The ultimate load is related to the safety factor, j.
2.
Its span wing has g ultimate load.
3.
The design load factor is 3.8 g, with an ultimate load of 5.7 g.
4.
With respect to aircraft structure and design, ultimate load is the amount of load applied to a component beyond which the component will fail.
5.
Thanks to its ultimate load factor of 15.1, it could dive as fast as 500 mp . h . ( True Air Speed ).
6.
Unlike civilian aircraft, NATO aircraft frame strength is required to remain without detrimental deformations at 115 percent of the limit or specified loads, and without structural failure at ultimate loads.
7.
Strength requirements are specified in terms of limit loads ( the maximum loads to be expected in service ) and ultimate loads ( limit loads multiplied by prescribed factors of safety ).
8.
The marketing failure of these airplanes demonstrated that airlines were generally unwilling to accept reduced efficiency at cruise and smaller ultimate load-carrying capacity in return for a slight performance gain at particular airports.
9.
"Regia Aeronautica " requested Zappata's proposal be modified to incorporate greater strength : the design ultimate load factor was to be increased from 7.0 to 10.0.
10.
The Renegade II wing design was sand-bag tested on 16 February 1988 to, or + 7.2 g working load, with a + 10 and-6 gs ultimate load.
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