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National Stock Number:
9540-01-233-0624
Federal Supply Class:
9540
National Item Identification Number:
012330624
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:
| 10133-1201 | 29321 | TRANSTAR METALS CORP | | 1MA100D01-10050 | 76301 | THE BOEING COMPANY | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS10133-1201 | 0U583 | SAE INTERNATIONAL | | AMS10133-1201 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | AND10133-1201 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | AND10133-1201-7075-0 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD |
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Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL | | FIRST TIP RADIUS | 0.063 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | O-ANNEALED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 1.250 INCHES NOMINAL | | OVERALL WIDTH | 1.250 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | O TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.063 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | SPECIFICATION/STANDARD DATA | 76301-1MA100 MANUFACTURERS STANDARD |
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