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EFIS on Airbus A320 / A330
Preparation for the upcoming jumpseat flight
Yuuji Izumo Gilbert Lee Jacklyn Wu
CARE - Charity for Aviation - Recreation and Education
CARE –
Charity for Aviation Recreation and Education
Collaborated with
Hong Kong Air Cadet Corps
+
Sea Cadets
+
Scout Association of Hong
Kong
to provide different aviation
knowledge courses since
2009
CARE –
Charity for Aviation Recreation and Education
We also visited and established a
connection with the UK based
Anglian Flight Centres in 2015
Outstanding students who
completed the 60-week-course at
CARE will be recommended to
Anglian Flight Centres
for participating self-funded private
pilot programme
Electronic Flight Information
System
Primary Flight Display (PFD)
&
Navigation Display (ND)
Flight parameters are displayed on
Primary Flight Displays (PFD)
while navigation data is displayed on
Navigation Displays(ND)
PFD1 PFD2ND1 ND2
PFD1 ND1
ND has several modes
In ARC mode,
• Aircraft Position
• Navaids
• Airfields
• TCAS(Traffic
information)
Other modes include
• ROSE VOR
• ROSE LS
• PLAN
ND has several modes
In ARC mode,
• Aircraft Position
• Navaids
• Airfields
• TCAS(Traffic
information)
Other modes include
• ROSE VOR
• ROSE LS
• PLAN
ND has several modes
In ARC mode,
• Aircraft Position
• Navaids
• Airfields
• TCAS
Other modes include
• ROSE VOR
• ROSE LS
• PLAN
Planned Route
Aircraft
Weather Radar
(WXR)
Aircraft
MCDUs
Multipurpose Control
and Display Units
are the MMI of
FMGS
Flight Management and
Guidance System
Pushback Red
Pushback Blue
Pushback Green
Primary Flight Display
Artificial Horizon
Indicated Air Speed
Altimeter
Vertical Speed Indicator
•Attitude,
•Airspeed,
•Altitude,
•Vertical Speed,
•Heading and Track
Classic
instrument
“T”
configuration
Flight Mode
Annunciator
(FMA)
Announce FMA
“MAN FLEX 55,
SRS, RUNWAY,
AUTO THRUST
BLUE”
In the middle of the glare shield, there is a Flight Control
Unit
The FCU is one of the interface units between the pilots
and the Autoflight system
There are selectors on the FCU which will affect the
indications seen on the PFD and ND
The selectors, with associated indication, are
provided for:
• Speed,
• Heading,
• Altitude.
You will see how these selectors affect the EFIS
displays in the modules that follow.
SPEED HEADING ALTITUDE
Radio Altimeter
(RA)
• Activated below
2500 feet above
ground
The fixed black and yellow
symbols represents the
aircraft
Read attitude information:
• Imagine looking the aircraft
from the back
• Sky is BLUE
• Ground is BROWN
The Sky Pointer
Moves to show angle of
bank
Always points to the sky
Sky Pointer
Indicates side slip
Replaces the balance
indicator(the ball)
Side Slip
Index
30 degrees
20 degrees
10 degrees
The fixed black and yellow
symbols represents the
aircraft
The fixed black and yellow
symbols represents the
aircraft
The gray compass scale
moves against a fixed
yellow line which
represents the centerline of
the aircraft
In the example shown the
aircraft is heading 091
degrees
HEADING 091
TRACK DIAMOND
Small green diamond
represents the aircraft track
In the example shown the
track is 094 degrees which
means that the aircraft has 3
degrees of drift to the right
TRACK 094
The main part of the
display is dedicated to the
Altimeter. To the far right
is the Vertical Speed
display
Altimeter Vertical Speed
STD
FL 70
In the final stage of
an approach the
ground reference
ribbon will reappear
along with a landing
elevation line
30.08
QNH
Ground Reference Ribbon
Landing Elevation Line
The Speed scale moves behind a fixed yellow reference
line and triangle. In the example shown the indicated
airspeed is steady at 250 knots
When the aircraft is
accelerating, or
decelerating a
Speed Trend Arrow
appears
This arrow shows
the value that will be
attained in 10
seconds if the ac(de)
celeration remains
constant
Speed Trend Arrow
However, if Auto
Thrust is engaged,
you won’t need to
move the thrust lever
to control the speed
In the assessment
Auto Thrust is
engaged for you.
Localiser indicator
indicates the aircraft’s
horizontal position
relative to the
centreline of the
runway
Glideslope indicator
indicates the aircraft’s
vertical position
relative to a 3 degrees
profile to the runway
160
180
200
220
=
S
140
160
180
200
220
=
F
140
As soon as the flap lever
is in position 2 , S Speed is
removed
F Speed, and a new VFE
Next indications will
appear. The Flap limit
speed will move to a new
limit
VFE Next
Flap Limit speed, VFE
F speed
160
180
200
220
=
F
140
Notice that the approach speed
target, V Approach, has now
appeared as a magenta triangle
The aircraft will continue
decelerating towards F speed
By reducing towards F speed
the aircraft will be below the VFE
for the next flap setting
Flap 3 can now be set
VFE Next
Flap Limit speed, VFE
V Approach Speed
160
180
200
220
=
F
140
140
160
180
200
=
F
120
As before VFE
Next and VFE move
to reflect the new
flap position
Flap full can now
be selected
VFE Next
Flap Limit speed, VFE
140
160
180
200
=
F
120
100
120
140
160
The aircraft
will eventually
stabilise at
Approach
speed
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EFIS on Airbus A320 / A330