NSN 9540-01-239-6532
Part Details | STRUCTURAL CHANNEL
9540-01-239-6532 A structural shape fabricated from a ferrous or nonferrous material and has a flange extending usually at right angles in the same direction from each edge of a web and/or resembling the letter U in cross-sectional form.
Alternate Parts: 332D18024, 332D1802-4, 9540-01-239-6532, 01-239-6532, 9540012396532, 012396532
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 13, 2006 | 01-239-6532 | 37019 ( CHANNEL, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
CHANNEL
Cross Reference | NSN 9540-01-239-6532
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 332D1802-4 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-01-239-6532
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 5.600 FEET NOMINAL |
| BASIC SHAPE STYLE | CHANNEL |
| OVERALL WIDTH | 0.766 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES MINIMUM AND 0.073 INCHES MAXIMUM |
| RIGHT SIDE FLANGE THICKNESS | 0.063 INCHES MINIMUM AND 0.073 INCHES MAXIMUM |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| MATERIAL | ALUMINUM ALLOY 7075 |
| SPECIAL FEATURES | THREE HOLES IRREGULARLY PLACED ALONG CENTER LINE 0.218/0.229 IN. DIA |
| END ITEM IDENTIFICATION | USED ON SENTRY F22 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CHANNEL |