Daher-Socata TBM 900 Pilot's Information Manual page 211

SECTION 4
NORMAL PROCEDURES
EASA Approved
AFTER STARTING ENGINE (1/3)
1 - PFD 1, MFD and PFD 2
2 - "GENERATOR" selector
For these tests, "BLEED" switch must be left OFF, to unload the generator circuit.
- On "MAIN" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
when current ≤ 50 amps :
- on "ST-BY" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If the indicated voltage on the "ST-BY" generator is low (close to 27 volts), reset the "ST-BY" generator and
recheck the voltage.
The indicated voltage should be in the green range.
- then again on "MAIN"
3 - "AP / TRIMS" switch
4 - Oxygen supply . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 - PFD 1, MFD and PFD 2
Detailed control procedures of G1000 avionics system are described in the "GARMIN" G1000 Integrated
Flight Deck Cockpit Reference Guide for the Socata TBM 900.
- Brightness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- DISPLAY BACKUP button
When ammeter < 100 A :
6 - ECS panel
- "BLEED" switch
- "A/C" switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
A cabin temperature good regulation will only be obtained, if "A/C" switch is set to AUTO.
- PRES MODE
- "CONTROL" selector
- "TEMP/° C" selectors
- "HOT AIR FLOW" distributor
Usually selected to CABIN. However, if canopy misting is evident, select DEFOG to increase demisting
efficiency.
Page 4.4.20
GENERATOR LOAD < 200 AMPS
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PILOT'S OPERATING HANDBOOK
CAUTION
Voltage and current checked
Voltage and current checked
Available for the planned flight
(see tables of paragraph "IN-FLIGHT AVAILABLE
OXYGEN QUANTITY" in this Chapter
and Chapter 7.10 for a FAR 135 type operation)
then return to NORMAL mode
NORMALmode
(reset if necessary)
ON
Adjust if necessary
Check
AUTO
AUTO
AUTO
As required
Adjust
As required
Edition 0 -- October 31, 2013
Rev. 1