However, depending on the power source i.e. EDP or RAT, some differences should be outlined:
? Emer Gen powered by the EDP
Significant remaining systems in ELEC EMER CONFIG
FLY PFD1, AP1, Pitch trim, rudder trim, alternate law
NAVIGATE ND1, FMGC1, radar, RMP1, VOR1, DME1, (ILS1, GPS1 if MMR installed)
COMMUNICATE VHF1 and HF1
Note: When the failure occurs, the AP, if engaged, will disengage. AP1 can be reengaged. Approach specificities:
When LAND RECOVERY is set ON:
‐ ILS1 (if MMR not installed) and SFCC slat flap channel are recovered ‐ Direct law when landing gear extended
‐ Landing is performed with pedal braking and Anti skid
? Emer Gen powered by the RAT
Significant remaining systems in ELEC EMER CONFIG
FLY PFD1, Alternate law
NAVIGATE RMP1, VOR1, (ILS1, GPS1 if MMR installed)
COMMUNICATE VHF1
Note: The AP, pitch trim and rudder trim are not available. The aircraft will be out of trim in roll due to right outboard aileron upfloat and it is necessary to pay close attention to bank angle and heading.
Approach specificities:
When LAND RECOVERY is set ON:
‐ ILS1 (if MMR not installed) and SFCC slat channel are recovered
‐ At slat extension, the emergency generator disconnects (in order to dedicate the RAT for flight controls) and landing is performed on Batteries with the same loads.
‐ Direct law when landing gear extended
‐ Landing is performed with pedal braking without Anti skid
RESTORATION FROM EMER ELEC
Applicable to: ALL
When ELEC EMER CONFIG occurs, the LAND RECOVERY AC and DC BUS bars are initially shed and will remain shed until the LAND REC pb is selected ON. This remains true if normal electrical configuration is restored. This is the reason why the crew will also select LAND REC pb ON for approach following a restoration from an ELEC EMER CONFIG.
ABNORMAL OPERATIONS
ELECTRICAL
Intentionally left blank
ABNORMAL OPERATIONS
FIRE PROTECTION
PREFACE
Applicable to: ALL
Fire and/or smoke in the fuselage present the crew with potentially difficult situations. Not only will they have to deal with the emergency itself but also the passengers are likely to panic should they become aware of the situation. It is essential therefore, that action to control the source of combustion is not delayed.
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本文鏈接地址：A330/A340 機組訓練手冊 FCTM Flight Crew Training Manual 2(32)
