AMS-QQ-A-250 5 by Sae International with NSN 9535015317800 - Submit a Quote
| Part No. : AMS-QQ-A-250 5 | Alternate P/N: AMSQQA2505 | Manufacturer : Sae International | NSN : 9535-01-531-7800 |
| Item Name : Plate Metal | CAGE Code : 0U583 | 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 of NSN 9535015317800 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 is a plate metal manufactured by sae international under CAGE Code 0U583. 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 sae international is in stock.
Are you interested in learning more about part number AMS-QQ-A-250 5? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com. And if you are interested in an even faster and more convenient purchasing platform, check out the ASAP Semiconductor App from Google Play or the App Store.
Characteristics Data of NSN 9535-01-531-7800, 9535015317800MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 6.000 INCHES NOMINAL ABRY LENGTH 24.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 1.0000 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY USAGE DESIGN AIRCRAFT CQBC MINIMUM TENSILE STRENGTH 62000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 42000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS HEAT HEAT TREATMENT T-351 SOLUTION HEAT TREATED MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5 AARN FABRICATION METHOD ROLLED ABGL WIDTH 6.000 INCHES NOMINAL ABRY LENGTH 24.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 1.0000 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY USAGE DESIGN AIRCRAFT CQBC MINIMUM TENSILE STRENGTH 62000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 42000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS HEAT HEAT TREATMENT T-351 SOLUTION HEAT TREATED MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 24.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 24.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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