NSN - 9535-01-531-7794, 9535015317794 of Sheet Metal
Aviation Axis stocks AMS QQ A 250 5, AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT3-0 08X6X36, AMS-QQ-A-250 5-T3-0.080X6X36 - Sheet Metal made by Sae International, Society Of Automotive Engineers Inc with 9535-01-531-7794. Owned and operated by ASAP Semiconductor, we have access to over 2 billion new and after-market parts applicable within the aerospace and defense industries. All our parts are shipped using our premier shipping and supply chain. We offer short lead-times and some of the fastest shipping times in the industry. We are well-equipped to handle any customer situation - including AOG. Submit an RFQ today and expect a response within 15 minutes or less. ASAP - the evolution of purchasing.
Alternative NSN: 9535-01-531-7794 |
Item Name: Sheet Metal |
Federal Supply Class (FSC): 9535 Plate Sheet Strip And Foil Nonferrous Base Metal |
NIIN: 015317794 |
NCB Code: USA (01) |
Manufacturers: Sae International, Society Of Automotive Engineers Inc |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS QQ A 250 5 | sae international | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-CDT3-0 08X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-T3-0.080X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-T3-0.080X6X36 | sae international | sheet metal | Avl | RFQ |
Technical Characteristics of NSN 9535015317794
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | III 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 |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
Related NSN List for 9535-01-531-7794, 9535015317794
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