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9535-01-531-2527
Metal Sheet
9535015312527 015312527 QQ-A-250/11-T6-0.02X12X36 AMS-QQ-A-250/11-CDT6-0,02X12X36
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
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May 2023
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Related Documents 9535-01-531-2527 4+ Documents (More...)
9535-01-531-2527 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-2527
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Metal Sheet 9535015312527 015312527 -T6-0.02X12X36 AMS-QQ-A-250/11-CDT6-0,02X12X36 A ferrous or
nonferrous product with cross-sectional https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-2527
Metal Sheet 9535015312527 015312527 -T6-0.02X12X36 AMS-QQ-A-250/11-CDT6-0,02X12X36 A ferrous or
nonferrous product with cross-sectional https//www.nsnlookup.com /fsg-95/fsc-9535/us 9535-01-531-2527
Metal Sheet 9535015312527 015312527 /fsg-95/fsc-9535/us 9535-01-050-3050 Metal Plate 9535010503050
Restrictions 9535-01-531-2527
9535-01-531-2527 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.
End Users 9535-01-531-2527
- Germany (ZG01)
- Effective Date:
- 1 Jun 2005
Approved Sources 9535-01-531-2527
- Part Number
- Manufacturer
- Status
- QQ-A-250/11-T6-0.02X12X36
- Manufacturer
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- QQ-A-250/11-T6-0.02X12X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Original Design
- Original Design
- AMS-QQ-A-250/11-CDT6-0,02X12X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-2527
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0200 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- End Item Identification [AGAV]
- Fuselage, F4f Jet Aircraft
- Material [MATT]
- Aluminum Alloy, Ams-Q-250/11, Alloy 6061
- Minimum Tensile Strength [CQBC]
- 42000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 35000 Pounds Per Square Inch
- Length [ABRY]
- 36.000 Inches Nominal
- Width [ABGL]
- 12.000 Inches Nominal
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Freight Information 9535-01-531-2527
9535-01-531-2527 has freight characteristics.. 9535-01-531-2527 has a variance between NMFC and UFC when transported by rail and the description should be consulted.