NSN 9535-01-532-0308
Part Details | METAL SHEET
9535-01-532-0308 A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Includes corrugated and perforated items. For items 0.005 inch or .125mm thick and less. see FOIL, METAL. For silver items see SILVER SHEET.
Alternate Parts: AMSQQA2505CD00,05X6X36, AMS-QQ-A-250/5-CD0-0,05X6X36, AMSQQA2505, AMS-QQ-A-250/5, AMSQQA2505O0.050X6X36, AMS-QQ-A-250/5-O-0.050X6X36, 9535-01-532-0308, 01-532-0308, 9535015320308, 015320308
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUL 26, 2005 | 01-532-0308 | 37015 ( SHEET, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-532-0308
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AMS-QQ-A-250/5-CD0-0,05X6X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/5 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/5-O-0.050X6X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9535-01-532-0308
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 5 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | S ANY ACCEPTABLE |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 36.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 6.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL |
| 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 |
| USAGE DESIGN | AIRCRAFT |
| END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |