Pipistrel Virus SW 121, Руководство по эксплуатации для пилотов

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3-19
Virus SW 121
Pilot Operating Handbook
POH-121-00-40-001
PAGE REV. 0
PAGE
SECTION 3
EMERGENCY PROCEDURES
APPROVED
3.8.4 LANDING WITH A DEFECTIVE MAIN LANDING GEAR TIRE
1
Land the airplane at the edge of the runway that is located on the
side of the intact tire, so that changes in direction during roll-out due
to the braking action of the defective tire can be corrected on the
runway.
2 Land with the wing low on the side of the intact tire.
3
Direction should be maintained using the rudder. This should be
supported 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-off 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 harness CHECK FASTENED AND TIGHTENED
After a safe touch-down:
2 Ignition OFF
3 Fuel Selector OFF
4 Master Switch OFF
3.9 PFD-MALFUNCTION
In the unlikely event of a PFD failure, the pilot may lose the ability to control
the autopilot through the PFD controls. If this malfunction occurs, the PFD
circuit breakers may be pulled and the airplane flown using the reversionary
mode, where the MFD screen displays also airspeed, altitude, attitude and
compass information and/or the mechanical instruments.
NOTE: The avionics system is equipped with dual ADAHRS units, which
provide pressure and attitude data to the screens. In event of PFD screen
failure, there is the reversionary mode, which will automatically display main
PFD data (airspeed, altitude, attitude, compass) on the MFD screen.
In case of ADAHRS failures: