NSN 9540-01-116-6768
Part Details | STRUCTURAL ANGLE
9540-01-116-6768 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.
Alternate Parts: ASTM B221, 1MA100B0110267, 1MA100B01-10267, QQA2003, QQ-A-200/3, MS14284E215, AMSQQA2003, AMS-QQ-A-200-3, 608906, 60-8906, 9540-01-116-6768, 01-116-6768, 9540011166768, 011166768
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | AUG 01, 1981 | 01-116-6768 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-116-6768
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1MA100B01-10267 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| MS14284E215 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| AMS-QQ-A-200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-8906 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-116-6768
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.150 INCHES NOMINAL |
| OVERALL WIDTH | 1.810 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.071 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.071 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.250 POUNDS PER LINEAR FOOT |
| SPECIFICATION/STANDARD DATA | 76301-A100 MANUFACTURERS STANDARD |
