Part Number: AMS-QQ-A-250 5 | Manufacturer: Society Of Automotive Engineers Inc | NSN: 9535-01-532-0310 (9535015320310) | Item Name : sheet metal | CAGE Code: 81343 | FSC: 9535 Plate Sheet Strip and Foil Nonferrous Base Metal | Alternate P/N : AMSQQA2505 |
The AMS-QQ-A-250 5 with NSN 9535015320310 is available in stock! Thanks for your interest in AerospaceSimplified.com. AMS-QQ-A-250 5, Sheet Metal part is manufactured by Society Of Automotive Engineers Inc. Want to request a quote for it? Please fill the form below with contact details, expected delivery date, and quantity.
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MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS; |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS; |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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