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

drifting parameter.
Flight phase mode: automatic presentation due to the
A/C situation.
TMUEIAE04-T04 LEVEL 1
EFFECTIVITY 31-67-00 Page 8
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 64
ALL
EIS: SYSTEM DISPLAY PRESENTATION - PERMANENT DATA
TMUEIAE04-P04 LEVEL 1
EFFECTIVITY 31-67-00 Page 9
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 65
ALL
LEFT INTENTIONALLY BLANK
TMUEIAE04 LEVEL 1
EFFECTIVITY 31-67-00 Page 10
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 66
ALL
31 - INDICATING/RECORDING SYSTEMS
31-67-00 EIS: ECAM FLIGHT DISPLAYS
CONTENTS:
General
Flight Phase 1
Flight Phase 2
Flight Phase 3, 4, 5
Flight Phase 6
Flight Phase 7
Flight Phase 8
Flight Phase 9
Flight Phase 10
Self Examination
TMUEISI01 LEVEL 1
EFFECTIVITY 31-67-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 67
ALL
EIS: ECAM FLIGHT DISPLAYS
In this module, parameters are given for a CFM engine
(For an IAE engine, EPR replaces N1).
Values are given using the metric system.
The AIRCOND and the DOOR/OXY pages are given as an
example.
This may be different to your aircraft configuration.
GENERAL
A manual page call can replace the current display at
any time. The APU or ENGINE system pages are displayed
in priority if they are started. They remain displayed
10 seconds after APU AVAIL or at the end of ENG START.
FLIGHT PHASE 1: DOOR/OXY PAGE
The APU page appears during the APU start sequence and
it will be replaced by the DOOR/OXY page 10 seconds
after the APU start sequence.
The ENG page appears during the Engine start sequence
and it will be replaced by the WHEEL page after the
Engine start sequence.
The flight phases are computed by the FWCs.
TMUEISI01-T01 LEVEL 1
EFFECTIVITY 31-67-00 Page 2
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 68
ALL
EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 1: DOOR OXY PAGE
TMUEISI01-P01 LEVEL 1
EFFECTIVITY 31-67-00 Page 3
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 69
ALL
EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 2: WHEEL PAGE
The WHEEL page is displayed only when engine start has
been completed. The FLT/CTL page replaces WHEEL page
for 20 seconds when either sidestick is moved or when
rudder deflection is above 22 degrees.
TMUEISI01-T02 LEVEL 1
EFFECTIVITY 31-67-00 Page 4
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 70
ALL
TMUEISI01-P02 LEVEL 1
EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 2: WHEEL PAGE
EFFECTIVITY 31-67-00 Page 5
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 71
ALL
EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 3,4,5: ENGINE PAGE
During this phase, most warnings are inhibited.
T.O INHIBIT is displayed on the E/W display.
TMUEISI01-T03 LEVEL 1
EFFECTIVITY 31-67-00 Page 6
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 72
ALL
EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 3,4,5: ENGINE PAGE
TMUEISI01-P03 LEVEL 1
EFFECTIVITY 31-67-00 Page 7
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 73
ALL
EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 6: CRUISE PAGE
The CRUISE page is displayed in flight.
It contains both ENGINE and AIR information.
The CRUISE page appears as soon as SLATS are in and
the engines are no longer at take-off power. It
disappears when the L/G is selected down (WHEEL page
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 31 INDICATING AND RECORDING SYSTEM(9)