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9535-01-532-0309
Metal Sheet
9535015320309 015320309 AMS-QQ-A-250/5 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250/5-CD0-0,1X12X48
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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Related Documents 9535-01-532-0309 5+ Documents (More...)
AMS-QQ-A-250/5 SHEET,METAL 37 EA NS Request Quotation Updated Every Day 9535-01-532-0309 RQST NE Updated
SHEET,METAL 37 EA NS Request Quotation Updated Every Day 9535-01-532-0309 RQST NE Updated AMS-QQ-A
-9535/us 9535-01-532-0309 Metal Sheet 9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250
Metal Sheet 9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250/5- or nonferrous
-250 / AMS-QQ-A -250 /5-T3- AMS-QQ-A -250/5- AMS-QQ-A -250 / - AMS-QQ-A - -250 /5 / AMS-QQ-A - AMS-QQ-A
-T3- AMS-QQ-A-250/5- AMS-QQ-A - -250 /5 / AMS-QQ-A -250 /5-T3 / AMS-QQ-A - AMS-QQ-A -250 / AMS-QQ-A
-9535/us 9535-01-532-0309 Metal Sheet 9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250
9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250 -O-0.100X12X48 AMS-QQ-A-250/5- or
us 9535-01-532-0309 Metal Sheet 9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250/5-CD0
Metal Sheet 9535015320309 015320309 AMS-QQ-A-250/5-O-0.100X12X48 AMS-QQ-A-250/5- -9535/us 9535-
Restrictions 9535-01-532-0309
9535-01-532-0309 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 9535-01-532-0309
- Germany (ZG01)
- Effective Date:
- 1 Jul 2005
- Netherlands (ZN01)
- Effective Date:
- 1 Oct 2015
Approved Sources 9535-01-532-0309
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-250/5
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-250/5-O-0.100X12X48
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-250/5
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/5-O-0.100X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-250/5-CD0-0,1X12X48
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9535-01-532-0309
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Solid
- Cross-Sectional Thickness [ADVM]
- 0.1000 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-250/5 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- 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; Maximum Tensile Strength 32000.0 Pounds Per Square Inch; Maximum Yield Strength 14000.0 Pounds Per Square Inch
- Width [ABGL]
- 12.000 Inches Nominal
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Freight Information 9535-01-532-0309
9535-01-532-0309 has freight characteristics.. 9535-01-532-0309 has a variance between NMFC and UFC when transported by rail and the description should be consulted.