NSN 9540-01-435-5250
Part Details | STRUCTURAL ANGLE
9540-01-435-5250 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: CVC100011019GAX144, CVC10001-1019GAX144, MILT81556, MIL-T-81556, CVC100011019GA, CVC10001-1019GA, 9540-01-435-5250, 01-435-5250, 9540014355250, 014355250
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | AUG 27, 1996 | 01-435-5250 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-435-5250
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CVC10001-1019GAX144 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| MIL-T-81556 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| CVC10001-1019GA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-435-5250
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | ANNEALED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| OVERALL WIDTH | 2.100 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.450 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.380 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.500 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 105.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| FIRST TIP INNER RADIUS | 0.062 INCHES NOMINAL |
| FIRST TIP OUTER RADIUS | 0.062 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |