|
|
|
National Stock Number: 9540-00-516-6158
Federal Supply Class: 9540
National Item Identification Number: 005166158
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:
| 1249581-2400 | 88277 | THE BOEING COMPANY | | 14044 | 01634 | ALUMINUM CO OF AMERICA | | 24183 | 01634 | ALUMINUM CO OF AMERICA | | 72761 | 03462 | HOWMET CORPORATION | | 60-160 | 29321 | TRANSTAR METALS CORP | | 3887 | 77783 | ALCOA/REYNOLDS METALS COMPANY | | PA60-160 | 06012 | TRANSTAR METALS CORP | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | S1249581 | 18355 | THE BOEING COMPANY | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | S1249581 | 88277 | THE BOEING COMPANY |
|
Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.093 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP RADIUS | 0.093 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.093 INCHES NOMINAL | | LENGTH | 20.000 FEET 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 | | OVERALL HEIGHT | 0.750 INCHES NOMINAL | | OVERALL WIDTH | 1.000 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.093 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.180 POUNDS PER LINEAR FOOT |
|