PILOT’S OPERATING HANDBOOK
SECTION 4
NORMAL PROCEDURES
EASA Approved
Edition 0 -- October 31, 2013
Rev. 1
Page 4.4.25
BEFORE TAKEOFF (1/3)
CAUTION
GENERATOR LOAD < 200 AMPS
1 - Park brake
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WARNING CAS MESSAGE
”PARK BRAKE”
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 - Throttle
Flight IDLE
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
[Ng : 69 % (
±
2 %)]
3 - Throttle
Flight IDLE to HI / IDLE twice,
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
then Flight IDLE
During this test, keep the time spent with the propeller RPM in the caution (yellow) range at a minimum.
4 - Flaps
TO
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 - DE ICE SYSTEM panel
As required
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
”AIRFRAME DE ICE” switch
As required
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
”PROP DE ICE” switch
As required
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If runway is in good condition, without icing conditions :
-
”INERT SEP” switch
As required
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WARNING CAS MESSAGE
”INERT SEP ON”
As required
. . . . . .
CAS message goes out immediately, but it takes 30 seconds to retract the separator.
If there is standing water or other contamination on the runway :
-
”INERT SEP” switch
Leave ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WARNING CAS MESSAGE
”INERT SEP ON”
ON
. . . . . . . . . . . . . .
-
”WINDSHIELD” switch
As required
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
”PITOT L HTR” switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
”PITOT R & STALL HTR” switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If icing conditions are foreseen, refer to Chapter 4.5 ”PARTICULAR PROCEDURES” of this Section, Paragraph
”Flight into known icing conditions”.
6 - Flight controls
Deflections checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Содержание TBM 900
Страница 349: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 2 7 Figure 7 2 2 2 2 WING FLAPS ...
Страница 385: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 3 Figure 7 4 1 2 2 ROLL ...
Страница 390: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 8 Figure 7 4 3 2 2 ELEVATOR ...
Страница 395: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 13 Figure 7 4 5 2 2 RUDDER ...
Страница 398: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 16 INTENTIONALLY LEFT BLANK ...
Страница 410: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 5 12 Figure 7 5 6 PARKING BRAKE ...
Страница 413: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 6 3 Figure 7 6 1 2 2 POWERPLANT ...