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) | 01-531-7798 (015317798) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-250 5-T3-0.071X12X48 | sae international | sheet metal | RFQ |
AMS QQ A 250 5 T3 0 071X12X48 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5-CDT3-0 071X12X48 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5 | sae international | sheet metal | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 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 | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 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 - 9535-01-531-7798, 9535015317798 | ||||
9510-00-583-5160 (9510005835160) | 9540-01-044-6686 (9540010446686) | 9535-01-387-2251 (9535013872251) | 9540-01-572-7809 (9540015727809) | |
9510-00-045-3343 (9510000453343) | 9515-00-230-6718 (9515002306718) | 9530-00-512-2362 (9530005122362) | 9535-01-524-2390 (9535015242390) | |
9535-01-646-9148 (9535016469148) | 9540-01-231-5077 (9540012315077) | 9505-00-952-7540 (9505009527540) | 9525-00-596-3498 (9525005963498) | |
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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