Skåning
Well-Known Member
http://kemhubri.dephub.go.id/knkt/ntsc_home/ntsc.htm
The basics after a quick look:
Equipment failure leads to alternate law
Pilot flying (first officer) initially corrects rudder induced left roll but also pitches up 15 degrees.
Aircraft climbs rapidly to FL380, stall warning followed by stall.
Pilot flying maintains full back stick to end of recording.
Stall upset recognized by Captain but no clear transfer of control.
Contrasting dual stick inputs for the most part.
From the report:
Contributing factors
The cracking of a solder joint of both channel A and B resulted in loss of electrical continuity and led to RTLU failure.
The existing maintenance data analysis led to unresolved repetitive faults occurring with shorter intervals. The same fault occurred 4 times during the flight.
The flight crew action to the first 3 faults in accordance with the ECAM messages. Following the fourth fault, the FDR recorded different signatures that were similar to the FAC CB‟s being reset resulting in electrical interruption to the FAC‟s.
The electrical interruption to the FAC caused the autopilot to disengage and the flight control logic to change from Normal Law to Alternate Law, the rudder deflecting 2° to the left resulting the aircraft rolling up to 54° angle of bank.
Subsequent flight crew action leading to inability to control the aircraft in the Alternate Law resulted in the aircraft departing from the normal flight envelope and entering prolonged stall condition that was beyond the capability of the flight crew to recover.
The basics after a quick look:
Equipment failure leads to alternate law
Pilot flying (first officer) initially corrects rudder induced left roll but also pitches up 15 degrees.
Aircraft climbs rapidly to FL380, stall warning followed by stall.
Pilot flying maintains full back stick to end of recording.
Stall upset recognized by Captain but no clear transfer of control.
Contrasting dual stick inputs for the most part.
From the report:
Contributing factors
The cracking of a solder joint of both channel A and B resulted in loss of electrical continuity and led to RTLU failure.
The existing maintenance data analysis led to unresolved repetitive faults occurring with shorter intervals. The same fault occurred 4 times during the flight.
The flight crew action to the first 3 faults in accordance with the ECAM messages. Following the fourth fault, the FDR recorded different signatures that were similar to the FAC CB‟s being reset resulting in electrical interruption to the FAC‟s.
The electrical interruption to the FAC caused the autopilot to disengage and the flight control logic to change from Normal Law to Alternate Law, the rudder deflecting 2° to the left resulting the aircraft rolling up to 54° angle of bank.
Subsequent flight crew action leading to inability to control the aircraft in the Alternate Law resulted in the aircraft departing from the normal flight envelope and entering prolonged stall condition that was beyond the capability of the flight crew to recover.