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In approach:
When flaps/slats are locked, if the flight
crew does not select the current speed,
the aircraft continues to decelerate down
to a speed that is not consistent with the
real aircraft configuration
Refer to AO-027
ABNORMAL
FLAPS/SLATS
CONFIGURATION
To be continued on next page
A330/A340 FLIGHT CREW TRAINING MANUAL
PREVENTING IDENTIFIED RISKS
PREVENTING IDENTIFIED RISKS
A330/A340 FLEET PIR-010 P 4/4
FCTM 17 JUN 09
Continued from previous page
ATA Risk Consequences Csqce type Refer to FCTM
27/32 In the case of flight
with slats/flaps extended
or landing gear extended,
the flight crew takes
into account the FMS
predictions
Erroneous computation (i.e. time, fuel),
because the FMS does not take into
account the abnormal configuration
Refer to AO-027
ABNORMAL
FLAPS/SLATS
CONFIGURATION
28 The flight crew does not
check fuel before fuel
crossfeed
Fuel loss Refer to AO-028 FUEL
LEAK
34 Error in the use of RMP Loss of transmission to ATC due to
an erroneous manipulation (particularly
when SEL is on)
34 The flight crew performs
the TCAS procedure, but
does not set the FDs to
OFF
The autothrust mode remains in THR
CLB or THR DES, which are not the
appropriate modes. This may lead to
flight control protection activation
Refer to SI-060
OPERATIONAL
RECOMMENDATION
34 The flight crew selects
ADR to OFF using the
ADIRS rotary selector,
instead of the ADR
pushbutton
Irreversible loss of redundancy (the
associated IR is lost, and cannot be
recovered until the end of the flight)
Refer to AO-034
ADR/IRS FAULT
70 In the case of an engine
failure after takeoff, the
flight crew does not
stabilize the aircraft on
the flight path before
performing ECAM actions
Performing the ECAM actions before the
aircraft is stabilized on the flight path,
reduces efficiency due to the PF’s high
workload, and may lead to a trajectory
error
Refer to AO-020
ENGINE FAILURE
AFTER V1
70 In the case of an engine
failure in cruise, the flight
crew presses the EO CLR
key on the MCDU
Pressing the EO CLR key on the MCDU
is an irreversible action that leads to
the loss of single engine computation
(discrepancy between the computation
and real aircraft status)
Refer to AO-020
ENGINE FAILURE
DURING CRUISE
80 For EMERGENCY
DESCENT, the flight crew
turns but does not pull
the knobs, or does both,
but not in the correct
sequence, with no FMA
crosscheck
The flight crew does not detect that
the descent is not engaged. Delayed
descent leads to limited oxygen for
passengers
Refer to OP-030
Autopilot/Flight Director

　
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