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737 composite horizontal 737 horizontal stabilizer access cutout Advanced Composite Stabilizer airframe airline analysis Boeing 737 Aircraft Commercial Transport composite horizontal stabilizer composite material composite structures composite vertical fin composite vertical stabilizer DC-10 composite vertical DC-l0 vertical stabilizer design limit load design ultimate load empennage structures Energy Efficiency ACEE fabrication fail-safe test failure load February l983 figure l9 finite element model flanges front spar full scale ground test article ground test series interlaminar tension L-1011 composite vertical L-l0ll Aircraft L-l0ll fin Langley Research Center LB/IN limit load tests load introduction loose holes lug pin McCarty mechanical fasteners NASA CR plies ponents POUNDS WEIGHT precured primary structure reaction loads rear spar redesigned cover scale composite secondary loads shear load shown in figure simulate sine-wave spar and rib spar cap Stabilizer for Boeing stabilizer was loaded stiffeners strain struc structural failure subcomponent tion Transport Aircraft tural utilization of composites