Tecnam P2010, Flight Manual

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AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 3-25
10. O
THER EMERGENCIES
10.1 L
OSS OF
E
SSENTIAL
B
US
In case of loss of essential bus, the following will be lost (related breakers are listed):
PFD/MFD FLAP ACTUATOR
COM1 PITOT HEAT
GPS/NAV1 STROBE LIGHT
EIS LANDING LIGHT
FUEL PUMP AHRS
FIELD ADC
STALL WARNING ANN. PANEL
XPDR
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/NAV2.
Engine parameters and related warnings/cautions are lost.
Flaps extension and retraction will be lost, apply Flaps control failure procedure
(See Para 10.6).
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 L
OSS OF
M
AIN
B
US
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
NAV LIGHT
INSTRUMENT (clock,
pitch trim indic.)
A.D.I. (available running on internal bat-
tery power)
TAXI LIGHT COM2
INSTR. LIGHT 28/12 VDC CONVERTER
NAV2
CABIN LIGHT RUDDER TRIM ACTUATOR
ADF
START 12VDC SOCKET
DME
Fail safe operation of audio panel allows pilot to transmit and use COM1 using
headphones only; speakers will not be available.
For night flights, all instrument lights will be lost, but emergency light will still be
available.
Ed. 1, Rev.0
Section 3 – Emergency procedures -
OTHER EMERGENCIES