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#1
October 3rd 03, 01:58 PM
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snip
.. JAR further requires that the break load be no lower than 1.5 times the allowed load. Yes, 1.5 times is the ulimiate design factor for the aircraft. However 1.0 times the allowed load is the limit facter. If you exceed the limit factor you may (will?) damage the aircraft structure but it will not fail until 1.5 times the limit. This is especially true of metal structures where the material itself will fail (i.e. Break) at about 1.5 times the yeild strength(i.e. bend permanently). Brian Case CFIIG/ASEL snip 
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