NSN 9540-01-353-6237
Part Details | STRUCTURAL BEAM
9540-01-353-6237 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: 3E99, 3E-99, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 6012312024O, 60-1231/2024-O, 9540-01-353-6237, 01-353-6237, 9540013536237, 013536237
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | FEB 13, 1992 | 01-353-6237 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
H SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-353-6237
Part Number | Cage Code | Manufacturer |
---|---|---|
3E-99 | 43999 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
60-1231/2024-O | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-353-6237
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY 2024 |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
FABRICATION METHOD | EXTRUDED |
SURFACE TREATMENT | ANODIZE |
HEAT TREATMENT | O-ANNEALED |
LENGTH | 12.000 FEET NOMINAL |
BASIC SHAPE STYLE | H SHAPE |
OVERALL WIDTH | 2.000 INCHES NOMINAL |
LEFT SIDE FLANGE HEIGHT | 3.750 INCHES NOMINAL |
RIGHT SIDE FLANGE HEIGHT | 3.750 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
RIGHT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
WEB FLANGE THICKNESS | 0.500 INCHES NOMINAL |
LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
RIGHT BOTTOM 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 |
FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
WEIGHT PER UNIT MEASURE | 2.192 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | O TEMPER AND 10AC FINISH |
END ITEM IDENTIFICATION | B-1B ACFT |