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Virus SW 600 D
iS engine POH Supplement
SPOH-127-00-41-001
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SECTION 3
EMERGENCY PROCEDURES
APPROVED
3
Direction should be maintained using the rudder. This should be sup-
ported by use of the brake. It is possible that the brake must be applied
strongly - if necessary to the point where the wheel locks.
CAUTION: A defective tire is not easy to detect. The damage normally
occurs during take-o or landing and is hardly noticeable during fast taxiing.
It is only during the lower taxiing speeds that a tendency to swerve occurs.
3.8.5 LANDING WITH DEFECTIVE BRAKES
1 Safety Belts CHECK FASTENED AND TIGHTENED
After a safe touch-down:
2 LANE A/B Switches OFF
3 Fuel Selector OFF
4 Master Switch OFF
3.10 GENERATOR/ ELECTRICAL SYSTEM FAILURE
Battery Failure
In case of battery failure, be aware that the engine will keep running, howev-
er a re-start will not be possible.
NOTE: When EarthX battery type is installed, battery over-voltage, low
voltage or other battery system malfunctions, are additionally indicated by
the optional Batt Caution light on the switch panel. The rate at which the
light flashes, indicates what type of malfunction or error is in question. Please
refer to EarthX ETX lithium battery user’s manual for additional information
about how to troubleshoot any battery errors/malfunctions. Alternalitvely, the
battery malfunction warning can be displayed on the PFD/MFD when the
battery caution light is not installed.
The EarthX battery disconnects itself in case of over- or undervoltage.
Generator/s Failure
The engine is equipped with two 3-phase A/C current generator (alterna-
tors). Generator A is used by the Engine Control Unit (ECU) and Generator B
is used to power the aircraft systems (avionics, battery charging etc).
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