Page 36 - Demo

2.10/22
REV 11
A330
CHINA AIRLINES
REV 11
PAGE 22
RUDDER TRIM RUNAWAY
– LATERAL CONTROL .................... USE TO LEVEL WINGS – RUDDER.........................................................CENTRALIZE
Check the rudder position on the F/CTL SD page.
Note: This failure will be seen mainly as uncommanded roll (induced by yaw). In most conditions, the aircraft will self stabilize in a steady heading sideslip.
For continued flight, either maintain rudder central or leave the aircraft in a steady stabilized heading sideslip, but ensure that all changes between rudder centralized and steady heading sideslip are made smoothly. As speed is reduced, the FCPC may allow more rudder to be applied by the trim runaway.
– FOR LDG .......................................... USE NORMAL CONF