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) | 01-532-0311 (015320311) |
| NCB Code | USA (01) |
| Manufacturer | Sae International, Society Of Automotive Engineers Inc |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMS-QQ-A-250 5-O-0.125X12X48 | sae international | sheet metal | RFQ |
| AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | RFQ |
| AMS QQ A 250 5 O 0 125X12X48 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250 5 | sae international | sheet metal | RFQ |
| AMS-QQ-A-250-5-CD0-0 125X12X48 | society of automotive engineers inc | 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 | 0.1250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| 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 | O-ANNEALED |
| 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 | 0.1250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| 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 | O-ANNEALED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| Relevant Components for NSN - 9535-01-532-0311, 9535015320311 | ||||
| 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) | |
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