 | 9540-00-197-9856 | ANGLE,STRUCTURAL | 01/01/1963 |
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 | 9540-00-197-9856 | ANGLE,STRUCTURAL | | 0 |
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 | ASTM-B-221 | ALUMINUM |  GALI CORPORATION | 2 | | QQ-A-200/8 | EXTRUSION | GALI CORPORATION | 9 | | AMS-QQ-A-200/8 | MATERIAL | GALI CORPORATION | 28 | | QQ-A200/8 | ANGLE | GALI CORPORATION | 521 | | ASTM-B221 | ANGLE | GALI CORPORATION | 151 | | AMS-QQ-A-200/8 | DIA | TIGER ENTERPRISES & TRADING, INC | 0 |
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 | AMS-QQ-A-200/8 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 | | AND10133-3003 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | 99237 | | ASTM B221 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | 81346 | | QQ-A-200/8 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERV | 81348 | | AMS-QQ-A-200/8 | SAE INTERNATIONAL | 0U583 | | SAE-AMS-QQ-A-200/8 | SAE INTERNATIONAL | 0U583 |
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 | FABRICATION METHOD | EXTRUDED | | LENGTH | 20.000 FEET MINIMUM AND 30.000 FEET MAXIMUM | | LEFT SIDE FLANGE THICKNESS | 0.312 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | | BASE FLANGE THICKNESS | 0.312 INCHES NOMINAL | | FIRST TIP RADIUS | 0.312 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
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