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National Stock Number:
9540-01-369-9117
Federal Supply Class:
9540
National Item Identification Number:
013699117
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:
| 1MA100-10164 | 76301 | THE BOEING COMPANY | | 1MA100D01-10164 | 76301 | THE BOEING COMPANY | | AMS 4476 | 0U583 | SAE INTERNATIONAL | | AMS 4476 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS10133-2401 | 0U583 | SAE INTERNATIONAL | | AMS10133-2401 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10133-2401 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | 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 | O-ANNEALED | | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LENGTH | 10.000 INCHES MINIMUM AND 12.000 INCHES MAXIMUM | | OVERALL HEIGHT | 2.250 INCHES NOMINAL | | OVERALL WIDTH | 2.500 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 ANNEALED CONDITION | | SECOND TIP RADIUS | 0.125 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | UPPER RADIUS |
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