NSN 9535-01-531-7800
Part Details | METAL PLATE
9535-01-531-7800 A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Excludes ARMOR PLATE; PLATE, FLOOR, METAL; TERNEPLATE; and TINPLATE. For silver plate items see SILVER SHEET.
Alternate Parts: AMSQQA2505CDT3511,0X6X24, AMS-QQ-A-250/5-CDT351-1,0X6X24, AMSQQA2505, AMS-QQ-A-250/5, AMSQQA2505T3511.000X6X24, AMS-QQ-A-250/5-T351-1.000X6X24, 9535-01-531-7800, 01-531-7800, 9535015317800, 015317800
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUL 21, 2005 | 01-531-7800 | 37013 ( PLATE, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-531-7800
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AMS-QQ-A-250/5-CDT351-1,0X6X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/5 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/5-T351-1.000X6X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9535-01-531-7800
| 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 | T-351 SOLUTION HEAT TREATED |
| MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| LENGTH | 24.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 6.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 1.0000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS |
| USAGE DESIGN | AIRCRAFT |
| END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |