曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

amber in case of low pressure of blue, green and yellow
hydraulic systems.
TMUFC1202-T04 LEVEL 1
EFFECTIVITY 27-00-00 Page 8
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 68
ALL
ECAM PAGE PRESENTATION
TMUFC1202-P04 LEVEL 1
EFFECTIVITY 27-00-00 Page 9
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 69
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFC1202 LEVEL 1
EFFECTIVITY 27-00-00 Page 10
Jun 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 70
ALL
27 - FLIGHT CONTROLS
27-00-00 PITCH CONTROL NORMAL D/O
CONTENTS:
Side Stick
Elevator Aileron Computer (ELAC)
Spoiler Elevator Computer (SEC)
Flight Management Guidance Computer (FMGC)
Elevators
Trimmable Horizontal Stabilizer (THS)
Trim Wheels
Self Examination
TMUFCT302 LEVEL 3
EFFECTIVITY 27-00-00 Page 1
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 71
ALL
PITCH CONTROL NORMAL D/O
SIDE STICK
The side stick sends electrical orders to the Elevator
Aileron Computers and Spoiler Elevator Computers.
ELEVATOR AILERON COMPUTER (ELAC)
There are 2 ELACs. ELAC 2 normally controls the
elevators and trimmable horizontal stabilizer with
ELAC 1 as a back-up.
In case of ELAC 2 failure, ELAC 1 automatically takes
over.
TMUFCT302-T01 LEVEL 3
EFFECTIVITY 27-00-00 Page 2
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 72
ALL
PITCH CONTROL NORMAL D/O
TMUFCT302-P01 LEVEL 3
EFFECTIVITY 27-00-00 Page 3
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 73
ALL
PITCH CONTROL NORMAL D/O
SPOILER ELEVATOR COMPUTER (SEC)
In case of dual ELAC failure, SEC 1 or 2 automatically
takes over pitch control.
FLIGHT MANAGEMENT and GUIDANCE COMPUTER (FMGC)
When the auto pilot is engaged, the Flight Management
and Guidance Computer sends auto pilot commands to the
ELACs.
ELEVATORS
Each elevator is powered by two actuators, one in
active mode, the other in damping mode with automatic
change over in case of failure.
Both actuators become active in case of large pitch
demands.
The green and yellow actuators are controlled by ELAC
2 and the blue actuators are controlled by ELAC 1.
TRIMMABLE HORIZONTAL STABILIZER (THS)
The trimmable horizontal stabilizer is positioned by
a screw actuator driven by two hydraulic motors which
are controlled by one of three electric motors.
One electrical trim motor is operative at a time and
the other 2 are in stand-by.
Motor 1 is controlled by ELAC 2, motor 2 by ELAC 1 or
SEC 1, motor 3 by SEC 2.
TRIM WHEELS
The Mechanical trim which has priority over the
electrical trim, is operated from the manual trim
wheels.
TMUFCT302-T02 LEVEL 3
EFFECTIVITY 27-00-00 Page 4
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 74
ALL
PITCH CONTROL NORMAL D/O - SPOILER ELEVATOR COMPUTER
TMUFCT302-P02 LEVEL 3
EFFECTIVITY 27-00-00 Page 5
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 75
ALL
SELF EXAMINATION
The Elevator and the THS are normally controlled by
ELAC 2. What happens if ELAC 2 fails ?
A - Pitch control is automatically
transferred to ELAC 1.
B - Pitch control is automatically
transferred to SEC 1 and SEC 2.
C - Pitch control is lost.
TMUFCT302 LEVEL 3
EFFECTIVITY 27-00-00 Page 6
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 76
ALL
27 - FLIGHT CONTROLS
27-90-00 PITCH CONTROL ABNORMAL D/O
CONTENTS:
Alternate Law in Elevator and Aileron Computer (With
Protection)
Alternate Law in Elevator and Aileron Computer (Without
Protection)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 27 FLIGHT CONTROLS(10)