| Alternative NSN: 9535-01-531-7060 |
| Item Name: Sheet Metal |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| NIIN: 015317060 |
| NCB Code: USA (01) |
| Manufacturers: Sae International, Society Of Automotive Engineers Inc |
Browse NSN parts of NSN 9535-01-531-7060 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9535-01-531-7060 like AMS-QQ-A-250 4, AMS-QQ-A-250 4, AMS-QQ-A-250 4-CD0-0 05X12X48, AMS-QQ-A-250 4-O-0.050X12X48, AMS-QQ-A-250 4-O-0.050X12X48 described as Sheet Metal from industry leading manufactures such as Sae International, Society Of Automotive Engineers Inc. We are proud to offer an inventory of over 2 billion ready-to-ship parts, 24/7 availability, and key locations in the U.S./abroad. These attributes allow us to meet all aircraft on ground (AOG) requirements with ease.
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 4 | Sae International | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 4 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 4-CD0-0 05X12X48 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 4-O-0.050X12X48 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 4-O-0.050X12X48 | Sae International | sheet metal | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED" |
| ABGL | WIDTH | 12.000 INCHES NOMINAL" |
| ABRY | LENGTH | 48.000 INCHES NOMINAL" |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT" |
| AGTA | BASIC SHAPE STYLE | SOLID" |
| ALBY | USAGE DESIGN | AIRCRAFT" |
| FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH" |
| HEAT | HEAT TREATMENT | O-ANNEALED" |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4" |
| AARN | FABRICATION METHOD | ROLLED" |
| ABGL | WIDTH | 12.000 INCHES NOMINAL" |
| ABRY | LENGTH | 48.000 INCHES NOMINAL" |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT" |
| AGTA | BASIC SHAPE STYLE | SOLID" |
| ALBY | USAGE DESIGN | AIRCRAFT" |
| FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH" |
| HEAT | HEAT TREATMENT | O-ANNEALED" |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4" |
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9505-00-056-1762 (9505000561762) |
9505-00-056-1763 (9505000561763) |
9505-00-057-2157 (9505000572157) |
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9505-00-057-9449 (9505000579449) |
9505-00-059-6171 (9505000596171) |
9505-00-059-6172 (9505000596172) |
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9505-00-059-6174 (9505000596174) |
9505-00-059-6175 (9505000596175) |
9505-00-059-6176 (9505000596176) |
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9505-00-061-1592 (9505000611592) |
9505-00-061-1593 (9505000611593) |
9505-00-061-1594 (9505000611594) |
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