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same or opposite direction?
A - The surface movement is proportional to
the algebraic sum of the deflection of
both side sticks.
B - The surface movement is proportional to
the movement of the last side stick
deflected.
C - The surface movement is proportional to
the movement of the first side stick
deflected.
How is it possible to inhibit the output of the
other side stick?
A - By pulling harder than the other pilot.
B - By pressing in the take over pushbutton.
C - The captain is always right.
What happens if the take over pushbutton of one
side stick is pressed in for more than 40 seconds?
A - The other side stick remains deactivated
after the take over pushbutton is
released.
B - The other side stick remains activated
after the take over pushbutton is
released.
C - Both side sticks are deactivated.
How can a deactivated side stick be reactivated?
A - By a momentary action on the take over
pushbutton of any side stick.
B - By pulling the deactivated side stick
harder than the other pilot.
C - By a simultaneous action on both take
over pushbuttons.
TMUFC1103 LEVEL 1
EFFECTIVITY 27-00-00 Page 18
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 60
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27 - FLIGHT CONTROLS
27-00-00 ECAM PAGE PRESENTATION
CONTENTS:
Spoiler / Speed Brake
Hydraulic System Pressure
ELAC / SEC
Aileron / Roll Spoilers
Ground Spoilers
Elevator Position
Pitch Trim Position
Rudder Position
TMUFC1202 LEVEL 1
EFFECTIVITY 27-00-00 Page 1
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 61
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ECAM PAGE PRESENTATION
SPOILER / SPEED BRAKE
Each spoiler and speed brake indication is green when
the surface is operative and amber when inoperative.
HYDRAULIC SYSTEM PRESSURE
The hydraulic system pressure indication is normally
green and becomes amber in case of low pressure.
ELAC / SEC
The Elevator Aileron Computer (ELAC) and Spoiler
Elevator Computer (SEC) reference numbers are normally
green and become amber in case of failure.
AILERON / ROLL SPOILERS
The aileron position is indicated by a green index on
a white scale.
They become amber if both actuators are inoperative.
TMUFC1202-T01 LEVEL 1
EFFECTIVITY 27-00-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 62
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ECAM PAGE PRESENTATION
TMUFC1202-P01 LEVEL 1
EFFECTIVITY 27-00-00 Page 3
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 63
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ECAM PAGE PRESENTATION
GROUND SPOILERS
At landing, the WHEEL page appears automatically on
the lower ECAM and shows the ground spoilers status.
TMUFC1202-T02 LEVEL 1
EFFECTIVITY 27-00-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 64
ALL
ECAM PAGE PRESENTATION
TMUFC1202-P02 LEVEL 1
EFFECTIVITY 27-00-00 Page 5
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 65
ALL
ECAM PAGE PRESENTATION
ELEVATOR POSITION
The elevator position is indicated by a green index
on a white scale. They become amber if both actuators
are inoperative.
PITCH TRIM POSITION
The normally green pitch trim position indication
becomes amber in case of green and yellow hydraulic
system low pressure.
The PITCH TRIM inscription is normally white. It
becomes amber in case of Trimmable Horizontal
Stabilizer jam.
TMUFC1202-T03 LEVEL 1
EFFECTIVITY 27-00-00 Page 6
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 66
ALL
ECAM PAGE PRESENTATION
TMUFC1202-P03 LEVEL 1
EFFECTIVITY 27-00-00 Page 7
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 67
ALL
ECAM PAGE PRESENTATION
RUDDER POSITION
The normally green rudder position indication becomes
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