NSN 9540-01-367-1250
Part Details | STRUCTURAL BEAM
9540-01-367-1250 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: AND101361603, AND10136-1603, ASTM B221, 1MA160D0310066, 1MA160D03-10066, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, 9540-01-367-1250, 01-367-1250, 9540013671250, 013671250
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | NOV 07, 1992 | 01-367-1250 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
RIGHT QUARTER RADIUS
SQUARE W/ INNER AND OUTER CORNER RADII
RIGHT QUARTER RADIUS
SQUARE W/ INNER AND OUTER CORNER RADII
RIGHT QUARTER RADIUS
SQUARE W/ INNER AND OUTER CORNER RADII
RIGHT QUARTER RADIUS
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-367-1250
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10136-1603 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1MA160D03-10066 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-367-1250
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 1.125 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| LEG THICKNESS | 0.094 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| TOP FLANGE WIDTH | 1.750 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | 8 RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | 8 RIGHT QUARTER RADIUS |
| SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| THIRD TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| THIRD TIP INNER RADIUS | 0.047 INCHES NOMINAL |
| THIRD TIP OUTER RADIUS | 0.047 INCHES NOMINAL |