AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| 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 | sae international | sheet metal | RFQ |
| AMS-QQ-A-250 5-CDT3-0 08X12X24 | 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-T3-0.080X12X24 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250 5-T3-0.080X12X24 | sae international | 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 | ||||
| 9540-01-071-0129 (9540010710129) | 9515-01-681-5985 (9515016815985) | 9540-00-526-2604 (9540005262604) | 9530-00-528-8713 (9530005288713) | |
| 9540-01-138-6475 (9540011386475) | 9510-00-952-5947 (9510009525947) | 9530-01-269-2176 (9530012692176) | 9520-00-950-5291 (9520009505291) | |
| 9540-00-060-5492 (9540000605492) | 9510-00-926-4695 (9510009264695) | 9510-00-866-1053 (9510008661053) | 9515-00-079-0992 (9515000790992) | |
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.
Request for Quote