Part No. : AMS-QQ-A-250 5-O-0.032X6X36 | Alternate P/N : AMSQQA2505O0032X6X36 | Manufacturer : Society Of Automotive Engineers Inc |
CAGE Code : 81343 | Item Name : Sheet Metal | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NSN : 9535-01-532-0297 |
You can send a request for quote for p/n AMS-QQ-A-250 5-O-0.032X6X36 to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by Society Of Automotive Engineers Inc (CAGE Code 81343). The description of it is Sheet Metal. The national stock number associated with this part is NSN 9535015320297. This part belongs to FSC Plate Sheet Strip and Foil Nonferrous Base Metal part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with AMS-QQ-A-250 5-O-0.032X6X36 part requirements.
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MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 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 | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 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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