NSN 9540-01-543-4432
Part Details | STRUCTURAL BEAM
9540-01-543-4432 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: LS393071, LS39307-1, 9540-01-543-4432, 01-543-4432, 9540015434432, 015434432
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | SEP 13, 2006 | 01-543-4432 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
Cross Reference | NSN 9540-01-543-4432
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LS39307-1 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 9540-01-543-4432
| Characteristic | Specifications |
|---|---|
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 1.288 INCHES MINIMUM AND 1.312 INCHES MAXIMUM |
| LEFT SIDE TOP FLANGE THICKNESS | 0.085 INCHES MINIMUM AND 0.095 INCHES MAXIMUM |
| LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.034 INCHES MINIMUM AND 2.086 INCHES MAXIMUM |
| TOP FLANGE WIDTH | 4.056 INCHES MINIMUM AND 4.128 INCHES MAXIMUM |
| SPECIAL FEATURES | BASIC T CONFIGURATION WITH FLANGE ON VERTICAL LEG |
| END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | T SECTION-CHEM MILL |