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National Stock Number:
9540-00-720-1357
Federal Supply Class:
9540
National Item Identification Number:
007201357
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:
| 1159929 | 18355 | THE BOEING COMPANY | | 1159929 | 88277 | THE BOEING COMPANY | | 1223964 | 18355 | THE BOEING COMPANY | | 1223964 | 88277 | THE BOEING COMPANY | | 1249328 | 18355 | THE BOEING COMPANY | | 1249328 | 88277 | THE BOEING COMPANY | | 12746-3 | 27610 | INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP | | 13633 | 01634 | ALUMINUM CO OF AMERICA | | 44569 | 01634 | ALUMINUM CO OF AMERICA | | 60-208 | 29321 | TRANSTAR METALS CORP | | 8006 | 01484 | REYNOLDS METALS CO | | AMS-QQ-A-200/2 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | E122502 | 0WLU1 | GENERAL DYNAMICS CORP CONVAIR DIV LINDBERGH FIELD FACILITY | | E122502 | 14170 | HUGHES MISSILE SYSTEMS CO SAN DIEGO | | E122502 | 63910 | BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION I | | E122502 | 7B709 | TRACOR FLIGHT SYSTEMS INC SUB OF TRACOR INC | | LS3511 | 98897 | LOCKHEED MARTIN CORP | | QQ-A-200/2 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | OVERALL HEIGHT | 2.500 INCHES NOMINAL | | OVERALL WIDTH | 4.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2014 | | NONDEFINITIVE SPEC/STD DATA | 2014 ALLOY AND T4 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.970 POUNDS PER LINEAR FOOT |
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