NSN 9535-01-531-6276
Part Details | METAL PLATE
9535-01-531-6276 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: AMSQQA2504CDT3510,313X8X36, AMS-QQ-A-250/4-CDT351-0,313X8X36, AMSQQA2504, AMS-QQ-A-250/4, AMSQQA2504T3510.313X8X36, AMS-QQ-A-250/4-T351-0.313X8X36, 9535-01-531-6276, 01-531-6276, 9535015316276, 015316276
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUL 15, 2005 | 01-531-6276 | 37013 ( PLATE, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-531-6276
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AMS-QQ-A-250/4-CDT351-0,313X8X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/4 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/4-T351-0.313X8X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9535-01-531-6276
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 4 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | S ANY ACCEPTABLE |
| HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MINIMUM TENSILE STRENGTH | 64000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| LENGTH | 36.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 8.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 0.3130 INCHES NOMINAL |
| USAGE DESIGN | AIRCRAFT |
| END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |