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TMUFC1405-T03 LEVEL 3
EFFECTIVITY 27-60-00 Page 6
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 202
ALL
TMUFC1405-T03 LEVEL 3
SPEED BRAKE AND GROUND SPOILER DESCRIPTION AND OPERATION - GROUND SPOILER FUNCTION
EFFECTIVITY 27-60-00 Page 7
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 203
ALL
SPEED BRAKE AND GROUND SPOILER DESCRIPTION AND OPERATION
GROUND SPOILER LOGIC
Here are the Ground Spoiler function and Partial Lift
Damping function logics in detail.
The Partial Lift Dumping function is elaborated in the
SECs and activated at reverse selection if only one
main landing gear leg is compressed. Spoilers 1 to 5
are partially deflected in order to lower the second
gear leg on to the ground and consequently to activate
the Ground Spoiler function.
For normal landing (both MLG legs compressed) the
Partial Lift Damping function is masked by the Ground
Spoiler function.
As soon as both Main Landing Gear legs are compressed,
the Ground Spoiler function is activated.
TMUFC1405-T04 LEVEL 3
EFFECTIVITY 27-60-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 204
ALL
TMUFC1405-T04 LEVEL 3
SPEED BRAKE AND GROUND SPOILER DESCRIPTION AND OPERATION - GROUND SPOILER LOGIC
EFFECTIVITY 27-60-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 205
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SPEED BRAKE AND GROUND SPOILER DESCRIPTION AND OPERATION
SELF EXAMINATION
What happens when the sum of roll and speed brake
commands exceeds the maximum possible deflection of
a spoiler ?
A - The speed brake function is inhibited.
B - All spoilers receive an additional
deployment order until one reaches its
maximum possible deflection.
C - The symmetrical surface is retracted
until the difference between the two
surfaces is equal to the roll order.
What are the necessary conditions for ground
spoiler preselection ?
A - Ground spoilers armed and both throttles
at idle or one throttle at reverse and
the other one at not more than idle.
B - Ground spoilers not armed and both
throttles at idle.
C - Both throttles at idle only.
TMUFC1405 LEVEL 3
EFFECTIVITY 27-60-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 206
ALL
27 - FLIGHT CONTROLS
27-00-00 FLIGHT CONTROL WARNINGS
CONTENTS:
Elevator Aileron Computer Pitch Fault
Elevator Aileron Computer Fault
Alternate Law
Aileron Servo Fault
Aileron Fault
Stabilizer Jam
Spoiler Fault
Sidestick Configuration Fault
TMUFC1502 LEVEL 3
EFFECTIVITY 27-00-00 Page 1
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 207
ALL
TMUFC1502-P01 LEVEL 3
FLIGHT CONTROL WARNINGS
EFFECTIVITY 27-00-00 Page 2
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 208
ALL
TMUFC1502-P02 LEVEL 3
FLIGHT CONTROL WARNINGS
EFFECTIVITY 27-00-00 Page 3
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 209
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TMUFC1502 LEVEL 3
EFFECTIVITY 27-00-00 Page 4
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 210
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27 - FLIGHT CONTROLS
27-90-00 EFCS CONTROL INTERFACE
CONTENTS:
Pilot Orders
Flight Control Panels
Hydraulic Pressure
Rudder Pedal Position
Flight Management Guidance Computer
Flight Augmentation Computer
Air Data Inertial Reference System
Landing Gear Control and Interface Unit
Slat and Flap Control Computer
Radio Altimeter
Braking/Steering Control Unit
Wheel Tachometer
Accelerometer
Self Examination
TMUFCLG02 LEVEL 3
EFFECTIVITY 27-90-00 Page 1
May 31/00
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