|
|
|
National Stock Number:
9535-01-532-0308
Federal Supply Class:
9535
National Item Identification Number:
015320308
Description:
SHEET,METAL
Detail:
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.
|
Manufacturer Information:
| AMS-QQ-A-250/5 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/5 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/5-CD0-0,05X6X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/5-O-0.050X6X36 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/5-O-0.050X6X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
|
Techincal Specification:
| BASIC SHAPE STYLE | SOLID | | CROSS-SECTIONAL THICKNESS | 0.0500 INCHES NOMINAL | | FABRICATION METHOD | ROLLED | | HEAT TREATMENT | O-ANNEALED | | LENGTH | 36.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH | | WIDTH | 6.000 INCHES NOMINAL | | USAGE DESIGN | AIRCRAFT |
|