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Printed page 126. PDF page 137.
caused separation of the rudder, and four systems of hydraulic pressure line for the rudder control system were all fractured. 4.1.6.6 It is estimated that such destruction of the aircraft progressed within a period as short as a few seconds.Open official document at PDF page 137AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 270.
fuselage or the aft Passenger cabin ; . (3) malfunctions of the vertical fin and the rudder control systems (4) malfunctions of the horizontal stabilizer, the elevator control systems, and the stabilizer trim control system (5) malfunctions of pressurization, air-conditOpen official document at PDF page 270AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 271.
fuselage or the aft passenger cabin None (3) Malfunctions of the vertical fin and the rudder control system (2 cases) In flight 902 of June 18, there was a discrepancy that with the upper rudder at the neutral position theOpen official document at PDF page 271AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 289.
but no corresponding movement of the aircraft was observed. Abnormality occurred on rudder control systems at 1824:36.2 through this time. (magnified plot] , Corresponding to abnormal external force, airspeed decreased a little, and AOA and PCH increased, and large motOpen official document at PDF page 289AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 77.
structural component, Siving rise to collapse of the rear spar, and to separation of the rudder supported by the spar, as well as to damage of the rudder-related control cable system and the rudder-related hydraulic lines. 3.1.2.5 Study on FlutterOpen official document at PDF page 77AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 89.
into a limit cycle as amplitude increases. (5) Lateral-Directional Control Out of the rudder and the aileron-spoiler systems originally used for lateral- directional control, it is considered that the rudder had been separated almost at the same time when theOpen official document at PDF page 89AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119