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National Stock Number:
9540-00-148-4308
Federal Supply Class:
9540
National Item Identification Number:
001484308
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:
| 1418821 | 88277 | THE BOEING COMPANY | | 1418821-3600 | 88277 | THE BOEING COMPANY | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS10133-0702 | 0U583 | SAE INTERNATIONAL | | AMS10133-0702 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10133-0702 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL | | FIRST TIP RADIUS | 0.094 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 | 0.094 INCHES NOMINAL | | OVERALL HEIGHT | 0.875 INCHES NOMINAL | | OVERALL WIDTH | 0.875 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.094 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.190 POUNDS PER LINEAR FOOT |
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