Piper SEMINOLE 2013 Pilot Operating Handbook page 55

With garmin g1000 system
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PA-44-180, SEMINOLE
3.1
GENERAL (continued)
Crew Alerting System (CAS) Messages
Warnings – Red
Event
High Cylinder Head
Temperature
Low Fuel Quantity
Alternator Failure
Starter Engaged
Landing Gear
Failure
Landing Gear
Position Unsafe
High Heater
Temperature
Underspeed
Protection
*CAS Messages/Alerts may have small time delays to avoid nuisance alarms.
ISSUED: June 5, 2013
REVISED: October 27, 2014
checklist
cAS Message
cAS Warnings with Text Messages
L ENG CHT
R ENG CHT
L FUEL QTY
R FUEL QTY
L ALTR FAIL
R ALTR FAIL
L START ENGD
R START ENGD
GEAR SYS
CHECK GEAR
HTR OVRHEAT
USP ACTIVE
EMERGENcy PROcEDURES
Page
3-21
Left and/or right engine CHT
exceeds 500 °F
3-22
Left or right fuel quantity is less
than 5 GAL
3-26
Left and/or right alternator is
3-27
turned ON and has failed as
determined by voltage regulator
3-41
Left or right engine starter is
engaged for greater than 30
seconds
3-25
Landing
malfunction while on the ground
3-24
Landing gear selector is not
in the down position when
aircraft is less than 400 ft AGL
with MAP less than 14 in Hg
(mutable aural) or flaps greater
than first "notch" (non-mutable
aural).
Landing gear is selected UP
while on the ground.
3-43
Cabin heater has sensed an
overheat condition and has shut
down the heater
3-38c
The autopilot Underspeed
Protection (USP) mode is
actively preventing an under
speed condition.
SEcTION 3
cause*
gear
system
REPORT: VB-2307
3-3

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