ASAP Semiconductor appreciates your request for quotation sent via JetParts360.com for part number AMS-QQ-A-250 5-T3-0.125X6X36 made by Manufacturer Sae International with it's corresponding NSN 9535015317799, CAGE Code 0U583 and FSC 9535 Plate, Sheet, Strip, and Foil; Nonferrous Base Metal. This AMS-QQ-A-250 5-T3-0.125X6X36 part is described as Sheet Metal. You can expect a response from a dedicated customer service expert from ASAP Semiconductor within 15 minutes. Each RFQ is answered in the order it was received. We request you to fill out your contact information, as well as quantity, and any target price along with an expected delivery date for AMS-QQ-A-250 5-T3-0.125X6X36 part. We will strive to provide you with an aggressive price to earn the opportunity for your business.
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9535-01-531-7799, 9535015317799 Characteristics Data
MRC
Criteria
Characteristic
AARN
FABRICATION METHOD
ROLLED
ABGL
WIDTH
6.000 INCHES NOMINAL
ABRY
LENGTH
36.000 INCHES NOMINAL
ADVM
CROSS-SECTIONAL THICKNESS
0.1250 INCHES NOMINAL
AGAV
END ITEM IDENTIFICATION
FUSELAGE F4F JET AIRCRAFT
AGTA
BASIC SHAPE STYLE
SOLID
ALBY
USAGE DESIGN
AIRCRAFT
CQBC
MINIMUM TENSILE STRENGTH
61000 POUNDS PER SQUARE INCH
CQHQ
MINIMUM YIELD STRENGTH
40000 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 SHEET THICKNESS
HEAT
HEAT TREATMENT
T-3 SOLUTION HEAT TREATED
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
0.1250 INCHES NOMINAL
AGAV
END ITEM IDENTIFICATION
FUSELAGE F4F JET AIRCRAFT
AGTA
BASIC SHAPE STYLE
SOLID
ALBY
USAGE DESIGN
AIRCRAFT
CQBC
MINIMUM TENSILE STRENGTH
61000 POUNDS PER SQUARE INCH
CQHQ
MINIMUM YIELD STRENGTH
40000 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 SHEET THICKNESS
HEAT
HEAT TREATMENT
T-3 SOLUTION HEAT TREATED
MATL
MATERIAL
ALUMINUM ALLOY, QQ-A-250/5
NSN Components Related to AMS-QQ-A-250 5-T3-0.125X6X36
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