NSN 9535-01-531-7069
Part Details | METAL SHEET
9535-01-531-7069 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: AMSQQA2504CD00,19X12X48, AMS-QQ-A-250/4-CD0-0,19X12X48, AMSQQA2504, AMS-QQ-A-250/4, AMSQQA2504O0.190X12X48, AMS-QQ-A-250/4-O-0.190X12X48, 9535-01-531-7069, 01-531-7069, 9535015317069, 015317069
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUL 19, 2005 | 01-531-7069 | 37015 ( SHEET, METAL ) |
REFERENCE DRAWINGS & PICTURES
ROUND
Cross Reference | NSN 9535-01-531-7069
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AMS-QQ-A-250/4-CD0-0,19X12X48 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/4 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-250/4-O-0.190X12X48 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9535-01-531-7069
| 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 | O-ANNEALED |
| LENGTH | 48.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | 0 ROUND |
| WIDTH | 12.000 INCHES NOMINAL |
| CROSS-SECTIONAL THICKNESS | 0.1900 INCHES NOMINAL |
| SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
| USAGE DESIGN | AIRCRAFT |
| END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |