Manufacturer is responsible for defining a procedure for both
failure conditions.
Loss of Power
Aircraft Manufacturer is responsible for defining a procedure for
this failure condition.
4.2) Failures during engine start
4.2.1) Engine does not start
Insufficient supply from electrical power source.
• Ensure that Engine starter and EMS system is supplied by an
external power source until engine reached idle speed
Insufficient fuel supply.
• Ensure that Engine is supplied with fuel in appropriate quality
Starting at low oil temperature.
• Use high quality oil without friction modifier see
.
4.3) Re-Start during flight
If the propeller continues to rotate during flight by windmilling,
but the speed is not sufficient to start the engine, the electric
starter can be used. It is not required to wait until the propeller
stand still.
4.4) The sprag clutch fails to decouple from the starter
ATTENTION
Shut down engine!
Risk of fire and danger of the electric starter overheating.
Follow engine shut OFF procedure (see
).
4.5) Exceedance of operational limits
ATTENTION
When exceeding a operating limit, adapt engine power setting.
Any exceeding of an operating limit has to be entered by the pi-
lot into engine logbook, stating duration and duration of this
condition. Unscheduled maintenance action may be required
(see Maintenance Manual Line).
Aircraft Manufacturer is responsible for defining an abnormal
operation procedure for each operating limit.
Page 4-6
December 01 2017
BRP-Rotax
Effectivity: 915 i A Series
Edition 0 / Rev. 0
Summary of Contents for 898851
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