Maximum take-off weight is increased by, to and the range is extended by; this is achieved by reducing flight loads, partly from optimising the fly-by-wire control laws.
This is achieved by reducing flight loads, partly from optimising the fly-by-wire control laws. Maximum take-off weight is increased by, to and an additional in range.
Maximum take-off weight is increased by, to and an additional in range. This is achieved by reducing flight loads, partly from optimising the fly-by-wire control laws.
Maximum take-off weight is increased by, to and an additional in range. This is achieved by reducing flight loads, partly from optimising the fly-by-wire control laws.