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9535-01-531-7783
Metal Sheet
9535015317783 015317783 AMS-QQ-A-250/5 AMS-QQ-A-250/5-T3-0.016X12X36 AMS-QQ-A-250/5-CDT3-0,016X12X36
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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AMS-QQ-A-250/5 SHEET,METAL 37 EA NS Request Quotation Updated Every Day 9535-01-531-7783 RQST NE Updated
-250 /5-T3 -250 /5-T3- AMS-QQ-A -250/5- -T3 / AMS-QQ-A 250 / 5 -T3 AMS-QQ-A -250 /5 / Restrictions 9535
Metal Sheet 9535015317783 015317783 AMS-QQ-A-250/5-T3-0.016X12X36 AMS-QQ-A-250/5-CDT3-0,016X12X36
- AMS-QQ-A - -250 /5 / AMS-QQ-A -250/5- AMS-QQ-A - AMS-QQ-A https//www.nsnlookup.com /fsg-95/fsc
Metal Sheet 9535015317783 015317783 AMS-QQ-A-250/5-T3-0.016X12X36 AMS-QQ-A-250/5-CDT3-0,016X12X36 A
ferrous or nonferrous product -CDT3-0,016X12X36 -T3 -0.016X12X36 AMS-QQ-A-250/5 -CDT3-0,016X12X36 https
9535-01-570-8040 Metal Sheet 9535015708040 015708040 -T3 AMS-QQ-A -250 /5 / AMS-QQ-A - 250/ 5- - / AMS-QQ-A
/fsg-95/fsc-9535/us 9535-01-531-7783 Metal Sheet 9535015317783 015317783 AMS-QQ-A-250/5-T3-0.016X12X36
AMS-QQ-A -250/5- /us 250 250 /5 -T3 AMS-QQ-A -250 / - AMS-QQ-A 250/5- AMS-QQ-A - -250 /5 / AMS-QQ-A
-T3 AMS-QQ-A -250 /5 / AMS-QQ-A - 250/ 5- - / AMS-QQ-A - 250/ 5 - - - AMS-QQ-A https -250 -250
Restrictions 9535-01-531-7783
9535-01-531-7783 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 9535-01-531-7783
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
- Netherlands (ZN01)
- Effective Date:
- 1 Oct 2015
Approved Sources 9535-01-531-7783
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/5
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/5-T3-0.016X12X36
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/5-T3-0.016X12X36
- 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-CDT3-0,016X12X36
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-531-7783
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.0160 Inches Nominal
- Fabrication Method [AARN]
- Rolled
- Heat Treatment [HEAT]
- T-3 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]
- 59000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 39000 Pounds Per Square Inch
- Usage Design [ALBY]
- Aircraft
- Length [ABRY]
- 36.000 Inches Nominal
- Special Features [FEAT]
- Thin Layers Approximately Equal Thickness Of Aluminum Alloy 1230 Anodic To Core Are Bonded To Both Surfaces; Nominal Cladding Thickness For Each Layer To Be 5.0 Percent Of Composite Thickness Or 4.0 Percent Of Finished Sheet Thickness
- Width [ABGL]
- 12.000 Inches Nominal
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Freight Information 9535-01-531-7783
9535-01-531-7783 has freight characteristics.. 9535-01-531-7783 has a variance between NMFC and UFC when transported by rail and the description should be consulted.