AMS-QQ-A-250 5-T3-0.040X12X48 by Society Of Automotive Engineers Inc with NSN 9535015317788 - Submit a Quote
| Part No. : AMS-QQ-A-250 5-T3-0.040X12X48 | Alternate P/N: AMSQQA2505T30040X12X48 | Manufacturer : Society Of Automotive Engineers Inc | NSN : 9535-01-531-7788 |
| 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 5-T3-0.040X12X48 of NSN 9535015317788 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 5-T3-0.040X12X48 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 5-T3-0.040X12X48 society of automotive engineers inc is in stock.
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Characteristics Data of NSN 9535-01-531-7788, 9535015317788MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABRY LENGTH 48.000 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT ALBY USAGE DESIGN AIRCRAFT CQHQ MINIMUM YIELD STRENGTH 39000 POUNDS PER SQUARE INCH HEAT HEAT TREATMENT T-3 SOLUTION HEAT TREATED ABGL WIDTH 12.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0400 INCHES NOMINAL AGTA BASIC SHAPE STYLE SOLID CQBC MINIMUM TENSILE STRENGTH 59000 POUNDS PER SQUARE INCH FEAT SPECIAL FEATURES 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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