Part Details | METAL PLATE
9535-01-471-4470 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: AMS 4050 0.625 48X144, 9535-01-471-4470, 01-471-4470, 9535014714470, 014714470
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 03, 2000 | 01-471-4470 | 37013 ( PLATE, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-471-4470
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AMS 4050 0.625 48X144 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9535-01-471-4470
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | ANY ACCEPTABLE |
| HEAT TREATMENT | T-7451 SOLUTION HEAT TREATED |
| MINIMUM TENSILE STRENGTH | 74000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 64000 POUNDS PER SQUARE INCH |
| LENGTH | 144.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 48.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 0.6250 INCHES NOMINAL |
| SPECIAL FEATURES | WS IS AIRCRAFT,B-2 BOMDER (ATB); PLATE IS SOLUTION HEAT TREATED, STRESS RELIEVED AND OVERAGED; PLATE IS 0.625" THICK |
| SPECIFICATION/STANDARD DATA | 81343-MS 4050F PROFESSIONAL/INDUSTRIAL ASSOCIATION SPECIFICATION |