CS-VLA 155 Elevator control forces in manoeuvres

• ED Decision 2003/18/RM found in: CS-VLA Amdt 1 - Very Light Aeroplanes (Mar 2009)

CS-VLA 155 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 ‘g’ is such that the stick force to achieve the positive limit manoeuvring load factor is not less than 7 daN in the clean configuration.