ED Decision 2016/010/R
(See AMC 25.905)
(a) reserved
(b) Engine power and propeller shaft rotational speed may not exceed the limits for which the propeller is certificated. (See CS-P 50.)
(c) Each component of the propeller blade pitch control system must meet the requirements of CS-P 420.
(d) Design precautions must be taken to minimise the hazards to the aeroplane in the event a propeller blade fails or is released by a hub failure. The hazards which must be considered include damage to structure and critical systems due to impact of a failed or released blade and the unbalance created by such failure or release. (See AMC 25.905(d).)
[Amdt 25/3]
[Amdt 25/18]
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