AMS-QQ-A-250 8-CDH34-0 02X12X36 by Society Of Automotive Engineers Inc with NSN 9535015320507 - Submit a Quote
| Part No. : AMS-QQ-A-250 8-CDH34-0 02X12X36 | Alternate P/N: AMSQQA2508CDH34002X12X36 | Manufacturer : Society Of Automotive Engineers Inc | NSN : 9535-01-532-0507 |
| Item Name : Sheet Metal | CAGE Code : 81343 | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
ASAP Aviation Procurement is pleased to announce that part number AMS-QQ-A-250 8-CDH34-0 02X12X36 of NSN 9535015320507 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number AMS-QQ-A-250 8-CDH34-0 02X12X36 is a sheet metal manufactured by society of automotive engineers inc under CAGE Code 81343. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote.In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. AMS-QQ-A-250 8-CDH34-0 02X12X36 society of automotive engineers inc is in stock.
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Characteristics Data of NSN 9535-01-532-0507, 9535015320507MRC Criteria Characteristic MATT Material ALUMINUM ALLOY 5052 HEAT Heat Treatment H-34 STRAIN HARDENED AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL ABGL Width 12.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE, F4F JET AIRCRAFT CQBC Minimum Tensile Strength 34000 POUNDS PER SQUARE INCH MDCL Material Document And Classification QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE ALBY Usage Design AIRCRAFT MRC Decoded Requirement Clear Text Reply FEAT Special Features MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0200 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 5052 |
| HEAT | Heat Treatment | H-34 STRAIN HARDENED |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 34000 POUNDS PER SQUARE INCH |
| MDCL | Material Document And Classification | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |
| ALBY | Usage Design | AIRCRAFT |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0200 INCHES NOMINAL |
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