NSN 9540-00-230-2339
Part Details | STRUCTURAL BEAM
9540-00-230-2339 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: AND101362407, AND10136-2407, 31106, ASTM B221, AND101362407QQA20011T6511, AND10136-2407/QQ-A-200/11-T6511, QQA20011, QQ-A-200/11, LS1013624075, LS10136-2407-5, LS101362407, LS10136-2407, AMS101362407, AMS10136-2407, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-230-2339, 00-230-2339, 9540002302339, 002302339
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 10, 1971 | 00-230-2339 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
LOWER RADIUS
FULL RADIUS
LOWER RADIUS
FULL RADIUS
LOWER RADIUS
FULL RADIUS
LOWER RADIUS
FULL RADIUS
Cross Reference | NSN 9540-00-230-2339
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10136-2407 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 31106 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| AND10136-2407/QQ-A-200/11-T6511 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS10136-2407-5 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| LS10136-2407 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| AMS10136-2407 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-230-2339
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEG THICKNESS | 0.125 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 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 | 2.500 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | LOWER RADIUS |
| FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| THIRD TIP STYLE | FULL RADIUS |
| THIRD TIP RADIUS | 0.063 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.650 POUNDS PER LINEAR FOOT |
| USAGE DESIGN | AIRCRAFT |