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

positions.
Rudder pedals override disconnects the autopilot.
TMUFGCH01-T03 LEVEL 1
EFFECTIVITY 22-00-00 Page 6
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 46
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING - THRUST LEVERS, SIDE STICKS & RUDDER PEDALS
TMUFGCH01-P03 LEVEL 1
EFFECTIVITY 22-00-00 Page 7
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 47
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING
RESETS
The FMGC, FAC, FCU and MCDU resets are possible in the
cockpit.
Depending on the computer (1 or 2), the circuit
breakers are located either on the overhead circuit
breakers panel 49VU or on the rear circuit breakers
panel 121VU.
TMUFGCH01-T04 LEVEL 1
EFFECTIVITY 22-00-00 Page 8
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 48
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING - RESETS
TMUFGCH01-P04 LEVEL 1
EFFECTIVITY 22-00-00 Page 9
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 49
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING
RMPs
The Radio Management Panels (RMPs) are located on the
center pedestal near Multipurpose Control and Display
Units 1 and 2.
The RMPS are used for navaid standby selection.
EWD/SD
The Engine/Warning Display (EWD) and the System Display
(SD) are located on the main instrument panel.
The EWD displays AFS warning messages.
The SD displays AFS information such as inoperative
systems on the STATUS page or landing capabilities
availability.
TMUFGCH01-T05 LEVEL 1
EFFECTIVITY 22-00-00 Page 10
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 50
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING - RMPs & EWD/SD
TMUFGCH01-P05 LEVEL 1
EFFECTIVITY 22-00-00 Page 11
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 51
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING
ATTENTION GETTERS
The attention getters are located on the glareshield
panel on the Capt and F/O sides.
The MASTER CAUTION and/or the MASTER WARNING are
activated when an AFS disconnection occurs.
The AUTOLAND warning is activated when a problem occurs
during final approach in automatic landing.
TMUFGCH01-T06 LEVEL 1
EFFECTIVITY 22-00-00 Page 12
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 52
ALL
AUTO FLIGHT SYSTEM CONTROL AND INDICATING - ATTENTION GETTERS
TMUFGCH01-P06 LEVEL 1
EFFECTIVITY 22-00-00 Page 13
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 53
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFGCH01 LEVEL 1
EFFECTIVITY 22-00-00 Page 14
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 54
ALL
22 - AUTO FLIGHT SYSTEM
22-00-00 BASIC OPERATIONAL PRINCIPLES
CONTENTS:
General
Data Base Loading
Power-up Test FD Engagement
MCDU Initialization
A/THR Engagement
AP Engagement
Self Examination
TMUFGCQ01 LEVEL 1
EFFECTIVITY 22-00-00 Page 1
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 55
ALL
BASIC OPERATIONAL PRINCIPLES
GENERAL
This sequence describes the operational use of the
Flight Management and Guidance Computers (FMGCs) in a
normal operation with a total availability of the
concerned functions.
The short-term pilot orders are entered through the
Flight Control Unit (FCU). The long-term pilot orders
are entered through the Multipurpose Control and
Display Unit (MCDU).
Four key-words for the control principle and both types
of guidance are to be kept in mind in order to avoid
handling errors.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 22 AUTO FLIGHT SYSTEM(12)