Item Name | Sheet Metal |
Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
National Item Identification Number (NIIN) | 01-531-7792 (015317792) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-250 5-T3-0.080X12X24 | sae international | sheet metal | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5-CDT3-0 08X12X24 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5 | sae international | sheet metal | RFQ |
AMS-QQ-A-250 5-T3-0.080X12X24 | society of automotive engineers inc | sheet metal | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 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 | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 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 |
Relevant Components for NSN - 9535-01-531-7792, 9535015317792 | ||||
9520-01-538-3805 (9520015383805) | 9530-00-247-5514 (9530002475514) | 9535-01-380-4829 (9535013804829) | 9530-01-496-8011 (9530014968011) | |
9540-01-428-9530 (9540014289530) | 9540-00-403-5155 (9540004035155) | 9515-01-614-8950 (9515016148950) | 9515-01-465-0340 (9515014650340) | |
9520-01-104-1132 (9520011041132) | 9530-00-596-9061 (9530005969061) | 9540-00-595-8549 (9540005958549) | 9530-00-236-0363 (9530002360363) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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