Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 4.4.38
Before taxiing
2/4
►
Continuing
8 -
Ng
Increase
≈
80 %
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
To check AIRFRAME DE ICE
●
NOTE
●
Theoretically, necessary air bleed to inflate wing and empennage leading
edges, as well as depression necessary to their deflation are sufficient when
THROTTLE is positioned on Flight IDLE. However, it is advised for check to
choose a Ng power > 80 % in order to obtain operation design pressure, which
enables illuminating surely in green the status light and avoiding
VACUUM LOW
untimely alarms.
●
9 -
AIRFRAME DE ICE system
Check ON
. . . . . . . . . . . . . . . . . . . . . . . . . .
Check illumination in green of the status light
10 -
Visually check functioning of deicer boots during 1 total cycle.
●
NOTE
●
The cycle lasts 67 seconds. Check both inflation impulses :
- the first impulse inflates the external and middle wing boots,
- the second impulse inflates the leading edge boots of empennages and inner
wing.
●
11 -
AIRFRAME DE ICE switch
OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 -
DE ICE SYSTEM mode switch
AUTO
. . . . . . . . . . . . . . . . . . . . . . . . . . .
13 -
INERT SEP switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Keep ON while taxiing in order to avoid ingestion of particles by the engine
14 -
Flight controls
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Proper operation from stop to stop, full deflection
Check autopilot and electrical pitch trim :
15 -
AP / TRIMS
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
●
NOTE
●
Detailed control procedures of autopilot and electrical pitch trim are described in
the GARMIN Integrated Flight Deck Pilot's Guide.
●
Continue
►
PIM - DO NOT USE FOR FLIGHT OPERATIONS
