NSN 9540-01-094-6109

Part Details | STRUCTURAL BEAM

9540-01-094-6109 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: AND101362007, AND10136-2007, ASTM B221, AND101362007ASTM B2210, AND10136-2007/ASTM B221-0, QQA20011, QQ-A-200/11, MS14374E019, AMSQQA20011, AMS-QQ-A-200/11, 101362007, 10136-2007, CVC10010545CA, CVC10010-545CA, 9540-01-094-6109, 01-094-6109, 9540010946109, 010946109

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAY 12, 198001-094-610937018 ( 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 9540-01-094-6109
Part Number Cage Code Manufacturer
AND10136-200799237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
AND10136-2007/ASTM B221-014153DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
MS14374E01996906MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
10136-200729321TRANSTAR METALS CORP
CVC10010-545CA80378TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT
Technical Data | NSN 9540-01-094-6109
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT O-ANNEALED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE T SHAPE
OVERALL HEIGHT1.750 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.094 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.094 INCHES NOMINAL
LEG THICKNESS0.094 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.000 INCHES NOMINAL
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.000 INCHES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.125 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.125 INCHES NOMINAL
TOP FLANGE WIDTH2.000 INCHES NOMINAL
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE LOWER RADIUS
FIRST TIP RADIUS0.094 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPS NOT IDENTICAL
THIRD TIP STYLE FULL RADIUS
THIRD TIP RADIUS0.047 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.415 POUNDS PER LINEAR FOOT