Mfg Part Number: AMS-QQ-A-250 5-CDT351-1 0X6X24
Alternate P/N: AMSQQA2505CDT35110X6X24
NSN : 9535-01-531-7800
NIIN : 015317800
CAGE Code : 81343
Manufacturer: Society Of Automotive Engineers Inc
Item Name : Plate Metal
Here at Internet For Aviation, we have AMS-QQ-A-250 5-CDT351-1 0X6X24 Plate Metal from Society Of Automotive Engineers Inc, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific AMS-QQ-A-250 5-CDT351-1 0X6X24 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
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 |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 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 |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
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