PowerPoint
Airbus A320 simulator flight
Preparation and lecture for DACP screening
Yuuji Izumo Jacklyn Wu
IVAO HKStanding Committee on Aviation Resource and Education
Development
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1
Good morning
Sorry, early
Since many content
My name is Yuuji
Objective
To understand the requirements of the DACP simulator
assessment
To have a basic idea of the Airbus flight control system
To practise the assessment via personal computer flight
simulator
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What we are not going to do
To teach any Standard Operating Procedures
To teach how to fly an airliner
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What we are going to do
Read and interpret the instrument
Watch demonstration
Learn how to handle the aircraft
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Oh good
10 years
I am already know what to do
5
Everyone here will be invited to Cathay City
and fly a real Dragonair A320 Simulator!
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Follow instructions
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Primary Flight Display (PFD)& Navigation Display (ND)
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Sidestick & Steering Hand Wheels(Tiller)
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Rudder & Brake pedal
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Park Brake switch &
Flaps Lever
Mechanical Flight Control Systems
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Fly by wire Flight Control Systems
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Primary Flight Display (PFD)& Navigation Display (ND)
Flight parameters are displayed on
Primary Flight Displays PFD
while navigation data is displayed on Navigation DisplaysND
PFD1
PFD2
ND1
ND2
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ND gives the pilots a visual presentation of where the aircraft
is in relation to Airfields, Navaids, just like a map.
It can also function as an HSI or RMI, under VOR mode or LS
mode.
The yellow icon at the bottom depicts the aircraft while the
green line represents the planned flight path viewed from
above.
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Flight parameters are displayed on
Primary Flight Displays (PFD)
and intergraded few tradition component into one DU
Primary Flight Display
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Time for PFD!
Flight parameters are displayed on Primary Flight Displays (PFD)
and intergraded few tradition component into one DU
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The Artificial Horizon is in MIDDLE
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Indicated Air Speed on the left
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Altimeter tape on the right
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Also the Vertical Speed Indicator
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The Primary Flight display, displays all the normal Primary
Flight indications.
Attitude,
Airspeed,
Altitude,
Vertical Speed,
Heading and Track
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Indicators are laid out in a
classic instrument
T configuration.
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Like what you can see on GAs
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The upper part of the display is known as the
Flight Mode Annunciator (FMA)
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When below 2500 feet above ground, a digital
Radio Altimeter (RA)
is displayed
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Attitude information is shown at the center of the display
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The attitude indicator works in the normal sense
The aircraft is represented by 3 black and yellow symbols which
remain fixed
Just like looking the aircraft from the back
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Center = axle of the plane
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The Sky Pointer moves against a fixed scale to show angle of
bank.
The name is self-explanatory, it always points to the sky.
Sky Pointer
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----- Meeting Notes (16/02/2011 21:31) -----
32
Below the roll index is the Side Slip Index
This index moves to indicate side slip and replaces the balance
indicator(the ball).
Side Slip Index
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In this example the aircraft is in a 20 degree banked turn to
the left with a nose up pitch attitude of 10 degrees
30 degrees
20 degrees
10 degrees
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The attitude indicator works in the normal sense
The aircraft is represented by 3 black and yellow symbols which
remain fixed
Just like looking the aircraft from the back
The compass display is very conventional
The gray 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
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Bottom of PFD, something like ruler
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The small green diamond represents the aircraft track, and it is
normally referred to as the
TRACK DIAMOND
In the example shown the track is 094 degrees which means that
the aircraft has 3 degrees of drift to the right
TRACK 094
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A selected heading may appear either as;
a blue figure, on the appropriate side on the compass scale
or
a blue triangle
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On the FCU there is a Heading selector, with an indicator, that
is linked to the selected heading indication on the PFD compass
Target Heading
Selector and Indicator
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All the indications associated with Altitude are located on the
right hand side of the PFD
CLB
NAV
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The main part of the display is dedicated to the Altimeter. To
the far right is the Vertical Speed display
Altimeter
Vertical Speed
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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
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The vertical speed indication is showing a rate of descent of
800 feet/ minute
Also notice that the target altitude has been set to 9000
feet.
