FIIG
A13100
Basic Shape Style [AGTA]
Solid
Cross-Sectional Thickness [ADVM]
0.1250 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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9535-01-531-7078 Freight Data Freight Information 9535-01-531-7078

9535-01-531-7078 has freight characteristics.. 9535-01-531-7078 has a variance between NMFC and UFC when transported by rail and the description should be consulted.