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National Stock Number:
9540-01-363-7422
Federal Supply Class:
9540
National Item Identification Number:
013637422
Description:
ANGLE,STRUCTURAL
Detail:
A STRUCTURAL SHAPE FABRICATED FROM A FERROUS OR NONFERROUS MATERIAL AND RESEMBLING THE LETTER L IN CROSS-SECTIONAL FORM. THE EDGES MAY HAVE A BULB, BE ROUNDED, AND THE INSIDE CORNER MAY HAVE A FILLET.
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Manufacturer Information:
| 10134-1004 | 29321 | TRANSTAR METALS CORP | | 1MA100D06-10027 | 76301 | THE BOEING COMPANY | | AMS 4317 | 0U583 | SAE INTERNATIONAL | | AMS 4317 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-200/15 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10134-1004/QQ-A-200/15 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/15 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP INNER RADIUS | 0.125 INCHES NOMINAL | | FIRST TIP OUTER RADIUS | 0.010 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 0.750 INCHES NOMINAL | | OVERALL WIDTH | 1.000 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | T76511 TEMPER | | SECOND TIP INNER RADIUS | 0.125 INCHES NOMINAL | | SECOND TIP OUTER RADIUS | 0.010 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | | WEIGHT PER UNIT MEASURE | 0.231 POUNDS PER LINEAR FOOT |
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