Part Details | STRUCTURAL ANGLE
9540-00-146-7249 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: 22381, 1E84, QQA20011, QQA200-11, 7188, AMSQQA20011, AMS-QQA200-11, 9540-00-146-7249, 00-146-7249, 9540001467249, 001467249
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-146-7249 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
UPPER RADIUS
SQUARE END
UPPER RADIUS
Cross Reference | NSN 9540-00-146-7249
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 22381 | 01634 | ALUMINUM CO OF AMERICA |
| 1E84 | 43999 | BOEING COMPANY, THEDBA BOEING |
| QQA200-11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 7188 | 01484 | REYNOLDS METALS CO |
| AMS-QQA200-11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-146-7249
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED AND ARTIFICALLY AGED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.313 INCHES NOMINAL |
| OVERALL WIDTH | 1.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 87.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| FIRST TIP RADIUS | 0.047 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.047 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.430 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |