Part Details | METAL PLATE
9535-01-495-2549 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: MMS1420CONDT74512.75X48X144, MMS1420CONDT7451-2.75X48X144, MMS1420CONDT7451, 9535-01-495-2549, 01-495-2549, 9535014952549, 014952549
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 11, 2002 | 01-495-2549 | 37013 ( PLATE, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-495-2549
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MMS1420CONDT7451-2.75X48X144 | 76301 | BOEING COMPANY, THEDBA BOEING |
| MMS1420CONDT7451 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9535-01-495-2549
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | S ANY ACCEPTABLE |
| HEAT TREATMENT | T-7451 SOLUTION HEAT TREATED |
| MINIMUM TENSILE STRENGTH | 73000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 63000 POUNDS PER SQUARE INCH |
| LENGTH | 144.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 48.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 2.7500 INCHES NOMINAL |
| NONDEFINITIVE SPEC/STD DATA | 7050 ALLOY AND T7451 CONDITION |
| END ITEM IDENTIFICATION | F/A-18E/F HORNET AIRCRAFT |