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National Stock Number:
9540-01-031-0031
Federal Supply Class:
9540
National Item Identification Number:
010310031
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:
| AMS-QQ-A-250/12 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/12 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | BAC1490-2771 | 81205 | THE BOEING COMPANY | | QQ-A-250/12 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.040 INCHES NOMINAL | | FABRICATION METHOD | ROLLED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.060 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | O-ANNEALED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.040 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.060 INCHES NOMINAL | | OVERALL HEIGHT | 0.250 INCHES NOMINAL | | OVERALL WIDTH | 0.550 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | O TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.035 POUNDS PER LINEAR FOOT |
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