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Printed page 48. PDF page 50.
auto-thrust disengaged o Flight control law reverted from Normal Law to Alternate Law o Rudder deflected 2� and aileron deflection 0�. - The aircraft started to roll. - At 2316:54 UTC the FAC 2 was back to ON and allOpen official document at PDF page 50Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 104. PDF page 106.
FAULT message associated with the 6th master caution. The FAC 1+2 FAULT was followed by rudder deflected 2� to the left, the aircraft flight control status reverted from Normal Law to Alternate Law and the Auto Pilot (A/P) and theOpen official document at PDF page 106Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 117. PDF page 119.
disengaged, and the Flight control law reverted from Normal Law to Alternate Law. The rudder deflected 2� to the left. 117Open official document at PDF page 119Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 118. PDF page 120.
remained unavailable and all equipment controlled by FAC did not operating. 14. The rudder deflected 2� resulting in a roll rate of 6 degrees/second to the left, and without pilot input for 9 seconds, resulting the aircraft rolling to theOpen official document at PDF page 120Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014