|
|
|
National Stock Number:
9540-01-468-0130
Federal Supply Class:
9540
National Item Identification Number:
014680130
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-200/15 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/15 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | CVC10001-331CJ | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | QQ-A-200/15 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.320 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP RADIUS | 0.032 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.320 INCHES NOMINAL | | LENGTH | 12.000 INCHES NOMINAL | | OVERALL HEIGHT | 2.000 INCHES NOMINAL | | OVERALL WIDTH | 2.500 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE, UNEQUAL LEGS AND THICKNESSES | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.032 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS |
|