NSN 9535-01-532-0294 of Sheet Metal - Parts Details
| Alternative NSN: 9535015320294 |
| 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: 015320294 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Society Of Automotive Engineers Inc |
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-QQ-A-250 5-O-0.032X12X36, AMS-QQ-A-250 5-CD0-0 032X12X36, AMS-QQ-A-250 5, AMS QQ A 250 5 O 0 032X12X36, AMS QQ A 250 5 under NSN 9535-01-532-0294 of Sheet Metal manufactured by Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-01-532-0294 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 9535-01-532-0294, 9535015320294
-
Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 5-O-0.032X12X36 Sae International sheet metal Avl RFQ AMS-QQ-A-250 5-CD0-0 032X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 5 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 5 O 0 032X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 5 Sae International sheet metal Avl RFQ
Characteristics Data of NSN 9535015320294MRC Criteria Characteristic MDCL Material Document And Classification QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE HEAT Heat Treatment O-ANNEALED AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL ABGL Width 12.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT ALBY Usage Design AIRCRAFT MRC Decoded Requirement Clear Text Reply 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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH MATT Material ALUMINUM ALLOY 2024 AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0320 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| HEAT | Heat Treatment | O-ANNEALED |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ALBY | Usage Design | AIRCRAFT |
| MRC | Decoded Requirement | Clear Text Reply |
| 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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
| MATT | Material | ALUMINUM ALLOY 2024 |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |