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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, DME 1, (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
REMAINING SYSTEMS
Criteria: 330-200
3 Applicable to: , , , , , , , ,
4 The electrical distribution has been designed to fly, navigate, communicate and ensure passengers
comfort.
A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
ELECTRICAL
A330/A340 FLEET AO-024 P 4/6
FCTM 17 JUN 09
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
REMAINING SYSTEMS
Criteria: 340-300
Applicable to: , , , , , , , , , , , ,
5 The electrical distribution has been designed to fly, navigate, communicate and ensure passengers
comfort.
A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
ELECTRICAL
A330/A340 FLEET AO-024 P 5/6
FCTM 17 JUN 09
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, Pitch trim, rudder trim, alternate law
NAVIGATE MCDU1 (B/U NAV), RMP1, VOR1, (ILS1, GPS1 if MMR installed)
COMMUNICATE VHF1
Note: The AP is not available. The rudder trim position indicator on centre pedestal is lost 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 flap channel are recovered
‐ Direct law when landing gear extended
‐ Landing is performed with pedal braking without 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
‐ Direct law when landing gear extended
　
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