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9535-01-531-7801
Metal Sheet
9535015317801 015317801 AMS-QQ-A-250/5 AMS-QQ-A-250/5-T4-0.063X12X48 AMS-QQ-A-250/5-CDT4-0,063X12X48
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
May 2023
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SHEET,METAL 37 EA NS Request Quotation Updated Every Day 9535-01-531-7801 RQST NE Updated - AMS-QQ-A
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Restrictions 9535-01-531-7801
9535-01-531-7801 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 9535-01-531-7801
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
- Netherlands (ZN01)
- Effective Date:
- 1 Oct 2015
Approved Sources 9535-01-531-7801
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/5
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/5-T4-0.063X12X48
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/5-T4-0.063X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/5
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/5-CDT4-0,063X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-7801
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0630 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- Heat Treatment [HEAT]
- T-4 Solution Heat Treated
- End Item Identification [AGAV]
- Fuselage F4f Jet Aircraft
- Material Document And Classification [MDCL]
- Qq-A-250/5 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Minimum Tensile Strength [CQBC]
- 61000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 38000 Pounds Per Square Inch
- Usage Design [ALBY]
- Aircraft
- Length [ABRY]
- 48.000 Inches Nominal
- Special Features [FEAT]
- Thin Layers Approximately Equal Thickness, Of Aluminum Alloy 1230 Anodic To The Core Are Bonded To Both Surfaces; Nominal Cladding Thickness For Each Layer To Be 2.5 Percent Of Composite Thickness Or 2.0 Percent Of Finished Sheet Thickness
- Width [ABGL]
- 12.000 Inches Nominal
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Freight Information 9535-01-531-7801
9535-01-531-7801 has freight characteristics.. 9535-01-531-7801 has a variance between NMFC and UFC when transported by rail and the description should be consulted.