NSN 9540-01-443-7365
Part Details | STRUCTURAL BEAM
9540-01-443-7365 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: 20006200101, 200062001-01, L21020571RS, L2102057/1RS, 9540-01-443-7365, 01-443-7365, 9540014437365, 014437365
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | APR 16, 1997 | 01-443-7365 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-443-7365
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 200062001-01 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| L2102057/1RS | 43999 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-443-7365
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| FABRICATION METHOD | ANY ACCEPTABLE |
| LENGTH | 23.970 INCHES MINIMUM AND 24.030 INCHES MAXIMUM |
| BASIC SHAPE STYLE | T SHAPE |
| LEFT SIDE TOP FLANGE THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.760 INCHES MINIMUM AND 0.780 INCHES MAXIMUM |
| TOP FLANGE WIDTH | 1.670 INCHES MINIMUM AND 1.690 INCHES MAXIMUM |
| RIGHT TOP INSIDE ANGLE | 95.2167 DEGREES MINIMUM AND 96.2167 DEGREES MAXIMUM |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| SPECIAL FEATURES | USED IN THE HS PROJECT. THE /1RS IS USED TO MAKE P/N -003/005/007/009/0013/015/017/019/023/025/027 |
| FSC APPLICATION DATA | STRUCTURAL SHAPES |
| END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLANGE,RS |