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UF94200
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CONTROL LAW PRESENTATION - DIRECT LAW - BASIC PRINCIPLE
TMUFCBC01-P07 LEVEL 1
EFFECTIVITY 27-90-00 Page 15
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 39
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CONTROL LAW PRESENTATION
MECHANICAL BACK-UP
The mechanical back-up permits the aircraft to be
controlled during a temporary complete loss of
electrical power or flight controls computers.
The longitudinal control is achieved using the trim
wheels as the elevators are kept at zero deflection.
The lateral control is achieved from pedals.
TMUFCBC01-T08 LEVEL 1
EFFECTIVITY 27-90-00 Page 16
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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CONTROL LAW PRESENTATION - MECHANICAL BACK-UP
TMUFCBC01-P08 LEVEL 1
EFFECTIVITY 27-90-00 Page 17
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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SELF EXAMINATION
In normal conditions, what are the active
protections in flare mode?
A - Bank angle and stall protections.
B - Bank angle and high speed protections.
C - Stall protection only.
What are the active protections in direct law?
A - Stall protection only.
B - No protection.
C - High speed protection.
TMUFCBC01 LEVEL 1
EFFECTIVITY 27-90-00 Page 18
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 42
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27 - FLIGHT CONTROLS
27-00-00 SIDE STICK OPERATION AND
PRIORITY INDICATION
CONTENTS:
Introduction
Priority Logic
Autopilot Disconnection
Self Examination
TMUFC1103 LEVEL 1
EFFECTIVITY 27-00-00 Page 1
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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SIDE STICK OPERATION AND PRIORITY INDICATION
INTRODUCTION
The Captain and the First Officer side stick assemblies
are similar. Their ergonomic characteristics are
adapted for use with the left hand at the Captain’s
station and with the right hand at the First Officer’s
station.
When a side stick is not used, it is springloaded to
neutral position.
TMUFC1103-T01 LEVEL 1
EFFECTIVITY 27-00-00 Page 2
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 44
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SIDE STICK OPERATION AND PRIORITY INDICATION - INTRODUCTION
TMUFC1103-P01 LEVEL 1
EFFECTIVITY 27-00-00 Page 3
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 45
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SIDE STICK OPERATION AND PRIORITY INDICATION
PRIORITY LOGIC
This logic is achieved in the Flight Control Computers
(Elevator Aileron Computers and Spoiler Elevator
Computers).
The CAPT side stick is moved first.
When a side stick is moved, an electrical signal
related to its angle deflection is sent to the system
computers.
TMUFC1103-T02 LEVEL 1
EFFECTIVITY 27-00-00 Page 4
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 46
ALL
SIDE STICK OPERATION AND PRIORITY INDICATION - PRIORITY LOGIC
TMUFC1103-P02 LEVEL 1
EFFECTIVITY 27-00-00 Page 5
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 47
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SIDE STICK OPERATION AND PRIORITY INDICATION
PRIORITY LOGIC
When both side sticks are deflected with no action on
any priority switch, the two green priority lights
(CAPT and F/O) flash and the aural indication "DUAL
INPUT" is generated every 5 seconds, as long as both
side sticks remain deflected.
When both side sticks are moved in the same direction,
the signals are algebrically added. The sum is limited
to the surface maximum deflection.
TMUFC1103-T03 LEVEL 1
EFFECTIVITY 27-00-00 Page 6
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 48
　
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