|
|
|
National Stock Number:
9540-01-428-9029
Federal Supply Class:
9540
National Item Identification Number:
014289029
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:
| AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | CVC10001-308CA | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.102 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL | | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL | | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | | HEAT TREATMENT | O-ANNEALED | | LEFT SIDE FLANGE THICKNESS | 0.120 INCHES NOMINAL | | LEFT INSIDE ANGLE | 87.0 DEGREES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | OVERALL HEIGHT | 1.180 INCHES NOMINAL | | OVERALL WIDTH | 3.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND 0 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
|