De Ice Boots
3-18-02
continued
CAUTION
On landing approach after boot failure (flaps 0°), the PFD dynamic speed
bug will not be correct and should not be used as reference.
CAUTION
The total landing distance will be longer by up to 160%. Refer to Section 5,
Performance, Flight in Icing Conditions,
Flight in Icing Conditions - Landing
for the exact landing distance calculation.
CAUTION
In the case of heavy brake usage, soft brake pedals and/or wheel fusible
plugs release may occur during a following taxi. Limitation in Section 2,
Systems and Equipment Limits,
---------- END -----------
Inertial Seperator
3-18-03
WARNING
AN INERTIAL SEPARATOR FAILURE IN ICING CONDITIONS CAN CAUSE
DEGRADATION OF THE AIRCRAFT ENGINE PERFORMANCE (AN INCREASE
IN ITT).
AN INERTIAL SEPARATOR FAILURE DURING OPERATIONS IN FOREIGN
OBJECT DAMAGE (FOD) ENVIRONMENTS MAY CAUSE LONG TERM
ENGINE DETERIORATION AND SHOULD BE REPORTED FOR POST FLIGHT
MAINTENANCE.
1.
INERT SEP switch......................
Set to CLOSED and wait 30 seconds
2.
INERT SEP switch......................
Set to OPEN
3.
INERT SEP circuit breaker
(Essential Bus
L
F2).....................
Check. Do not reset unless tripped
If caption returns to normal operation after 45 seconds:
4.
Aircraft.........................................
Continue flight and monitor system
If caption stays in failure status after 45 seconds:
5.
INERT SEP switch......................
Maintain OPEN (together with ICE PROP
PROTECTION PROPELLER ON) to
maintain PUSHER ICE MODE
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 3-18-3
12-C-A15-40-0318-00A-141A-A
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GENERAL
AND
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PURPOSES
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