|
|
|
National Stock Number:
9540-00-140-4977
Federal Supply Class:
9540
National Item Identification Number:
001404977
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 | | AND10133-1602 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | LS10133-1602-5 | 98897 | LOCKHEED MARTIN CORP | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | | FIRST TIP RADIUS | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | OVERALL HEIGHT | 1.750 INCHES NOMINAL | | OVERALL WIDTH | 1.750 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER | | SECOND TIP RADIUS | 0.125 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.520 POUNDS PER LINEAR FOOT |
|