Daher TBM 850, Pilot'S Information Manual

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T B M
PILOT’S OPERATING HANDBOOK 850
SECTION 7
DESCRIPTION
Page 7.3.4 Edition 1 -- June 22, 2007
Rev. 13
Cockpit overhead panel (Figure 7.3.2)
This panel includes following elements :
-- the loud--speaker of GMA # 1,
-- the loud--speaker of GMA # 2,
-- the VMO alarm buzzer,
-- the ”HORN TEST” knob,
-- the emergency lighting rheostat.
It is attached to the cabin upper part between frames C6 and C7.
The VMO alarm buzzer is electrically supplied by ”ESS BUS 2” bar and
protected by ”AURAL WARN” circuit breaker and the emergency lighting
rheostat is electrically supplied by ”BATT BUS” bar and protected by ”PANEL
EMER” circuit breaker.
Aural warning operation
The GMA # 1 and # 2 audio control panels receive signals from the aural
warning box. According to the airplane configuration, these signals are
low--pitched and / or high--pitched.
The ”HORN TEST” knob allows to test the correct operation of aural
warnings :
-- Set the ”SOURCE” selector to BAT or to GPU.
-- Set the “AVIONICS” MASTER switch to ON.
-- Push and hold the ”HORN TEST” knob :
. the VMO buzzer emits ”bips”,
. the loud--speakers emit alternate low--pitched and high--pitched
sounds.
-- Release the knob to stop the alarms.
Post--MOD70--0407--00D (V15.11 GARMIN software)
General alarms warning lights and CAS messages
Warning (red) and Caution (yellow) messages appear on the GDU 1500 MFD
CAS display to alert crew about monitored systems discrepancies. As a
message appears, a chime is heard. Refer to the GARMIN G1000 Pilot’s
Guide to know all possible CAS messages.
PIM - DO NOT USE FOR FLIGHT OPERATIONS