|
|
National Stock Number: 9540-00-512-6876
Federal Supply Class: 9540
National Item Identification Number: 005126876
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:
10164559 | A486G | NIMIKKEISTOKESKUS NCB FINLAND | 1MA100D05-10008 | 76301 | THE BOEING COMPANY | AND10134-0602 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | QQA200-11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
BASIC SHAPE STYLE | ANGLE | BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.063 INCHES NOMINAL | FIRST TIP RADIUS | 0.063 INCHES NOMINAL | FIRST TIP STYLE | RIGHT QUARTER RADIUS | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | OVERALL HEIGHT | 0.500 INCHES NOMINAL | OVERALL WIDTH | 0.750 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 7075 | NONDEFINITIVE SPEC/STD DATA | T73511 TEMPER | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP RADIUS | 0.063 INCHES NOMINAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.098 POUNDS PER LINEAR FOOT |
|