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9535-01-531-2525
Metal Sheet
9535015312525 015312525 SAE-AMS-QQ-A-250/1 QQ-A-250/1-0-0.063X8X36 AMS-QQ-A-250/1-CD0-0,063X8X36
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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Sheet9535015312525 015312525 SAE-AMS-QQ-A-250/1 AMS-QQ-A-250/1-CD0-0,063X8X36 A ferrous or nonferrous
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Sheet9535015312525 015312525 SAE-AMS-QQ-A-250/1 QQ-A-250/1-0-0.063X8X36 AMS-QQ-A-250/1-CD0-0,063X8X36
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Restrictions 9535-01-531-2525
9535-01-531-2525 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 9535-01-531-2525
- Germany (ZG01)
- Effective Date:
- 1 Jun 2005
Approved Sources 9535-01-531-2525
- Part Number
- Manufacturer
- Status
- SAE-AMS-QQ-A-250/1
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-250/1-0-0.063X8X36
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- QQ-A-250/1-0-0.063X8X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Original Design
- Original Design
- AMS-QQ-A-250/1-CD0-0,063X8X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-2525
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0630 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- End Item Identification [AGAV]
- Fuselage F4f Jet Aircraft
- Material Document And Classification [MDCL]
- Qq-A-250/1 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 1100
- Minimum Yield Strength [CQHQ]
- 3500 Pounds Per Square Inch
- Minimum Tensile Strength [CQBC]
- 11000 Pounds Per Square Inch
- Length [ABRY]
- 36.000 Inches Nominal
- Width [ABGL]
- 8.000 Inches Nominal
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Freight Information 9535-01-531-2525
9535-01-531-2525 has freight characteristics.. 9535-01-531-2525 has a variance between NMFC and UFC when transported by rail and the description should be consulted.