|
|
|
National Stock Number:
9540-01-175-7694
Federal Supply Class:
9540
National Item Identification Number:
011757694
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:
| 10134-1003-7075TO | 29321 | TRANSTAR METALS CORP | | 1MA100D01-10260 | 76301 | THE BOEING COMPANY | | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | | AMS10134-1003 | 0U583 | SAE INTERNATIONAL | | AMS10134-1003 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10134-1003/QQ-A-200/11-0 | 14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | AND10134-1003 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | COLD FINISH | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | O-ANNEALED | | LEFT INSIDE ANGLE | 98.40 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/11 ASSN STD SINGLE MATERIAL RESPONSE | | OVERALL WIDTH | 1.375 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 7075 | | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION | | OVERALL HEIGHT | 1.250 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.130 POUNDS PER LINEAR FOOT |
|