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9535-01-532-0507
Metal Sheet
9535015320507 015320507 AMS-QQ-A-250/8 AMS-QQ-A-250/8-H34-0.020X12X36 AMS-QQ-A-250/8-CDH34-0,02X12X36
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
January 2023
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Restrictions 9535-01-532-0507
9535-01-532-0507 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 9535-01-532-0507
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
Approved Sources 9535-01-532-0507
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/8
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/8-H34-0.020X12X36
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/8-CDH34-0,02X12X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/8-H34-0.020X12X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/8
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-532-0507
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0200 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- Heat Treatment [HEAT]
- H-34 Strain Hardened
- End Item Identification [AGAV]
- Fuselage, F4f Jet Aircraft
- Material Document And Classification [MDCL]
- Qq-A-250/8 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 5052
- Minimum Tensile Strength [CQBC]
- 34000 Pounds Per Square Inch
- Usage Design [ALBY]
- Aircraft
- Length [ABRY]
- 36.000 Inches Nominal
- Special Features [FEAT]
- Maximum Tensile Strength 41000.0 Pounds Per Square Inch
- Width [ABGL]
- 12.000 Inches Nominal
NATO Stock Numbers Related to 9535-01-532-0507
Freight Information 9535-01-532-0507
9535-01-532-0507 has freight characteristics.. 9535-01-532-0507 has a variance between NMFC and UFC when transported by rail and the description should be consulted.