suurim koormus, millel õhusõiduki kere läheb katki
the limit load multiplied by the appropriate factor of safety
in stress analysis, the minimum load that in its last increment causes a physical breakdown in an aircraft or component during a strenght test or a load that, according to computation, should cause such breakdown
Это интересно
Valdkond ICAO lisade põhjal loodud klassifikaatori järgi: Lennukõlblikkus
In the various loading conditions prescribed in 3.6, no part of the aeroplane structure shall sustain detrimental deformation at
any load up to and including the limit load, and the aeroplane structure shall be capable of supporting the ultimate load.