STD
FL 70
30.08
QNH
7000
Target Altitude
Vertical Speed 800ft/min
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The Speed scale moves behind a fixed yellow reference line and
triangle. In the example shown the indicated airspeed is steady at
250 knots
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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 acdeceleration remains constant
Speed Trend Arrow
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Selected Target Airspeed
Manual speed selection is achieved by a rotary selector on the
FCU panel
Speed Selector and Indication
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However, if Autothrust is engaged, you wont need to move the
thrust lever to control the speed.
In the assessment Autothrust is engaged for you.
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Use the tiller to turn.
Be smooth during the turns.
You dont need to touch the sidestick.
Idle thrust is enough for taxy.
Use brakes if necessary.
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For departure, usually CONF 1+F(corresponds to the 1 on the
handle) or 2 used.
The instructor may set the flaps for you.
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The Thrust Lever has several detents. They are:
IDLE
CL(Climb)
FLX/MCT(Flex/Maximum Continuous Thrust)
TOGA(Take Off/Go Around)
Push the Thrust Lever to FLX/MCT detent for take off
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Push the stick forward during the take off roll until 80
knots.(Half stick forward)
Neutral the stick between 80-100 knots.
Keep the plane straight using the rudder pedals.
When you hear Rotate, gently pull the stick. (About 2/3
backstick) On reaching 15 degrees of pitch, follow the Flight
Directors(Green Cross).
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LVR CLB
You will see a flashing LVR CLB(Lever Climb) on the FMA when
passing 1,500 feet.
Pull the Thrust Lever to the CLB(Climb) detent. It is
one-clickbelow the FLX detent.
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160
180
200
250
220
S
240
The aircraft is now above
S speed, and is accelerating, so the flaps can be fully
retracted
Call Flaps zero for flaps retraction.
Target Speed
Minimum Slat retraction speed
S Speed
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THE MOST IMPORTANT PART
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You have control.
I have control.
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Each side stick is fitted with a red Take-over pushbutton.
Autopilot is disconnected if the button is pressed.
Press twice to cancel audible warning
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If both sidesticks are being moved at the same time, the pilot
flying can keep pressing the Take-over pushbutton to gain
control.
The arrow points left showing that the Captain has control.
Avoid moving the sidestick when another pilot is having
control.
Priority left
Dual Input
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When the Flight Director is selected
Flight Director indications are on the attitude indicator
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Notice that there is an indication on the FMA when the Flight
Directors are switched on
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Vertical =
Roll Bar
Horizontal line =
Pitch Bar
Flight Director Roll Bar
Flight Director Pitch bar
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Roll to the right directed
Pitch up directed
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In this example the FD is directing a pitch up and roll to the
right
Once the aircraft has achieved the required pitch and bank the
Flight Director bars will once again be centralised
Now lets look at the airspeed indications on the PFD
Roll to the right directed
Pitch up directed
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Approach and Landing
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The Localizer indicator indicates the aircrafts horizontal
position relative to the centreline of the runway.(Left or
right)
The Glideslope indicator indicates the aircrafts vertical
position relative to a 3 degrees profile to the runway.(High or
Low)
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220
240
260
280
=
o
180
200
220
240
=
o
140
When the aircraft decelerates to Green Dot Speed and below VFE
next, Flap 1 can now be selected.
Note that a target speed of 140 knots has appeared. This
represents the approach speed target
VFE Next
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180
200
220
240
=
o
140
160
180
200
220
=
S
140
Once the flap lever is in position 1, S Speed, VFE Next and the
Flap limit speed indications will appear
The speed will decrease towards S speed
VFE Next
Flap Limit speed, VFE
S Speed
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160
180
200
220
=
S
140
Notice that at S speed the aircraft is below the limit speed for
the next flap setting, VFE Next
Flap 2 can now be selected
VFE Next
S Speed
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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.
Landing gear can lowered, when the aircraft is 2,500 feet
AGL.
VFE Next
Flap Limit speed, VFE
F speed
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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
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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
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140
160
180
200
=
F
120
100
120
140
160
The aircraft will eventually stabilize at Approach speed and the
VFE will be adjusted.
There are indications associated with speed and angle of attack
protections
Protection speeds
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A lot to memorize?
The most important part: FOLLOW the FD
Enjoy the flight
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Contact us
http://ivao.hk
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