|
|
|
National Stock Number:
9540-01-367-1989
Federal Supply Class:
9540
National Item Identification Number:
013671989
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:
| 1MA100D06-10275 | 76301 | THE BOEING COMPANY | | AMS-QQ-A-200/15 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/15 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.070 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.070 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 1.250 INCHES NOMINAL | | OVERALL WIDTH | 2.350 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T76511 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
|