Daher TBM 850, Pilot'S Information Manual

Page: 359 / 1225

SECTION 4
NORMAL PROCEDURES
EASA Approved
T B M
850 PILOT’S OPERATING HANDBOOK
AMPLIFIED PROCEDURES Page 4.4.37 Edition 1 -- June 22, 2007
Rev. 14
AMPLIFIED PROCEDURES
AFTER STARTING ENGINE (1/4)
1 -- ”GENERATOR” selector
For these tests, ”BLEED” switch must be left OFF, to unload the
generator circuit.
On ”MAIN”
Voltage and current checked . . . . . . . . . . . . . . . . . . .
when 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”
2 -- ”AVIONICS” MASTER switch ON . . . . . . . . . . . . . . . . . . . . . . . . . . .
3 -- ”AP TRIMS” MASTER switch ON . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 -- ”FUEL SEL” switch AUTO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 -- ”SHIFT” push--button PRESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Verify rotation of FUEL TANK SELECTOR
6 -- Oxygen supply 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)
7 -- LEFT PFD REVERSIONARY mode DISENGAGED . . . . . . . . . . . .
(“DISPLAY BACK UP” button “IN”)
8 -- PFD 1, MFD and PFD 2
Detailed control procedures of G1000 avionics system are
described in the ”GARMIN” G1000 Integrated Flight Deck Pilot’s
Guide for the Socata TBM 850.
Brightness
ADJUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If necessary
DISPLAY BACKUP button CHECK . . . . . . . . . . . . . . . . . . . . . . . . . .
then return to NORMAL mode
PIM - DO NOT USE FOR FLIGHT OPERATIONS