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Printed page label not indexed. PDF page 33.
Attached Figure-5). Medical inspection at hospital upon their rescue indicated that all four survivors were seriously injured with bone fractures at parts different for each due to strong impact from the crash, and subjected more or less to a traumaticOpen official document at PDF page 33AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 129.
situation where part of the vertical fin is separated and the hydraulic pressure of all four systems decrease to zero and most of control functions are lost would be out of the scope of the education and training or knowledgeOpen official document at PDF page 129AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page 130. PDF page 141.
Recommendation A-85-134, Dec.5, 1985) Design mofification should be made so that the integrity of all four hydraulic systems will not be impaired in the event that a significant pressure buildup occurs in the normally unpressurized empennage. c) Reevaluation of theOpen official document at PDF page 141AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 34.
section, there was found comparatively little cosmetic damage, but autopsy indicated almost all of them suffered from total bruise, brain damage or bursting of internal organs, resulting in instantaneous or near-instantaneous death except for the four survivors. 2. 14 SurvivalOpen official document at PDF page 34AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 65.
an investigation on four leading edge flap rotary actuators (set position unknown for all). 2.15.3 Investigation of Warning Lights, Switch Lights, ete It was very difficult to identify systems or to judge on their operational Status, because the wiring, electricOpen official document at PDF page 65AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 123.
pressure presumed in the fail- safe design, resulting in the rupture of the APU firewall and the vertical fin. 3.2.5.3 A Study on Redundancy of Control System (1) Such redundancy is incorporated in the design of the control system thatOpen official document at PDF page 123AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119