CS-VLA 155 Ā Elevator control forces in manoeuvres
ED Decision 2003/18/RM
The elevator control forces during turns or when recovering from manoeuvres must be such that an increase in control forces is needed to cause an increase in load factor. It must be shown by flight measurements that the stick force per āgā is such that the stick force to achieve the positive limit manoeuvring load factor is not less than 7 daN in the clean configuration.
Loading collections...