TBM
PILOT’S OPERATING HANDBOOK
700
SECTION 4
NORMAL PROCEDURES
EASA Approved
Page 4.4.36
Edition 1 -- November 30, 2010
Rev. 0
AMPLIFIED PROCEDURES
AFTER STARTING ENGINE (1/4)
1 -- ”AVIONICS” MASTER switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . .
2 -- ”AP TRIMS” MASTER switch
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . .
3 -- ”GENERATOR” selector
For these tests, ”BLEED VALVE” switch must be left OFF, to unload
the generator circuit.
-- On ”MAIN”
Voltage and current checked
. . . . . . . . . . . . . . . . .
when battery current
≤
50 amps :
-- on ”ST--BY”
Voltage and current checked
. . . . . . . . . . . . . . . . .
(reset if necessary)
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”
4 -- 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 700.
-- Brightness
ADJUST
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If necessary
-- DISPLAY BACKUP button
CHECK
. . . . . . . . . . . . . . . . . . . . . . .
then return to NORMAL mode
If battery current < 100 A :
5 -- ECS panel
Selecting the air conditioning system ON will start the blower. To
avoid overloading the generator, ensure ammeter reading is less
than 100 amperes.
-- ”BLEED VALVE” switch
ON (LO or HI)
. . . . . . . . . . . . . . . . . . . .
