NSN 9540-01-475-1087
Part Details | STRUCTURAL ANGLE
9540-01-475-1087 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: CVC10000532CA, CVC10000-532CA, 9540-01-475-1087, 01-475-1087, 9540014751087, 014751087
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAY 23, 2000 | 01-475-1087 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
RIGHT QUARTER RADIUS
Cross Reference | NSN 9540-01-475-1087
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CVC10000-532CA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-475-1087
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430, ALLOY 7075 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 3.000 INCHES NOMINAL |
| OVERALL WIDTH | 3.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.250 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| END ITEM IDENTIFICATION | INTERMEDIATE; AIRCRAFT, B-2 BOMBER (ATB) |