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) | 01-531-5843 (015315843) |
| NCB Code | USA (01) |
| Manufacturer | Society Of Automotive Engineers Inc, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMS QQ A 250 4 T3 0 063X6X36 | society of automotive engineers inc | sheet metal | RFQ |
| AMSQQA250 4AT3-0060X0360X0.0630 | society of automotive engineers inc | sheet metal | RFQ |
| AMSQQA250 4AT3 0060X0360X0 0630 | sae international | sheet metal | RFQ |
| AMSQQA250 4A T3 36 0X6 0X0 063 | sae international | sheet metal | RFQ |
| AMS QQ A 250 4 T3 0 063X6X36 | sae international | sheet metal | RFQ |
| AMS-QQ-A-250/4 | society of automotive engineers inc | sheet metal | RFQ |
| AMSQQA250 4A-T3-36.0X6.0X0.063 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250 4-CDT3-0 063X6X36 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250/4 | sae international | sheet metal | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
| Relevant Components for NSN - 9535-01-531-5843, 9535015315843 | ||||
| 9535-00-250-6907 (9535002506907) | 9535-01-681-0031 (9535016810031) | 9535-00-505-6524 (9535005056524) | 9515-00-505-7365 (9515005057365) | |
| 9540-01-009-7327 (9540010097327) | 9535-01-466-7939 (9535014667939) | 9530-00-236-8449 (9530002368449) | 9505-00-186-9174 (9505001869174) | |
| 9540-01-367-4184 (9540013674184) | 9510-00-203-5734 (9510002035734) | 9515-00-153-3380 (9515001533380) | 9540-00-618-4576 (9540006184576) | |
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