NSN 9540-00-448-8414
Part Details | STRUCTURAL ANGLE
9540-00-448-8414 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: 253142, MMS158, 1M2633, QQA20011, QQA200-11, AMSQQA20011, AMS-QQA200-11, 604663, 60-4663, 9540-00-448-8414, 00-448-8414, 9540004488414, 004488414
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAY 11, 1970 | 00-448-8414 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-448-8414
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 253142 | 01634 | ALUMINUM CO OF AMERICA |
| MMS158 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 1M2633 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQA200-11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQA200-11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-4663 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-00-448-8414
| 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 | T-73510 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.500 INCHES NOMINAL |
| OVERALL WIDTH | 0.820 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.060 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 135.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.156 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T73510 TEMPER |