NSN 9540-01-369-8450
Part Details | STRUCTURAL ANGLE
9540-01-369-8450 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: 1MA100D0110323, 1MA100D01-10323, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, 9540-01-369-8450, 01-369-8450, 9540013698450, 013698450
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 07, 1993 | 01-369-8450 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-369-8450
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1MA100D01-10323 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-369-8450
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.400 INCHES NOMINAL |
| OVERALL WIDTH | 2.450 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.060 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.260 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 T0 TEMPER |