PRIMUS
r
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
Aircraft Door Status
-- The display in figure 4--50, also indicates the
status of the aircraft doors. Closed doors are shown in green. An
open door is indicated by a red DOOR OPEN message. Under
certain conditions, opening a door displays the DOOR OPEN status
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 to 5 quarts
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
Reference T/O Temperature (REF TO TEMP)
-- The pilot can enter
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/O status indicator points to the
selected engine T/O condition. The digits are either cyan or amber.
D
Engine T/O Mode
-- The engine take off mode readout is based on
the logic described in table 4--23.