NSN 9540-01-475-0888
Part Details | STRUCTURAL BEAM
9540-01-475-0888 A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges.
Alternate Parts: CVC1003116CA, CVC10031-16CA, 9540-01-475-0888, 01-475-0888, 9540014750888, 014750888
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAY 22, 2000 | 01-475-0888 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
I SHAPE
SQUARE END
SQUARE END
SQUARE END
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Cross Reference | NSN 9540-01-475-0888
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CVC10031-16CA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-475-0888
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430, ALLOY 7075 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | ANY ACCEPTABLE |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | I SHAPE |
| OVERALL HEIGHT | 2.050 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.055 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.055 INCHES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.015 INCHES NOMINAL |
| LEFT SIDE BOTTOM FLANGE THICKNESS | 0.015 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.630 INCHES NOMINAL |
| LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.630 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.680 INCHES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.680 INCHES NOMINAL |
| WEB FLANGE THICKNESS | 0.055 INCHES NOMINAL |
| TOP FLANGE WIDTH | 1.310 INCHES NOMINAL |
| BOTTOM FLANGE WIDTH | 1.310 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 11.0 DEGREES NOMINAL |
| LEFT BOTTOM INSIDE ANGLE | 11.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 169.0 DEGREES NOMINAL |
| RIGHT BOTTOM INSIDE ANGLE | 169.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| END ITEM IDENTIFICATION | INTERMEDIATE; AIRCRAFT B-2 BOMBER (ATB) |