NSN 9540-01-367-1989
Part Details | STRUCTURAL ANGLE
9540-01-367-1989 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: 1MA100D0610275, 1MA100D06-10275, QQA20011, QQ-A-200/11, AMSQQA20015, AMS-QQ-A-200/15, 9540-01-367-1989, 01-367-1989, 9540013671989, 013671989
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | NOV 09, 1992 | 01-367-1989 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-367-1989
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1MA100D06-10275 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/15 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-367-1989
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| OVERALL WIDTH | 2.350 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.070 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.070 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T76511 TEMPER |