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9535-01-531-6282
Metal Plate
9535015316282 015316282 AMS-QQ-A-250/4 AMS-QQ-A-250/4-T351-0.625X8X36 AMS-QQ-A-250/4-CDT351-0,625X8X36
A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Excludes ARMOR PLATE; PLATE, FLOOR, METAL; TERNEPLATE; and TINPLATE. For silver plate items see SILVER SHEET. View more Metal Plate
January 2023
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Restrictions 9535-01-531-6282
9535-01-531-6282 is a Metal Plate 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 9535-01-531-6282
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
Approved Sources 9535-01-531-6282
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/4
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/4-T351-0.625X8X36
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/4-T351-0.625X8X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/4
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/4-CDT351-0,625X8X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-6282
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.6250 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- Heat Treatment [HEAT]
- T-351 Solution Heat Treated
- 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
- Minimum Tensile Strength [CQBC]
- 63000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 42000 Pounds Per Square Inch
- Usage Design [ALBY]
- Aircraft
- Length [ABRY]
- 36.000 Inches Nominal
- Width [ABGL]
- 8.000 Inches Nominal
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Freight Information 9535-01-531-6282
9535-01-531-6282 has freight characteristics.. 9535-01-531-6282 has a variance between NMFC and UFC when transported by rail and the description should be consulted.