which fails with extreme heat could possible lead to a loss of useful power situation in which the emergency power lever may not be effective. The close proximity of the generator to the FCU can cause the fuel within the FCU to vapor-lock, inh
cable may occur when the aircraft is operated in freezing temperatures.
maintain N1 above 65 percent to improve engine response and ensure the generator stays online.
If resultant power is insufficient to execute a PEL
underpowered that high rates of descent occur, any delay in feathering the propeller may result in insufficient altitude to reach a suitable landing site. It is not recommended to delay feathering the propeller in the landing comfigu
is sufficient to maintain a rate of descent less than the feathered condition (600to 800 fpm clean), consideration should be given to allowing the engine to operate until the field is made.
If suffucuent power is restored
is not recommended when performing a landing using the manual fuel control system. If the use of BETA is required, ensure the EPL is in teh IDLE rande or DISCONNECT before selecting BETA with the PCL