Part Details | STRUCTURAL ANGLE
9540-00-140-2402 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: AND101340701, AND10134-0701, QQA20011, QQ-A-200/11, LS101340701, LS10134-0701, AMS101340701, AMS10134-0701, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-140-2402, 00-140-2402, 9540001402402, 001402402
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | AUG 27, 1971 | 00-140-2402 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-140-2402
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10134-0701 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS10134-0701 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| AMS10134-0701 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-140-2402
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.625 INCHES NOMINAL |
| OVERALL WIDTH | 0.875 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.063 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.110 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |