NSN 9540-01-491-0767
Part Details | STRUCTURAL BEAM
9540-01-491-0767 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: BAC1505100032 7075T0, BAC1505-100032 7075-T0, 9540-01-491-0767, 01-491-0767, 9540014910767, 014910767
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 12, 2001 | 01-491-0767 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-491-0767
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| BAC1505-100032 7075-T0 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-01-491-0767
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.108 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.108 INCHES NOMINAL |
| LEG THICKNESS | 0.063 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.840 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.160 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T0 TEMPER |
| END ITEM IDENTIFICATION | AIRCRAFT,AWACS,E-3A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUSION |