Static Heat
3-18-08
continued
3.
RH STATIC DE-ICE circuit
breaker (Main Bus
R
F2)..............
Check. Do not reset unless tripped
If caption returns to normal operation:
4.
Aircraft.........................................
Continue flight and monitor system
If caption stays in failure status:
5.
Autopilot......................................
Disconnect
6.
Aircraft.........................................
DEPART ICING CONDITIONS to positive
SAT atmosphere, if possible
7.
Aircraft.........................................
Avoid further icing conditions
8.
Aircraft.........................................
Land as soon as possible
9.
Landing approach.......................
Keep speed as indicated by Dynamic
Speed Bug (1.3 V
S
) with PUSHER ICE
MODE and flaps 15°. Maintain speed
above shaker activation
CAUTION
The total landing distance will be longer by up to 71%. Refer to Section 5,
Performance, Flight in Icing Conditions,
Flight in Icing Conditions - Landing
for the exact landing distance calculation.
---------- END -----------
Pusher
3-18-09
WARNING
A FAILURE OF THE STALL WARNING/STICK PUSHER SYSTEM TO RE-
DATUM TO ICE MODE WHEN IN ICING CONDITIONS CAN LEAVE THE
AIRCRAFT UNPROTECTED AGAINST THE NATURAL STALL WITH
RESIDUAL ICE ON THE AIRFRAME.
1.
STICK PUSHER test switch........
Press and hold for duration of Pusher test
sequence (approx. 5 seconds) (this
identifies Pusher ice mode computer or
selection failure)
If failure stays during test go to Step 7.
If failure disappears during test but returns after completion of test:
2.
PROPELLER switch...................
Cycle from OFF to ON
3.
INERT SEP switch......................
Cycle from CLOSED to OPEN
Continued on next page
Section 3 - Emergency Procedures (EASA Approved)
Deice Systems
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3-18-7
12-C-A15-40-0318-00A-141A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
