10.
OTHER
EMERGENCIES
10.1.
Loss OF
ESSENTIAL
Bus
In case
ofloss
of
essential bus, the following will be lost (related breakers are listed):
PFD
FLAP
ACTUATOR
CO
Ml
PITOT
HEAT
GPSl/NAVl
STROBE
LIGHT
EIS
LANDING
LIGHT
FUEL
PUMP
AHRS
FIELD
ADC
STALL
WARNING
ANN.
PANEL
Electrical power from Alternator is lost, battery will automatically provide energy
(duration at least 30 min.).
Pilot will need to make reference to standby instrument for primary flight infor-
mation and parameters.
Pilot will be able to use the audio panel and COM2/NA V2 via MFD.
Engine parameters and related warnings/cautions are lost.
Flaps extension and retraction will be lost, apply Flaps control failure procedure
(See Para I 0.6).
Strobe and landing lights will be lost, NAV and taxi lights are still available;
taxi light will be the only visual aid for landing in night conditions.
10.2.
Loss OF
MAIN
Bus
In
case
of
loss
of
main bus, the main bus voltage will drop to zero.
The following will be lost (related breakers are listed):
AUDIO
PANEL
START
RUDDER
TRIM
ACTUATOR
INSTR.
LIGHT
A.D.I. (running on internal battery power)
NAV
LIGHT
28/12
VDC
CONVERTER
(if
installed)
TAXI
LIGHT
12VDC
SOCKET
(if
installed)
CABIN
LIGHT
INSTRUMENT
(clock,
pitch trim
indic.)
FAN
(GlOOO)
COPILOT
SEAT
(if
installed)
PILOT
SEAT
(if
installed)
AVIONIC
MFD
COM2
GPS2/NAV2
ADF
XPDR
DME
Fail safe operation
of
Garmin
01000
allows pilot to transmit and use COMI using
headphones only; speakers will not be available.
For night flights, all instrument lights will be lost, but emergency light will still be
available.
2"d
Edition, Rev.3
Section
3 -
Emergency
procedures
OTHER
EMERGENCIES
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