§ 25.672 Stability augmentation and automatic and power-operated systems
If the functioning of stability augmentation or other automatic or power-operated systems is necessary to show compliance with the flight characteristics requirements of this part, such systems must comply with
§ 25.671 and the following:
(a) A
warning which is
clearly distinguishable to the pilot under expected flight conditions without requiring his attention must be provided for any failure in the stability augmentation system or in any other automatic or power-operated system which could result in an unsafe condition if the pilot were not aware of the failure. Warning systems must not activate the control systems.
(b) The design of the stability augmentation system or of any other automatic or power-operated system
must permit initial counteraction of failures of the type specified in
§ 25.671(c) without requiring exceptional pilot skill or strength, by either the deactivation of the system, or a failed portion thereof, or by overriding the failure by movement of the flight controls in the normal sense.
(c) It
must be shown that after
any single failure of the stability augmentation system or any other automatic or power-operated system -
(1) The
airplane is safely controllable when the failure or malfunction occurs
at any speed or altitude within the approved operating limitations that is critical for the type of failure being considered;
(2) The
controllability and maneuverability requirements of this part are met
within a practical operational flight envelope (for example, speed, altitude, normal acceleration, and
airplaneconfigurations) which is described in the
Airplane Flight Manual; and
(3) The
trim, stability, and stall
characteristics are not impaired below a level needed to permit continued safe flight and landing.
[Amdt. 25-23, [url=https://www.law.cornell.edu/rio/citation/35_FR_5675]35 FR 5675 Apr. 8, 1970]