When you require Plate Metal components such as part number AMS-QQ-A-250 5-T351-0.250X12X48 with the NSN 9535015317803 for your operations, Broadline NSN is your best bet. Whether you are searching for parts from manufacturers like Society Of Automotive Engineers Inc or something else, our team is dedicated to helping you acquire what you need with competitive rates and rapid lead times for your benefit. As such, when you have discovered items of interest, we encourage you to take advantage of our rapid RFQ service by filling out and submitting the form featured throughout our website. On this form, be sure to include relevant details such as your desired part quantity and budget parameters so that our dedicated team members can craft a customized solution that suits your particular operational needs.
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At Broadline NSN, we are dedicated to distributing reliable products such as those with the NSN 9535-01-531-7803 or CAGE code 81343. As an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited parts distributor, you can rely on the caliber of our offerings which feature more than 2 billion new, used, obsolete, and hard-to-find components that are readily available for your purchase at any time. Countless products are subject to rigorous quality control measures to guarantee their fit, form, and function prior to your purchase for your benefit, and all come from leading manufactures like Society Of Automotive Engineers Inc. Those looking for high-quality parts like listings belonging to the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal can count on our team to get them what they need in rapid time. Call or email us with any questions and we will be more than happy to assist you through any stage of the procurement process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7803 Item PartTypeName: PLATE,METAL | 9535 | 015317803 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-T351-0.250X12X48 | 5 | 2 | 3 |
| 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 | 40000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 62000 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 |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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