| 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) | 01-532-0309 (015320309) |
| NCB Code | USA (01) |
| Manufacturer | Sae International, Society Of Automotive Engineers Inc |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | sae international | sheet metal | 0u583 | RFQ |
| AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
| AMS-QQ-A-250 5-CD0-0 1X12X48 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
| AMS-QQ-A-250 5-O-0.100X12X48 | sae international | sheet metal | 0u583 | RFQ |
| AMS-QQ-A-250 5-O-0.100X12X48 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.1000 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 | 0.1000 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 |
| Components Related to NSN - 9535-01-532-0309, 9535015320309 | ||||
| 9540-00-043-3497 (9540000433497) | 9530-00-554-4860 (9530005544860) | 9510-00-261-5746 (9510002615746) | 9540-01-353-4621 (9540013534621) | |
| 9535-00-963-5124 (9535009635124) | 9540-01-437-8540 (9540014378540) | 9510-00-982-9526 (9510009829526) | 9510-00-288-6214 (9510002886214) | |
| 9535-00-086-9884 (9535000869884) | 9510-00-950-0970 (9510009500970) | 9535-01-558-5717 (9535015585717) | 9515-01-465-0276 (9515014650276) | |
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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