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and a DIR TO performed as required. AP/FD must be in HDG mode for the ACTIVATE SEC
F-PLN prompt to be displayed.
• If the crew has not prepared the ALTN FPLN, a selected climb will be initiated. Once
established in climb and clear of terrain, the crew will make a lateral revision at any waypoint to
insert a NEW DEST. The route and a CRZ FL (on PROG page) can be updated as required.
The crew will check the defaulted CRZ FL on PROG page and CI, (consistent with diversion
strategy), on PERF page.
REJECTED LANDING
Applicable to: ALL
A rejected landing is defined as a go-around manoeuvre initiated below the minima.
Once the decision is made to reject the landing, the flight crew must be committed to proceed
with the go-around manoeuvre and not be tempted to retard the thrust levers in a late decision to
complete the landing.
TOGA thrust must be applied but a delayed flap retraction should be considered. If the aircraft is on
the runway when thrust is applied, a CONFIG warning will be generated if the flaps are in CONF full.
The landing gear should be retracted when a positive climb is established with no risk of further touch
down. Climb out as for a standard go-around.
In any case, if reverse thrust has been applied, a full stop landing must be completed.
A330/A340 FLIGHT CREW TRAINING MANUAL
NORMAL OPERATIONS
GO AROUND
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A330/A340 FLEET NO-170 P 4/4
FCTM 17 JUN 09
A330/A340 FLIGHT CREW TRAINING MANUAL
NORMAL OPERATIONS
TAXI IN
A330/A340 FLEET NO-180 P 1/2
FCTM 17 JUN 09
BRAKE TEMPERATURE
Applicable to: ALL
The use of brake fans �� could increase oxidation of the brake surface hot spots if brakes are
not thermally equalized, leading to the rapid degradation of the brakes. For this reason, selection
of brake fans should be delayed until approximately five minutes after touchdown or just prior to
stopping at the gate (whichever occurs first). Selecting brake fans before reaching the gate allows
avoiding blowing carbon brake dust on ground personal.
If there is a significant difference in brake temperature between the wheels of the same gear, when
reaching the gate, this materializes a potential problem with brake e.g. if one wheel reaches the
limit temperature of 600 °C while all others wheels brakes indicate less than 400 °C to 450 °C, this
indicates that there is a potential problem of brake binding or permanent brake application on that
wheel. Conversely, if one wheel brake is at or below 60 °C whereas the others are beyond 200 °C,
this indicates that there is a potential loss of braking on that wheel.
If brake temperature is above 500 °C with fans OFF �� (350 °C fans ON �� ) , use of the parking
brake, unless operationally necessary, should be avoided to prevent brake damage.
The MEL provides information regarding brake ground cooling time, both with and without brake fans
�� .
ENGINES COOLING PERIOD
Applicable to: ALL
To avoid engine thermal stress, it is required that the engine be operated at, or near, idle for a
cooling period as described in FCOM (Refer to FCOM/PRO-NOR-SOP-25-A PARKING - ENG
MASTER ).
TAXI WITH ONE ENGINE SHUTDOWN
Applicable to: , , , , , , , , , , , , , ,
, , , , ,
Refer to NO-040 TAXI WITH ONE ENGINE SHUTDOWN
TAXI WITH TWO ENGINES SHUTDOWN
Applicable to: , , , , , , , , , , , ,
Refer to NO-040 TAXI WITH TWO ENGINES SHUTDOWN
A330/A340 FLIGHT CREW TRAINING MANUAL
NORMAL OPERATIONS
TAXI IN
A330/A340 FLEET NO-180 P 2/2
FCTM 17 JUN 09
AFTER LANDING FLOW PATTERN
Applicable to: ALL
AFTER LANDING FLOW PATTERN
ABNORMAL OPERATIONS
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A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
A330/A340 FLEET AO-PLP-TOC P 1/2
FCTM 17 JUN 09
AO-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
SUMMARY OF HIGHLIGHTS.............................................................................................................................1/2
AO-010 GENERAL
PREFACE............................................................................................................................................................1/6
LANDING DISTANCE PROC..............................................................................................................................1/6
Vapp DETERMINATION..................................................................................................................................... 1/6
IN FLIGHT LANDING DISTANCE CALCULATION FOLLOWING FAILURES..................................................... 4/6
　
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