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) | 01-531-7788 (015317788) |
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 040X12X48 | sae international | sheet metal | RFQ |
AMS-QQ-A-250 5-CDT3-0 04X12X48 | 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-T3-0.040X12X48 | 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 | 0.0400 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 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 | 0.0400 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 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 - 9535-01-531-7788, 9535015317788 | ||||
9510-00-224-1673 (9510002241673) | 9505-00-541-9654 (9505005419654) | 9540-01-353-5127 (9540013535127) | 9515-66-151-1706 (9515661511706) | |
9515-00-153-3357 (9515001533357) | 9535-01-012-2441 (9535010122441) | 9520-01-694-5689 (9520016945689) | 9510-01-484-4625 (9510014844625) | |
9530-00-993-4137 (9530009934137) | 9515-00-153-3227 (9515001533227) | 9515-01-555-3938 (9515015553938) | 9530-00-060-5594 (9530000605594) | |
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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