NSN 9535-01-517-7133 of Sheet Metal - Parts Details
| Alternative NSN: 9535015177133 |
| 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: 015177133 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications Promulgat , Society Of Automotive Engineers Inc , Sae International |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers QQ A 250 5, AMS-QQ-A-250 5, AMS QQ A 250 5 under NSN 9535-01-517-7133 of Sheet Metal manufactured by Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-517-7133 is FSC 9535 contains part details of Plate Sheet Strip and Foil Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9535-01-517-7133, 9535015177133
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Part No Manufacturer Item Name QTY RFQ QQ A 250 5 Federal Specifications Promulgat sheet metal Avl RFQ AMS-QQ-A-250 5 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 5 Sae International sheet metal Avl RFQ
Characteristics Data of NSN 9535015177133MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ADVM CROSS-SECTIONAL THICKNESS 0.0630 INCHES NOMINAL AGAV END ITEM IDENTIFICATION TORNADO, MLU, WING, ALENIA AERONAUTICA SPA AGTA BASIC SHAPE STYLE SOLID CQBC MINIMUM TENSILE STRENGTH 61000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 38000 POUNDS PER SQUARE INCH MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5 ZZZT NONDEFINITIVE SPEC/STD DATA T4 TEMPER AARN FABRICATION METHOD ROLLED ADVM CROSS-SECTIONAL THICKNESS 0.0630 INCHES NOMINAL AGAV END ITEM IDENTIFICATION TORNADO, MLU, WING, ALENIA AERONAUTICA SPA AGTA BASIC SHAPE STYLE SOLID CQBC MINIMUM TENSILE STRENGTH 61000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 38000 POUNDS PER SQUARE INCH MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5 ZZZT NONDEFINITIVE SPEC/STD DATA T4 TEMPER
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | TORNADO, MLU, WING, ALENIA AERONAUTICA SPA |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 38000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |
| AARN | FABRICATION METHOD | ROLLED |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | TORNADO, MLU, WING, ALENIA AERONAUTICA SPA |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 38000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |