PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-87
Electronic Flight Instrument System (EFIS)
AD--50947--R1@
AIRCRAFT DOOR
STATUS
ENGINE T/O
STATUS ARROW
ENGINE T/O DATA
TEMPERATURE
ENTRY
ENGINE OIL LEVEL
ANTI--ICE STATUS
ANNUNCIATION
Takeoff Display
Figure 4--50
D AircraftDoorStatus--Thedisplayinfigure4--50,alsoindicatesthe
status of the aircraft doors. Closed doors are shown in green. An
open door is indicated by a red DOOR OPEN message. Under
certainconditions,openingadoordisplaystheDOOROPENstatus
message boxed and flashing for 5 seconds.
D Engine Oil Level -- The oil quantity for each engine is shown.
Normally, the quantity is green. When the quantity drops to5quarts
and below, the digits are boxed and displayed in amber. Once the
aircraft is airborne, the oil level is removed.
D Anti--Ice (REF A--ICE) Status Annunciation -- The REF A--ICE
indicates the current state of the bleed air anti--ice system. The
annunciation indicates either ON or OFF.
D ReferenceT/OTemperature(REFTOTEMP)--Thepilot canenter
a reference temperature for the engine FADEC to use for takeoff
power calculation. This input can be normal or flexible T/O power.
The pilot can also select engine anti--ice for T/O. Depending on the
combination of entries, the engine T/Ostatus indicator points tothe
selected engine T/O condition. The digits are either cyan or amber.
D Engine T/O Mode --The engine take off mode readoutis basedon
the logic described in table 4--23.
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