|
|
|
National Stock Number: 9540-00-145-5730
Federal Supply Class: 9540
National Item Identification Number: 001455730
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:
| 137073 | 18355 | THE BOEING COMPANY | | 137073 | 88277 | THE BOEING COMPANY | | 8881 | 01634 | ALUMINUM CO OF AMERICA | | AMS-QQA200-3 | 0U583 | SAE INTERNATIONAL | | AMS-QQA200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | QQA200-3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED AND NATURAL AGED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | MATERIAL | ALUMINUM ALLOY | | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER | | OVERALL HEIGHT | 0.500 INCHES NOMINAL | | OVERALL WIDTH | 0.625 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.150 POUNDS PER LINEAR FOOT |
|