Navigation
FMGC.Failure................................................................................................8.90.1
IRS/ADR.Failures ..........................................................................................8.90.1
Dual.Radio.Altimeter.Failure .........................................................................8.90.2
Power.Plant
All.Engine.Flameout ....................................................................................8.100.1
Tail.Pipe.Fire ...............................................................................................8.100.2
Miscellaneous
Overweight.Landing ....................................................................................8.110.1
Emergency.Descent ....................................................................................8.110.2
Unreliable.Airspeed.Indications...................................................................8.110.2
General
FCTM REV.1.(6.JUN.05)
PREFACE
This chapter highlights techniques to be used in some non-normal operations. Some of the procedures discussed in this chapter are the result of double or triple failures. Whilst it is very unlikely that any of these failures will be encountered, it is useful to have a background understanding of the effect that they have on the handling and management of the aircraft. In all cases, handle the.ECAM.as.described.in.FCTM.Ch.2.
USE.OF.AUTOPILOT
The.use.of.the.autopilot.is.strongly.recommended:
.
In the case of engine failure, without any restriction including autoland or Cat.2/3.ILS.
.
In case of other failures, down to 500 ft AGL in all modes, however the AP has not been certified in all configurations and its performance cannot be guaranteed. If the AP is used in such circumstances, remain vigilant and be prepared to disconnect the AP if the aircraft deviates from the desired or.safe.flight.path.
MONITORING.AND.CROSS-CHECKING
Monitoring and cross-checking are essential components of effective procedures and remain primary tasks for all crew members. The PF shall monitor all ECAM/checklist.actions.
MEMORY.ITEMS
The.following.procedures.are.to.be.applied.from.memory:
.
WINDSHEAR
. WINDSHEAR.AHEAD
. TCAS
.
EGPWS
. LOSS.OF.BRAKING
. EMER.DESCENT.(inital.actions)
. UNRELIABLE.AIRSPEED.INDICATIONS.(initial.actions)
On completion of the memory items and when the aircraft is stabilised on the correct flight path, the PNF shall ensure that all the required memory actions have been carried out by reference to ECAM or checklist, and then complete the remainder.of.the.procedure.
8.10.2
A330/A340 Non-normal.Operations
REV.1.(6.JUN.05)
FCTM General
LANDING.DISTANCE.PROCEDURE
Should a failure occur with a “LDG DIST PROC APPLY” action displayed on the ECAM STATUS page, the pilot should enter the LDG CONF/APP SPD/LDG DIST/CORRECTIONS FOLLOWING FAILURES table in QRH Part 2 to establish:
. The.flap.lever.position.for.landing ..VREF.if.required.for.VAPP.determination . The.landing.distance.factor.for.landing.distance.calculation
VAPP.DETERMINATION
Certain.failures.affect.the.approach.speed:
.
Some failures (typically slat or flap) increase the VLS. In this case, the VLS displayed on the PFD takes into account the actual configuration. VLS.on.the.PERF.APPR.page.is.not.modified.
.
For some other failures, there is a requirement to fly at speed higher than VLS to improve the handling characteristics of the aircraft. In this case, ECAM provides a speed increment, called .VLS, which is displayed on the STATUS page. This speed increment is to be added to the VLS displayed on.the.PFD.when.the.landing.configuration.is.reached.
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