Pipistrel Virus SW 121, Руководство по эксплуатации для пилотов

Страница: 57 / 226

3-21
Virus SW 121
Pilot Operating Handbook
POH-121-00-40-001
PAGE REV. 0
PAGE
SECTION 3
EMERGENCY PROCEDURES
APPROVED
case of a battery failure. To assure generator restart power is available if the
generator fails, the battery disconnect switch should not be pulled during
flight.
NOTE: If it is necessary to reduce electrical loads due to an generator mal-
function, switch off electrical components and/or systems that are not essen-
tial for the current flight conditions rather than pulling circuit breakers. Load
shedding in this manner will prevent accidental circuit breaker disconnec-
tion and loss of power to flight-critical systems.
3.11 ENGINE INDICATING SYSTEM FAILURE
In the event of a Data Acquisition Unit failure, the engine indications displayed
on the MFD and PFD will be disabled.
In the event of Data Acquisition Unit failure, pull and reset the EIS circuit
breaker. If the engine indicating system fails to reset, land as soon as practical.
1 EIS Circuit Breaker CYCLE
2 Land as soon as practical.
3.12 COMMUNICATION FAILURE
1 Switches, Controls, Volume CHECK
2 Frequency CHANGE
3 Circuit Breakers CHECK
4 Headset CHANGE
5 Transmission ATTEMPT
6 If unsuccessful TRANSPONDER 7600
3.13 PITOT STATIC MALFUNCTION
Static Source Blocked
If erroneous readings of the static source instruments (airspeed, altimeter
and vertical speed) are suspected, the information from the GPS system
should be used for situational awareness.