NSN 9540-01-239-6531
Part Details | STRUCTURAL CHANNEL
9540-01-239-6531 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: 332D18023, 332D1802-3, 9540-01-239-6531, 01-239-6531, 9540012396531, 012396531
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | MAR 13, 2006 | 01-239-6531 | 37019 ( CHANNEL, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
CHANNEL
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-239-6531
Part Number | Cage Code | Manufacturer |
---|---|---|
332D1802-3 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-01-239-6531
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
LENGTH | 5.090 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 |
FIRST TIP STYLE | SQUARE END |
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 |