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9535-01-531-7063
Metal Sheet
9535015317063 015317063 AMS-QQ-A-250/4 AMS-QQ-A-250/4-O-0.040X12X48 AMS-QQ-A-250/4-CD0-0,04X12X48
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
January 2023
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Restrictions 9535-01-531-7063
9535-01-531-7063 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 9535-01-531-7063
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
Approved Sources 9535-01-531-7063
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/4
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/4-O-0.040X12X48
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/4
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/4-O-0.040X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/4-CD0-0,04X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-7063
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0400 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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Freight Information 9535-01-531-7063
9535-01-531-7063 has freight characteristics.. 9535-01-531-7063 has a variance between NMFC and UFC when transported by rail and the description should be consulted.