PILOT’S OPERATING HANDBOOK
SECTION 4
NORMAL PROCEDURES
EASA Approved
Edition 0 -- October 31, 2013
Rev. 1
Page 4.4.21
AFTER STARTING ENGINE (2/3)
7 - Stand-by instruments
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 - ADI/HSI on PFD1 / PFD2
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9 - Altimeter setting
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10 - VHF/VOR/GPS
Adjusted - Tested
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
Radar/Stormscope/TAS/TAWS/Radio altimeter (if installed)
Adjusted - Tested
. . . . . . . . . . .
11 - MFD flight management
-
Weight computing
Set/Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
FOB synchro
Set
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
FPL (if requested)
Set
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 - AP / TRIMS
-
”AP / TRIMS” operation
Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Detailed control procedures of autopilot and electrical pitch trim are described in the ”GARMIN” G1000
Integrated Flight Deck Cockpit Reference Guide for the Socata TBM 900.
-
Pitch trim
UP / DN, then adjusted
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Adjust the indicator in green range (graduated from 12 to 37 %).
-
Yaw trim
L / R, then adjusted
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Adjust the indicator in green range TO (TAKEOFF).
-
Roll trim
L / R, then adjusted
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Adjust the indicator first at neutral position (horizontal marker).
13 - DE ICE SYSTEM panel
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Flight into known icing conditions is authorized only when all ice protection equipment are operating
correctly. This equipment may be activated before takeoff, even during taxiing, in case of icing conditions on
ground. Refer to Chapter 4.5 ”PARTICULAR PROCEDURES” of this Section.
-
”PROP DE ICE” switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Check illumination of the green light located
above the switch
Illumination of the green light shows that power supplied to blade root electric resistors is between 8 and
10 amperes. It is advised to wait at least a whole half cycle (90 seconds) to check that both blade pairs are
correctly deiced.
-
”PROP DE ICE” switch
OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
”WINDSHIELD” switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Check illumination of the green lights located
above the switch (except if hot conditions)
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 ...