Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - October 31, 2013
Rev. 5
Page 4.4.38
Before taxiing
2/4
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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 the two green lights and avoiding
VACUUM LOW
untimely alarms.
●
9 -
AIRFRAME DE ICE switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10 -
Visually check functioning of deicer boots during 1 total cycle and
illumination of the two green lights located above the switch.
●
NOTE
●
The cycle lasts 67 seconds. Check both inflation impulses and illumination of
each corresponding green light :
- 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 -
INERT SEP switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Keep ON while taxiing in order to avoid ingestion of particles by the engine
13 -
Flight controls
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Proper operation from stop to stop, full deflection
Check autopilot and electrical pitch trim :
14 -
AP / TRIMS
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
●
NOTE
●
Detailed control procedures of autopilot and electrical pitch trim are described in
the GARMIN Integrated Flight Deck Pilot's Guide.
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Continue
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PIM - DO NOT USE FOR FLIGHT OPERATIONS
