NSN 9540-00-804-3097

Part Details | STRUCTURAL BEAM

9540-00-804-3097 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: AND101361403, AND10136-1403, E711107, QQA20011, QQ-A-200/11, E711107, E711107, AMSQQA20011, AMS-QQ-A-200/11, E711107, 9540-00-804-3097, 00-804-3097, 9540008043097, 008043097

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196200-804-309737018 ( 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 9540-00-804-3097
Part Number Cage Code Manufacturer
AND10136-140399237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
E71110763910BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
E7111070WLU1GENERAL DYNAMICS CORPCONVAIR DIV
E71110714170HUGHES MISSILE SYSTEMS COSAN DIEGO
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
E7111077B709TRACOR FLIGHT SYSTEMS INCSUB OF TRACOR INC
Technical Data | NSN 9540-00-804-3097
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6 SOLUTION HEAT TREATED
LENGTH12.000 FEET NOMINAL
BASIC SHAPE STYLE T SHAPE
OVERALL HEIGHT1.000 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.078 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.078 INCHES NOMINAL
LEG THICKNESS0.078 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.750 INCHES NOMINAL
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.750 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 WIDTH1.500 INCHES NOMINAL
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE LOWER RADIUS
FIRST TIP RADIUS0.078 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPS NOT IDENTICAL
THIRD TIP STYLE FULL RADIUS
THIRD TIP RADIUS0.039 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.230 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAT6 TEMPER