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3 F 6.5/82.5 6.5/80.1 6.5/75.4 6.5/68.1
(1) Due to the fact that the speed is unreliable, the SFCC may select the 1+F configuration in approach, instead of 1.
FINAL APPROACH AT STANDARD - 3 ° DESCENT FLIGHT PATH
LANDING GEAR DOWN
Above 265 t 265 t - 230 t 230 t - 200 t Below 200 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
3 VLS +10 4/62.7 4/60.7 4/56.9 3.5/50.3
FLYING TECHNIQUE TO STABILIZE SPEED:
Adjust pitch in order to fly the required flight path.
When target pitch is reached, flying intended flight path, adjust thrust to target.
If the aircraft pitch tends to increase, aircraft is slow, then increase thrust;
If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 131/140
FCOM 19 AUG 10
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY ITEMS (Cont'd)
INITIAL AND INTERMEDIATE APPROACH IN LEVEL FLIGHT
The approach phase between Green Dot speed (clean configuration) and the landing
configuration (CONF 3), is flown in level flight.
LANDING GEAR UP IN LEVEL FLIGHT
Above 190 t 190 t - 160 t Below 160 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
0 G-DOT 5/55.3 5.5/51.3 5/47.5
1 S 9/57.6 9/53.0 9/48.5
1+F (1) S 6/59.3 6/54.6 6/49.9
2 F 6/60.6 6/55.8 6/51.1
LANDING GEAR DOWN IN LEVEL FLIGHT (EXPECT GRVTY EXTENSION)
3 F 6.5/65.9 6.5/61.0 6.5/55.8
(1) Due to the fact that the speed is unreliable, the SFCC may select the 1+F configuration in approach, instead of 1.
FINAL APPROACH AT STANDARD - 3 ° DESCENT FLIGHT PATH
LANDING GEAR DOWN
Above 190 t 190 t - 160 t Below 160 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
3 VLS +10 4/48.9 4/45.0 4/41.3
FLYING TECHNIQUE TO STABILIZE SPEED:
Adjust pitch in order to fly the required flight path.
When target pitch is reached, flying intended flight path, adjust thrust to target.
If the aircraft pitch tends to increase, aircraft is slow, then increase thrust;
If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 132/140
FCOM 19 AUG 10
UNRELIABLE SPEED INDICATION/ADR CHECK PROC (BUSS)
Applicable to: ,
�� If the safe conduct of the flight is impacted:
MEMORY ITEMS:
AP/FD.................................................................................................................................. OFF
A/THR.................................................................................................................................. OFF
�� PITCH/THRUST:
Below THRUST RED ALT.................................................................................. 15° / TOGA
Above THRUST RED ALT and Below FL 100.......................................................10° / CLB
Above THRUST RED ALT and Above FL 100........................................................ 5° / CLB
FLAPS................................................................................................. Maintain current CONFIG
SPEEDBRAKES..................................................................................................Check retracted
L/G......................................................................................................................................... UP
GPS ALTITUDE.......................................................................................................Display on MCDU
PROBE WINDOW HEAT................................................................................................................ ON
AFFECTED ADR(S) IDENTIFICATION
Crosscheck all speeds and altitudes indications.
Alternates sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect.
�� If affected ADR(s) identified:
Affected ADR(s) P/B...........................................................................................................OFF
REMAINING AIR DATA............................................................................................ CONFIRM
�� If affected ADR(s) cannot be identified or all ADRs are affected:
ALL ADRs P/B.................................................................................................................... OFF
All ADRs pb must be switched OFF to replace the PFD's normal speed scale and altitude
indication to the backup speed scale and GPS altitude indication.
NAV ADR 1+2+3 FAULT
Refer to PRO-ABN-34-R NAV ADR 1+2+3 FAULT.
　
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