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FL 250 - FL 370 260 kt 5/CLB 4.5/CLB 4.5/CLB
Above FL 370 M 0.80 4/CLB 4/CLB 4/CLB
CRUISE
Adjust N1 to maintain approximate level flight with pitch attitude held constant. When time
permits, Refer to PRO-SUP-91-10 GENERAL and adjust pitch to maintain level flight.
CLEAN
Above 190 t 190 t - 160 t Below 160 t
FL Speed Pitch (°)/Thrust (% N1)
Below FL 200 240 kt 4.5/59.2 3.5/56.4 2.5/54.3
FL 200 - FL 370 260 kt 3.5/70.9 2.5/67.7 2/66.1
Above FL 370 M 0.80 3.5/79.5 3/76.7 2.5/73.1
DESCENT
Set the thrust to IDLE
CLEAN
Above 190 t 190 t - 160 t Below 160 t
FL Speed Pitch (°)/Thrust (% N1)
Above FL 370 M 0.80 1/IDLE 0/IDLE -0.5/IDLE
FL 370 - FL 200 260 kt 1.5/IDLE 0.5/IDLE -0.5/IDLE
FL 200 - FL 100 240 kt 2.5/IDLE 1.5/IDLE 0/IDLE
Below FL 100 240 kt 2.5/IDLE 1/IDLE 0/IDLE
Below FL 100 G-DOT 2.5/IDLE 2.5/IDLE 2.5/IDLE
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 116/140
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 117/140
FCOM 19 AUG 10
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY ITEMS
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
When at, or above MSA or Circuit Altitude: level off for troubleshooting.
GPS ALTITUDE.......................................................................................................Display on MCDU
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 118/140
FCOM 19 AUG 10
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY ITEMS (Cont'd)
LEVEL-OFF (PITCH & THRUST TABLE)
�� To level off for troubleshooting:
AP/FD................................................................................................................................OFF
A/THR................................................................................................................................OFF
Note: Check the actual slat/flap config. on ECAM, as flap auto-retraction may occur.
SLATS/FLAPS EXTENDED
Above 190 t 190 t - 160 t Below 160 t
CONF Speed Pitch (°)/Thrust (% N1)
　
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