Item Name | Plate 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) | 01-531-7800 (015317800) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-250 5-T351-1.000X6X24 | sae international | plate metal | RFQ |
AMS-QQ-A-250 5-CDT351-1 0X6X24 | society of automotive engineers inc | plate metal | RFQ |
AMS-QQ-A-250-5-T351-1-000X6X24 | society of automotive engineers inc | plate metal | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | plate metal | RFQ |
AMS-QQ-A-250 5 | sae international | plate metal | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
Relevant Components for NSN - 9535-01-531-7800, 9535015317800 | ||||
9540-01-018-7387 (9540010187387) | 9510-00-583-5174 (9510005835174) | 9520-00-071-4995 (9520000714995) | 9535-00-221-2321 (9535002212321) | |
9510-00-231-2027 (9510002312027) | 9540-01-525-0248 (9540015250248) | 9515-01-562-3748 (9515015623748) | 9540-00-487-5700 (9540004875700) | |
9515-00-206-8808 (9515002068808) | 9515-01-622-2680 (9515016222680) | 9520-00-277-4959 (9520002774959) | 9510-00-256-6279 (9510002566279) | |
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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