|
|
|
National Stock Number:
9540-00-145-5771
Federal Supply Class:
9540
National Item Identification Number:
001455771
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.
|
Manufacturer Information:
| 2-158 | 38597 | LOCKHEED MARTIN CORPORATION | | 50E3-12 | 80070 | LOCKHEED MARTIN CORPORATION | | 6494 | 01634 | ALUMINUM CO OF AMERICA | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS4154 | 0U583 | SAE INTERNATIONAL | | BAC1503-3471 | 82918 | THE BOEING COMPANY | | E121208 | 0WLU1 | GENERAL DYNAMICS CORP CONVAIR DIV LINDBERGH FIELD FACILITY | | E121208 | 14170 | HUGHES MISSILE SYSTEMS CO SAN DIEGO | | E121208 | 63910 | BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION I | | E121208 | 7B709 | TRACOR FLIGHT SYSTEMS INC SUB OF TRACOR INC | | LS3255 | 98897 | LOCKHEED MARTIN CORP | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.064 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.064 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 1.125 INCHES NOMINAL | | OVERALL WIDTH | 1.750 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 T6 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.220 POUNDS PER LINEAR FOOT |
|