PILOT’S OPERATING HANDBOOK
SECTION 4
NORMAL PROCEDURES
EASA Approved
Edition 0 -- October 31, 2013
Rev. 1
Page 4.4.28
TAKEOFF (1/2)
WHEN LINED UP
CAUTION
IF HEAVY PRECIPITATION, TURN IGNITION AND INERT SEP ON.
IF ICING CONDITIONS ARE FORESEEN, REFER TO CHAPTER 4.5, PARAGRAPH ”FLIGHT
INTO KNOWN ICING CONDITIONS”.
1 - Horizon
Check attitude
$
+ 2
°
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Horizon has been set so as to indicate a 2
°
nose up attitude, when airplane center of gravity is at a middle
average.
2 - Heading - HSI - Stand-by compass
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
The indication of the stand-by compass is disturbed when windshield deice systems are activated.
-
Altimeter setting on PFDs 1/2
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3 - Lights
-
”OFF/TAXI/LDG” switch
LDG
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 - Engine instruments
CHECK
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(ITT = green sector)
5 - CAS display
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
All messages OFF,
except
”INERT SEP ON”
if used
except
”IGNITION”
if used
6 - Apply brakes and increase power up to RPM in green range.
7 - Brakes
Released
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Torque will be about 40 % to 60 % before brake release. For a normal takeoff, maximum torque (100 %) will
be applied after brake release. On short runway, maximum torque will be applied before brake release.
8 - Throttle
TRQ = 100 %
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9 - Takeoff attitudes
-
Normal takeoff
Attitude : 10°
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
Short takeoff
.
Weight < 6579 lbs (2984 kg)
Attitude : 15
°
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
.
Weight
≥
6579 lbs (2984 kg)
Attitude : 12
°
5
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10 - Vertical speed indicator
Positive
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 - Brakes
Apply
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Briefly)
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 ...