NSN 9540-00-146-0726
Part Details | STRUCTURAL ANGLE
9540-00-146-0726 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: 14594, BAC15031061, BAC1503-1061, S122, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 9540-00-146-0726, 00-146-0726, 9540001460726, 001460726
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-146-0726 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-146-0726
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 14594 | 01634 | ALUMINUM CO OF AMERICA |
| BAC1503-1061 | 82918 | BOEING COMPANY, THEDBA BOEING |
| S122 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-146-0726
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.625 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.031 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.120 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |