NSN 9535-01-532-3832 of Sheet Metal - Parts Details
| Alternative NSN: 9535015323832 |
| 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: 015323832 |
| NCB Code: USA (01) |
| Manufacturers: 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 AMS-T-9046-COMPCP-1-0.032X36X96, AMS-T-9046-COMPCP-1-0 032X36X8, AMS-T-9046 under NSN 9535-01-532-3832 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-532-3832 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 9535-01-532-3832, 9535015323832
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Part No Manufacturer Item Name QTY RFQ AMS-T-9046-COMPCP-1-0.032X36X96 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-T-9046-COMPCP-1-0.032X36X96 Sae International sheet metal Avl RFQ AMS-T-9046-COMPCP-1-0 032X36X8 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-T-9046 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-T-9046 Sae International sheet metal Avl RFQ
Characteristics Data of NSN 9535015323832MRC Criteria Characteristic AARN FABRICATION METHOD ANY ACCEPTABLE ABGL WIDTH 36.000 INCHES NOMINAL ABRY LENGTH 96.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0320 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID CQBC MINIMUM TENSILE STRENGTH 80000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 70000 POUNDS PER SQUARE INCH FEAT SPECIAL FEATURES MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT HEAT HEAT TREATMENT ANNEALED MATL MATERIAL TITANIUM AARN FABRICATION METHOD ANY ACCEPTABLE ABGL WIDTH 36.000 INCHES NOMINAL ABRY LENGTH 96.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0320 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID CQBC MINIMUM TENSILE STRENGTH 80000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 70000 POUNDS PER SQUARE INCH FEAT SPECIAL FEATURES MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT HEAT HEAT TREATMENT ANNEALED MATL MATERIAL TITANIUM
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ANY ACCEPTABLE |
| ABGL | WIDTH | 36.000 INCHES NOMINAL |
| ABRY | LENGTH | 96.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 80000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM |
| AARN | FABRICATION METHOD | ANY ACCEPTABLE |
| ABGL | WIDTH | 36.000 INCHES NOMINAL |
| ABRY | LENGTH | 96.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 80000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM |