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Printed page Cover. PDF page 1.
Investigation Report PT. Indonesia Air Asia Airbus A320-216; PK-AXC Karimata Strait Coordinate 3�37'19"S - 109�42'41"E Republic of Indonesia 28 December 2014 KOMITE NASIONAL KESELAMATAN TRANSPORTASI REPUBLIC OF INDONESIA 2015Open official document at PDF page 1Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 10. PDF page 12.
recorders such as the Cockpit Voice Recorder and Flight Data Recorder. UTC : Universal Time Coordinate VLE : Maximum Landing Gear Extended Speed VLS : Lowest Selectable Speed VHF : Very High Frequency VS : Vertical speed WD : WindshearOpen official document at PDF page 12Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 14. PDF page 16.
advisory AUTO FLT RUD TRV LIM 1 appeared. The PF asked "ECAM action". 1 UTC (Universal Time Coordinate) is the primary time standard by which the world regulates clocks and time. It is, within about 1 second, mean solar timeOpen official document at PDF page 16Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 17. PDF page 19.
according to the Automatic Dependent Surveillance- Broadcasting (ADS-B) radar was on coordinate 3�3648.36"S - 109�4150.47"E and the aircraft altitude was approximately 24,000 feet. The last data recorded by FDR was at 2320:35 UTC with ISIS airspeed of 132 kts, pitchOpen official document at PDF page 19Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 31. PDF page 33.
pilot control of the roll and heading, it also limits the roll rate and bank angle, coordinates the turns, and damps any Dutch roll. The roll rate requested by the pilot during flight is proportional to the side-stick deflection, withOpen official document at PDF page 33Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014
Printed page 37. PDF page 39.
takes over the corresponding channel. Yaw damping stabilizes the aircraft in yaw and coordinates its turns. In automatic flight (AP engaged) during takeoff and go around, it assists rudder application after an engine failure (short-term yaw compensation). Note: When theOpen official document at PDF page 39Aircraft Accident Investigation Report: PT. Indonesia Air Asia, Airbus A320-216, PK-AXC, 28 December 2014