NSN 9540-01-495-6444
Part Details | STRUCTURAL ANGLE
9540-01-495-6444 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: 1MA100B0310064, 1MA100B03-10064, NAS342182024T8511, NAS342-18-2024T8511, 9540-01-495-6444, 01-495-6444, 9540014956444, 014956444
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 21, 2002 | 01-495-6444 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-495-6444
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1MA100B03-10064 | 76301 | BOEING COMPANY, THEDBA BOEING |
| NAS342-18-2024T8511 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
Technical Data | NSN 9540-01-495-6444
| 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-8511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 1.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
| OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.010 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| SPECIAL FEATURES | END VARIATIONS OBTAINABLE BY SPECIFING CORNER RADII |