|
|
|
National Stock Number:
9540-00-596-5663
Federal Supply Class:
9540
National Item Identification Number:
005965663
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:
| 1329898 | 18355 | THE BOEING COMPANY | | 67580 | 01634 | ALUMINUM CO OF AMERICA | | 9802 | 01634 | ALUMINUM CO OF AMERICA | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | K9802 | 01634 | ALUMINUM CO OF AMERICA | | PA3066 | 06012 | TRANSTAR METALS CORP | | CVC1879 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | S1465089 | 88277 | THE BOEING COMPANY |
|
Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.050 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.050 INCHES NOMINAL | | FIRST TIP RADIUS | 0.025 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.050 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 0.750 INCHES NOMINAL | | OVERALL WIDTH | 0.750 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 T6 TEMPER | | SECOND TIP RADIUS | 0.025 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.090 POUNDS PER LINEAR FOOT |
|
|