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back).
The T.O inhibit message disappears.
The CRUISE page is also displayed on ground when an
ANN LT TEST is performed.
TMUEISI01-T04 LEVEL 1
EFFECTIVITY 31-67-00 Page 8
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 6: CRUISE PAGE
TMUEISI01-P04 LEVEL 1
EFFECTIVITY 31-67-00 Page 9
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 7: WHEEL PAGE
During this phase, most warnings are inhibited. LDG
INHIBIT is displayed on the E/W display.
TMUEISI01-T05 LEVEL 1
EFFECTIVITY 31-67-00 Page 10
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
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EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 7: WHEEL PAGE
TMUEISI01-P05 LEVEL 1
EFFECTIVITY 31-67-00 Page 11
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 77
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EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 8: WHEEL PAGE
During this phase, most warnings are inhibited. LDG
INHIBIT is displayed on the E/W display.
NOTE: Ground spoilers are displayed extended only
after touch down.
TMUEISI01-T06 LEVEL 1
EFFECTIVITY 31-67-00 Page 12
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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ALL
EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 8: WHEEL PAGE
TMUEISI01-P06 LEVEL 1
EFFECTIVITY 31-67-00 Page 13
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 79
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EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 9: WHEEL PAGE
The LDG INHIBIT message disappears.
TMUEISI01-T07 LEVEL 1
EFFECTIVITY 31-67-00 Page 14
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 9: WHEEL PAGE
TMUEISI01-P07 LEVEL 1
EFFECTIVITY 31-67-00 Page 15
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 81
ALL
EIS: ECAM FLIGHT DISPLAYS
FLIGHT PHASE 10: DOOR PAGE
5 minutes after 2nd engine shutdown, the FWC starts a
new flight leg in phase 1.
TMUEISI01-T08 LEVEL 1
EFFECTIVITY 31-67-00 Page 16
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 82
ALL
EIS: ECAM FLIGHT DISPLAYS - FLIGHT PHASE 10: DOOR PAGE
TMUEISI01-P08 LEVEL 1
EFFECTIVITY 31-67-00 Page 17
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UF94200
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SELF EXAMINATION
Which ECAM page is displayed in cruise?
A - ENGINE page.
B - FLT/CTL page.
C - CRUISE page.
Which ECAM page is displayed when the landing gear
is selected down in phase 6?
A - WHEEL page.
B - CRUISE page.
C - FLT/CTL page.
TMUEISI01 LEVEL 1
EFFECTIVITY 31-67-00 Page 18
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 84
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31 - INDICATING/RECORDING SYSTEMS
31-56-00 EIS: ECAM CONTROL PANEL
UTILIZATION
CONTENTS:
OFF/BRT Knobs
TO CONFIG
EMER CANC
ALL
CLR
RCL
STS
ENGINE System Page
BLEED System Page
PRESS System Page
ELEC System Page
HYD System Page
FUEL System Page
APU System Page
COND System Page
DOOR/OXY System Page
WHEEL System Page
F/CTL System Page
TMUEISD01 LEVEL 1
EFFECTIVITY 31-56-00 Page 1
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 85
　
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