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National Stock Number: 9540-01-004-7675
Federal Supply Class: 9540
National Item Identification Number: 010047675
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:
1MA100A03-10114 | 76301 | THE BOEING COMPANY | AMS-QQA200-2 | 0U583 | SAE INTERNATIONAL | AMS-QQA200-2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AND10134-2001 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | QQA200-2 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASIC SHAPE STYLE | ANGLE | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL | FIRST TIP INNER RADIUS | 0.010 INCHES NOMINAL | FIRST TIP OUTER RADIUS | 0.010 INCHES NOMINAL | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED AND STRESS RELIEVED BY STRETCHING | 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 | 1.000 INCHES NOMINAL | OVERALL WIDTH | 2.000 INCHES NOMINAL | MATERIAL | ALUMINUM ALLOY | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | WEIGHT PER UNIT MEASURE | 0.358 POUNDS PER SQUARE FOOT |
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