dragonair certificate programme 2016 efis
TRANSCRIPT
PowerPoint
Airbus A320/A330 EFISPreparation for DACP Airbus Simulator Flying
Yuuji Izumo Jacklyn Wu Gilbert LeeCARE - Charity for Aviation - Recreation and Education
1Good morning Sorry, earlySince many content My name is Yuuji
ObjectiveTo prepare for the DACP simulator flyingTo revise the EFIS on modern jet liners
The simulator
Follow instructions
Primary Flight Display (PFD)& Navigation Display (ND)
Sidestick & Steering Hand Wheels(Tiller)
Rudder & Brake pedal
Thrust Levers
Overhead panel
Park Brake switch &Flaps Lever
Mechanical Flight Control Systems
Fly by wire Flight Control Systems
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
ND has several modes. In ARC mode,Aircraft PositionNavaidsAirfieldsTCAS(Traffic information)Other modes includeROSE VORROSE LSPLAN
Planned Route
Aircraft
Primary Flight Display
Time for PFD! Flight parameters are displayed on Primary Flight Displays (PFD) and intergraded few tradition component into one DU
16
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)
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 backSky is BLUEGround is BROWN
Center = axle of the plane26
The Sky Pointer Moves to show angle of bankAlways points to the sky
Sky Pointer
----- Meeting Notes (16/02/2011 21:31) -----
27
Indicates side slip Replaces the balance indicator(the ball)
Side Slip Index
30 degrees20 degrees10 degrees
The fixed black and yellow symbols represents the aircraft
Read attitude information:Imagine looking the aircraft from the backBlue is skyBrown is ground
The fixed black and yellow symbols represents the aircraft
Read attitude information:Imagine looking the aircraft from the backSky is BLUEGround is BROWN
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
Bottom of PFD, something like ruler 32
TRACK DIAMONDSmall 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
33
A selected heading may appear either as;
a blue figure, on the appropriate side on the compass scale or
a blue triangle
On the FCU there is a Heading selector, with an indicator, that is linked to the selected heading indication on the PFD compass
Target HeadingSelector and Indicator
All the indications associated with Altitude are located on the right hand side of the PFD
CLBNAV
The main part of the display is dedicated to the Altimeter. To the far right is the Vertical Speed display
AltimeterVertical Speed
STD
FL 70
In the final stage of an approach the ground reference ribbon will reappear along with a landing elevation line
30.08QNH
Ground Reference RibbonLanding Elevation Line
The vertical speed indication is showing a rate of descent of 800 feet/ minute
Also note that the target altitude has been set to 9000 feet.
STD
FL 70
30.08QNH7000
Target Altitude
Vertical Speed -800ft/min
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 acdeceleration remains constant
Speed Trend Arrow
Selected Target Airspeed
Manual speed selection is achieved by a rotary selector on the FCU panel
Speed Selector and Indication
However, if Autothrust is engaged, you wont need to move the thrust lever to control the speed.
The Flying
Taxy
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.
Take off
For departure, usually CONF 1+F(corresponds to the 1 on the handle) or 2 used.The instructor may set the flaps for you.
The Thrust Lever has several detents. They are:IDLECL(Climb)FLX/MCT(Flex/Maximum Continuous Thrust)TOGA(Take Off/Go Around)Push the Thrust Lever to FLX/MCT detent for take off
Announce Take OffHalf stick forward until 80 knots
Announce FMAMAN FLEX 55, SRS, RUNWAY, AUTO THRUST BLUE
Neutralize the stick
100 KnotsAnnounce Checked
100 KnotsChecked
V1RotatePull stick back to about 2/3About 3 degrees per secondAim at 15 degrees nose up, then follow FDRotate
Positive ClimbAnnounce Gear upPositive ClimbGear up
LVR CLB
Passing 1,500 feet,LVR CLB(Lever Climb) will flaxh on the FMA. Pull the Thrust Lever to the CLB(Climb) detent. It is one-clickbelow the FLX detent.
160180200250
220
S
240
Above S speed, and accelerating, CallFlaps Zero for flaps retraction.
Target Speed
Minimum Slat retraction speedS Speed
THE MOST IMPORTANT PART
You have control.I have control.
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
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
When the Flight Director is selected
Flight Director indications are on the attitude indicator
Notice that there is an indication on the FMA when the Flight Directors are switched on
Vertical = Roll Bar
Horizontal line =Pitch Bar
Flight Director Roll Bar
Flight Director Pitch bar
Roll to the right directed Pitch up directed
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 centred Roll to the right directed Pitch up directed
Approach and Landing
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)
220240260280
=o
180200220240=o140
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
180200220240=o140
160180200220=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 speedVFE Next
Flap Limit speed, VFE
S Speed
160180200220=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 selectedVFE Next
S Speed
160180200220=S
140
160180200220=
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
160180200220=
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
160180200220=
F
140
140160180200=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
140160180200=F
120
100120140160
The aircraft will eventually stabilize at Approach speed
A lot to memorize?The most important part: FOLLOW the FDEnjoy the flight
Seat Adjustment
Forward/Backward
Upward/Downward
Seat Adjustment
Height
Pitch
Pedal Adjustment
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