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National Stock Number: 9540-00-238-1553
Federal Supply Class: 9540
National Item Identification Number: 002381553
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:
1325309 | 18355 | THE BOEING COMPANY | 1325309 | 88277 | THE BOEING COMPANY | 15418 | 01634 | ALUMINUM CO OF AMERICA | AMS-QQA200-11 | 0U583 | SAE INTERNATIONAL | 2-1858 | 38597 | LOCKHEED MARTIN CORPORATION | AMS-QQA200-11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | QQA200-11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | BAC1504-5234 | 82918 | THE BOEING COMPANY |
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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 | 0.125 INCHES NOMINAL | FIRST TIP RADIUS | 0.125 INCHES NOMINAL | FIRST TIP STYLE | RIGHT QUARTER RADIUS | HEAT TREATMENT | T-6 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 | 1.250 INCHES NOMINAL | OVERALL WIDTH | 1.375 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 7075 | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER | SECOND TIP DIAMETER | 0.312 INCHES NOMINAL | SECOND TIP RADIUS | 0.125 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP STYLE | UPPER BULBOUS | WEIGHT PER UNIT MEASURE | 0.430 POUNDS PER LINEAR FOOT |
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