AMS-QQ-A-250 4-CD0-0 125X12X48 by Society Of Automotive Engineers Inc with NSN 9535015317078 - Submit a Quote
Part No. : AMS-QQ-A-250 4-CD0-0 125X12X48 | Alternate P/N: AMSQQA2504CD00125X12X48 | Manufacturer : Society Of Automotive Engineers Inc | NSN : 9535-01-531-7078 |
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 4-CD0-0 125X12X48 of NSN 9535015317078 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 4-CD0-0 125X12X48 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 4-CD0-0 125X12X48 society of automotive engineers inc is in stock.
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Characteristics Data of NSN 9535-01-531-7078, 9535015317078MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 12.000 INCHES NOMINAL ABRY LENGTH 48.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.1250 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY III USAGE DESIGN AIRCRAFT FEAT SPECIAL FEATURES MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH HEAT HEAT TREATMENT O-ANNEALED MATT MATERIAL ALUMINUM ALLOY 2024 MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | III USAGE DESIGN | AIRCRAFT |
FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
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