In aeronautics, "'limit load "'( LL ) is the maximum load factor authorized during flight, Mathematically, limit load is LL = LLF x W, where LL = limit load, LLF = limit load factor, and W = weight of the aircraft.
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In aeronautics, "'limit load "'( LL ) is the maximum load factor authorized during flight, Mathematically, limit load is LL = LLF x W, where LL = limit load, LLF = limit load factor, and W = weight of the aircraft.
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Engine mounts and other structural members are designed for the nominal LLF . The nominal or limit load B n is the load which should only occur once ( or only a very few times ) during the lifetime of an aircraft . B n may therefore only occur once during ( e . g . ) 60, 000 hours of flying.
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