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Printed page label not indexed. PDF page 38.
(including the APU fire wall) aft of BS2658 (to which APU fire wall is attached) was not found in the recovered debris. It is noted that the APU air intake duct attached to this part of structure was recovered fromOpen official document at PDF page 38AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page 125. PDF page 136.
which had been existent at the rivet connected portions of L18 splice were not found. The inspection method of the aft pressure bulkhead in the time of C maintenance might have been a proper method, because it was unconceivable atOpen official document at PDF page 136AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 21.
skin of the torque box and stringers were fractured and separated, but other parts were not recovered from the accident site. (2) A small portion of the vertical fin torque box base attached to the fuselage remained on the fuselageOpen official document at PDF page 21AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 24.
experiment vessel of the Oceanic Science and Technology Center. There was, however, nothing found which may be regarded as the wreckage of the the aircraft. (1) Investigation area An area in which part of the wreckage of the aircraft mightOpen official document at PDF page 24AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 32.
(refer to 2.1 History of the Flight) for the reason that the radar echo near Kowa had not been cleared up and that almost no radar echo was found over the sea further south, and it was acknowledged by theOpen official document at PDF page 32AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 62.
found in the paper filter element. Two valves were operable by finger, but the other was not. (p) Wing Gear Door Actuator (one, set position unknown) It was substantially damaged throughout, dented in the middle of the cylinder, and wasOpen official document at PDF page 62AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119