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10 s then remains steady.
(10) CHECK EWD message
Is displayed amber on the EWD and on both ND in case of discrepancy between N1, N2,
EGT, FF values on FADEC DMC bus and corresponding displayed information.
(11) White box
Displayed around a parameter when an engine needs specific monitoring i.e. :
Red or amber ‐ line exceedance of any parameter
‐ Engine starting sequence
‐ Engine stopped (in flight).
‐ Reverser unstowed in flight or on ground out of REV mode.
Note: In case of invalidity of any parameter, the associated digital indication is replaced by two
amber crosses. For N1 and EGT parameters, the needle and the box around the digital
display are removed.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 9/16
FCOM 19 AUG 10
SECONDARY PARAMETERS
START CONFIGURATION
(1) Oil quantity indication
The needle and the digital indication are normally green.
The digital indication pulses if the oil quantity drops below 1.8 quarts.
(Also displayed on ECAM CRUISE page).
Advisory is inhibited :
‐ at TO (FLEX or derated) or go around
‐ when reversers are selected
‐ in alpha floor mode
(2) Oil pressure indication
The needle and the digital indication are normally green.
The digital indication pulses if oil pressure exceeds 90 PSI.
The needle and the digital indication are red if the oil pressure drops below 13 PSI.
(3) Oil temperature indication
Normally green
The indication pulses above 140 °C
The indication becomes amber if temperature exceeds :
‐ 140 °C for more than 15 min
‐ or, 155 °C without delay.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 10/16
FCOM 19 AUG 10
(4) Oil filter clog indication
CLOG message appears in amber in case of excessive pressure loss accross the main oil
filter.
Note: This is not an indication that the bypass valve is open.
(5) Fuel used indication
The fuel used value computed by the FADEC is normally displayed in green.
After a transmission interruption by the FADEC, if the displayed value is 100 kg less than
the actual value it is crossed by 2 amber dashes.
It is reset at engine start, on ground.
Also displayed on ECAM CRUISE page.
(6) Fuel filter clog indication
CLOG message appears in amber in case of excessive pressure loss across the fuel filter.
(7) VIB indications
The indication is green.
It pulses above 5.7 units for N1 and 5.6 units for N2.
Also displayed on ECAM CRUISE page.
(8) Ignition indication
IGN is displayed in white during the start sequence.
The selected ignitors ”A” or ”B” or ”AB” are displayed in green when supplied.
Note: When the compressor delivery pressure is high, the igniters are not supplied,
even if IGN is displayed.
(9) Start valve position indication
green : valve fully open
green : valve fully closed.
amber : valve abnormally fully open
amber : valve abnormally fully closed
(10) Engine bleed pressure
Bleed pressure upstream of the precooler is normally displayed in green. It becomes
amber􀀃below􀀃21􀀃PSI􀀃with􀀃N2􀀃≥􀀃10􀀃%􀀃or􀀃in􀀃case􀀃of􀀃overpressure.􀀃
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 11/16
FCOM 19 AUG 10
AFTER START CONFIGURATION
(11) Nacelle temperature indication
Nacelle temperature needles are displayed. Becomes pulsing if the temperature exceeds
240 °C.
The advisory threshold is indicated by a small mark on the arc.
NAC is displayed in white.
All nacelle temperature indications are removed during engine start.
Note: In case of invalidity of any parameter, the associated digital indication is replaced by
two amber crosses.
For OIL QTY, OIL PR and NAC TEMP the needle is removed.
WARNINGS AND CAUTIONS
Applicable to:
E /WD : FAILURE TITLE
conditions AURAL WARNING MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ALL ENG FLAME OUT
Total engine flame out ENG NIL
N1 OVERLIMIT
N1 above 100.3 %
CRC MASTER
WARN NIL
NIL
4, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
　
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