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Jabiru Aircraft
Pilot Operating Handbook
Model J170-C
JP-FM-08
Revision:
0
3 April 2007
Page 43
Alternator failure is indicated by the illumination of the “CHG FAIL” light on the instrument panel.
While the Jabiru engine does not require external power to run, power consumption by the radio,
transponder and other electrical systems will eventually discharge the battery.
6.2.10
Spins
Intentional spins are prohibited in this aircraft. Should an inadvertent spin occur, the
following recovery procedure should be used:
1. Retard the throttle to idle
2. Centralise ailerons
3. Apply and hold full rudder opposite to the direction of rotation
4. Move stick progressively forward far enough to break stall
5.
Hold these control inputs until rotation stops
6.
As rotation stops, centralise rudder and make a positive, smooth recovery from
the resulting dive
WARNING
If the spin is encountered with flaps extended, DO NOT retract flaps until rotation ceases.
Premature flap retraction will delay recovery.