NSN 9540-01-118-1568
Part Details | STRUCTURAL ANGLE
9540-01-118-1568 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: AND101351005, AND10135-1005, ASTM B221, 1MA101B0410010, 1MA101B04-10010, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 9540-01-118-1568, 01-118-1568, 9540011181568, 011181568
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | AUG 28, 1981 | 01-118-1568 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-118-1568
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10135-1005 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1MA101B04-10010 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-118-1568
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.117 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | SQUARE END |
| SECOND TIP RADIUS | 0.117 INCHES NOMINAL |
| SECOND TIP DIAMETER | 0.234 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.217 POUNDS PER LINEAR FOOT |
| SPECIFICATION/STANDARD DATA | 76301-1A101 MANUFACTURERS STANDARD |