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National Stock Number:
9540-00-637-3262
Federal Supply Class:
9540
National Item Identification Number:
006373262
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:
| 1205311 | 18355 | THE BOEING COMPANY | | 1205311 | 88277 | THE BOEING COMPANY | | 2-1316 | 38597 | LOCKHEED MARTIN CORPORATION | | 34571 | 01634 | ALUMINUM CO OF AMERICA | | AMS-QQ-A-200/3 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10134-2005 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.188 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL | | FIRST TIP RADIUS | 0.188 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.188 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 1.250 INCHES NOMINAL | | OVERALL WIDTH | 2.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T4 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.188 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.680 POUNDS PER LINEAR FOOT |
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