NSN 9540-00-145-5806
Part Details | STRUCTURAL ANGLE
9540-00-145-5806 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: 12422, 1M139, QQA20011, QQ-A-200/11, LS35672, LS3567-2, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-145-5806, 00-145-5806, 9540001455806, 001455806
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-145-5806 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
UPPER RADIUS
SQUARE END
UPPER RADIUS
Cross Reference | NSN 9540-00-145-5806
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 12422 | 01634 | ALUMINUM CO OF AMERICA |
| 1M139 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS3567-2 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-145-5806
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.078 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.350 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER |