Mfg Part Number: AMS-QQ-A-250 5 | Alternate P/N: AMSQQA2505 |
NSN : 9535-01-532-0309 | NIIN : 015320309 |
CAGE Code : 0U583 | Manufacturer: Sae International |
Item Name : Sheet Metal | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
We appreciate your interest in our available AMS-QQ-A-250 5 NSN components. We are a leading distributor of NSN parts like 9535-01-532-0309, sourcing from top manufacturers like Sae International. If you would like an immediate quote for comparison on item Sheet Metal part AMS-QQ-A-250 5, please complete the RFQ provided on this page, and an account manager will reach out to you in 15 minutes or less. We aim to formulate our quotes with your unique needs in mind, so we ask you to please complete the RFQ with as much information as you can provide.
A National Stock Number (NSN) is a 13 digit numeric code assigned to items that allows for categorization and tracking through the federal supply system. These numbers are unique to each item and allow for accountability and ease of tracking. Aerospace Domain is a top distributor of NSN parts like AMS-QQ-A-250 5 from trusted manufacturers like Sae International. For this individual part, we have also included its CAGE Code 0U583 and FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal for convenience. Many of our NSN parts are subjected to rigorous quality assurance testing, which is why we stand by the quality of our products. We look forward to helping you acquire your NSN parts. For purchasing on the go, download the ASAP Semiconductor from the Google Play and Apple Store today.
MRC | Criteria | Characteristic |
---|---|---|
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
HEAT | HEAT TREATMENT | O-ANNEALED |
AARN | FABRICATION METHOD | ROLLED |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
ALBY | USAGE DESIGN | AIRCRAFT |
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 SHEET THICKNESS; |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
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