|
|
|
National Stock Number:
9540-00-488-3962
Federal Supply Class:
9540
National Item Identification Number:
004883962
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:
| 1M123 | 76301 | THE BOEING COMPANY | | 2288 0R 6203 | 77783 | ALCOA/REYNOLDS METALS COMPANY | | 78J | 01634 | ALUMINUM CO OF AMERICA | | AMS-QQ-A-200/3 | 0U583 | SAE INTERNATIONAL | | 60-70 | 29321 | TRANSTAR METALS CORP | | 2288 OR 6203 | 77783 | ALCOA/REYNOLDS METALS COMPANY | | T4048 | 03462 | HOWMET CORPORATION | | PA3110 | 06012 | TRANSTAR METALS CORP | | BAC1503-2731 | 81205 | THE BOEING COMPANY | | AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL | | FIRST TIP RADIUS | 0.031 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL | | OVERALL HEIGHT | 1.000 INCHES NOMINAL | | OVERALL WIDTH | 1.000 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 T3511 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.031 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.150 POUNDS PER LINEAR FOOT |
|