Are you searching for parts under NSN 9535-01-531-7796? We encourage you to search through our inventory of over 2 billion new and aftermarket parts applicable within the aerospace industry. Owned and operated by ASAP Semiconductor, ASAP Components stocks key parts of NSN 9535-01-531-7796 such as AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT3-0 05X12X48, AMS-QQ-A-250 5-T3-0.050X12X48, AMS-QQ-A-250-5-T3-0-050X12X48.
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| Item Name | Sheet Metal |
| INC Code | 37015 |
| 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) | 01-531-7796 (015317796) |
| NCB Code | USA (01) |
| Part Number | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | sae international | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-CDT3-0 05X12X48 | society of automotive engineers inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-T3-0.050X12X48 | sae international | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-T3-0-050X12X48 | society of automotive engineers inc | 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 |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 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 | 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 |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 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 - 9535-01-531-7796, 9535015317796 | ||||
| 9515-00-153-3373 (9515001533373) | 9520-01-581-2362 (9520015812362) | 9540-01-597-5789 (9540015975789) | 9515-01-419-7611 (9515014197611) | |
| 9530-00-529-7730 (9530005297730) | 9510-00-505-6438 (9510005056438) | 9535-00-074-2821 (9535000742821) | 9540-01-428-9026 (9540014289026) | |
| 9535-01-531-7128 (9535015317128) | 9535-00-085-4430 (9535000854430) | 9515-00-277-8520 (9515002778520) | 9535-00-249-5793 (9535002495793) | |
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Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |
