Part Details | STRUCTURAL BEAM
9540-00-001-5119 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: QQA20011, QQ-A-200/11, QQA20011, QQ-A-200/11, LS33758, LS337581, LS33758-1, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-001-5119, 00-001-5119, 9540000015119, 000015119
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | SEP 29, 1972 | 00-001-5119 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-001-5119
Part Number | Cage Code | Manufacturer |
---|---|---|
QQ-A-200/11 | 71176 | EMERSON ELECTRIC COBROWNING MFG DIV |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
LS33758 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
LS33758-1 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-001-5119
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 | 1.850 INCHES NOMINAL |
LEFT SIDE TOP FLANGE THICKNESS | 0.213 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE THICKNESS | 0.213 INCHES NOMINAL |
LEG THICKNESS | 0.288 INCHES NOMINAL |
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.646 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.654 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 | 7.300 INCHES NOMINAL |
LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
RIGHT TOP 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 |
WEIGHT PER UNIT MEASURE | 2.439 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
USAGE DESIGN | STRUCTURAL |