Inertial Seperator
3-18-03
continued
6.
Aircraft.........................................
DEPART ICING CONDITIONS to positive
SAT atmosphere, if possible
7.
Aircraft.........................................
Avoid further icing conditions
If any attained performance degradation continues:
8.
Aircraft.........................................
Land as soon as possible
---------- END -----------
LH Windshield Heat
LH + RH Windshield Heat
RH Windshield Heat
3-18-04
1.
LH W/SHLD circuit breaker (LH
PJB)............................................
Check. Do not reset unless tripped
2.
LH WSHLD switch......................
Set to OFF then to LIGHT or HEAVY
3.
RH W/SHLD circuit breaker (RH
PJB)............................................
Check. Do not reset unless tripped
4.
RH WSHLD switch......................
Set to OFF then to LIGHT or HEAVY
If caption returns to normal operation:
5.
Aircraft.........................................
Continue flight and monitor system
If caption stays in failure status and forward visibility through LH windshield is lost:
6.
Windshield..................................
Use RH windshield
If total forward visibility is lost:
7.
Aircraft.........................................
DEPART ICING CONDITIONS to positive
SAT atmosphere, if possible. Interior
fogging can be cleared by hand
8.
Aircraft.........................................
Avoid further icing conditions
If windshield has not cleared by time of landing:
9.
Cabin pressure............................
Make sure depressurized
10.
DV window..................................
Use, if required
---------- END -----------
Probes Off
3-18-05
Probes not on with static air temperature below 10 °C.
1.
PROBES switch..........................
Set to ON
---------- END -----------
Section 3 - Emergency Procedures (EASA Approved)
Deice Systems
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3-18-4
12-C-A15-40-0318-00A-141A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
