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UF94200
EFFECTIVITY Page 29
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EIS: ECAM AUDIO SIGNALS
DESCRIPTION
This table presents the audio signals with their
meaning.
For those which are continuous, the way to cancel them
(in addition to the EMERgency CANCel pushbutton on the
ECAM control panel) is also indicated.
RADIO HEIGHT CALL OUTS
Automatic radio height call outs (Synthetic voice;
example: "FOUR HUNDRED") are generated according to
aircraft wiring and airline selection from the standard
list.
Audio call out "HUNDRED ABOVE" is given when aircraft
radio height falls to selected Decision Height (DH) +
100 feet.
Audio call out "MINIMUM" is given when aircraft radio
height falls to selected DH.
ENHANCED GROUND PROXIMITY WARNINGS
The Enhanced Ground Proximity Warning System (EGPWS)
generates aural warnings (Synthetic voice) under 5
modes:
- Mode 1: Excessive rate of descent.
- Mode 2: Excessive terrain closure rate.
- Mode 3: Descent after take-off and
minimum terrain clearance.
- Mode 4: Unsafe terrain clearance.
- Mode 5: Descent below glide slope.
The Enhanced functions are:
- TAD: Terrain Awarness and Display
- TCF: Terrain Clearance Floor
For example, in mode 3, the generated aural warning
is "DON’T SINK".
TMUEISL02-T01 LEVEL 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM AUDIO SIGNALS
TMUEISL02-P01 LEVEL 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUEISL02 LEVEL 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
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31 - INDICATING/RECORDING SYSTEMS
31-60-00 EIS: ECAM DISPLAYS
CONTENTS:
Engine and Warning Display
System and Status Display
TMUEIS101 LEVEL 1
EFFECTIVITY 31-60-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM 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.
This may be different to your aircraft configuration.
ENGINE AND WARNING DISPLAY
The upper part of the engine warning display is
dedicated to the engine control parameters.
On the right part of the engine warning display, the
fuel on board is indicated.
A word, a number and a specific symbol indicate the
slats and flaps position.
On the lower part of the engine warning display, the
memo messages present the aircraft systems or functions
temporarily selected.
TMUEIS101-T01 LEVEL 1
EFFECTIVITY 31-60-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM DISPLAYS - ENGINE AND WARNING DISPLAY
TMUEIS101-P01 LEVEL 1
EFFECTIVITY 31-60-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM DISPLAYS
ENGINE AND WARNING DISPLAY (CONTINUED)
Normal check lists like take off or landing are
displayed.
TMUEIS101-T02 LEVEL 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
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EIS: ECAM DISPLAYS - ENGINE AND WARNING DISPLAY (CONTINUED)
TMUEIS101-P02 LEVEL 1
EFFECTIVITY 31-60-00 Page 5
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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EIS: ECAM DISPLAYS
ENGINE AND WARNING DISPLAY (CONTINUED)
As soon as a failure is detected, a special message
is displayed which has priority on the memo page.
NOTE: An overflow arrow appears when the warning or
caution message text exceeds the capacity of the
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