Tokyo - Osaka
Flight / Schedule
Tokyo - Osaka
Aircraft
Boeing 747-200Registration
JA8119
MSN
20783
Year of Manufacture
1974
Operator
Japan AirlinesDate
August 12, 1985 at 06:56 PM
Type
CRASHFlight Type
Scheduled Revenue Flight
Flight Phase
Flight
Crash Site
Mountains
Crash Location
Mt Osutaka Kanto
Region
Asia • Japan
Crash Cause
Human factor
Narrative Report
On August 12, 1985 at 06:56 PM, Tokyo - Osaka experienced a crash involving Boeing 747-200, operated by Japan Airlines, with the event recorded near Mt Osutaka Kanto.
The flight was categorized as scheduled revenue flight and the reported phase was flight at a mountains crash site.
524 people were known to be on board, 520 fatalities were recorded, 4 survivors were identified or estimated. This corresponds to an estimated fatality rate of 99.2%.
Crew on board: 15, crew fatalities: 14, passengers on board: 509, passenger fatalities: 506, other fatalities: 0.
The listed crash cause is human factor. JA8119 was a Japan Air Lines Boeing 747SR, a short range variant of the Boeing 747 Series 100. The was aircraft specifically configured for domestic flights with a high density seating arrangement. On June 2, 1978 the aircraft operated on a flight to Osaka (ITM). It floated after touchdown and on the second touchdown the tail struck the runway. The aircraft sustained substantial damage to the rear underside of the fuselage. The rear pressure bulkhead was cracked as well. The aircraft was repaired by Boeing. Engineers replaced the lower part of the rear fuselage and a portion of the lower half of the bulkhead. Seven years later, on August 12, 1985, JA8119 had completed four domestic flights when it landed at Tokyo-Haneda (HND) at 17:17. The next flight was to be flight 123 to Osaka (ITM). The aircraft took off from Tokyo-Haneda at 18:12. Twelve minutes later, while climbing through 23900 feet at a speed of 300 knots, an unusual vibration occurred. An impact force raised the nose of the aircraft and control problems were experienced. A decompression had occurred and the crew got indications of problems with the R5 door. In fact, the rear pressure bulkhead had ruptured, causing serious damage to the rear of the plane. A portion of its vertical fin, measuring 5 m together with the section of the tail cone containing the auxiliary power unit (APU) were ripped off the plane. Due to the damage, the hydraulic pressure dropped and ailerons, elevators and yaw damper became inoperative. Controlling the plane was very difficult as the airplane experienced dutch rolls and phugoid oscillations (unusual movement in which altitude and speed change significantly in a 20-100 seconds cycle without change of angle of attack). The aircraft started to descend to 6600 feet while the crew tried to control the aircraft by using engine thrust. Upon reaching 6600 feet the airspeed had dropped to 108 knots. The aircraft then climbed with a 39 degree pitch-up to a maximum of approx. 13400 feet and started to descend again. At 18:56 JAL123 finally brushed against a tree covered ridge, continued and struck the Osutaka Ridge, bursting into flames. A stewardess, one female passenger and two little girl survived while 520 other occupants were killed.
Aircraft reference details include registration JA8119, MSN 20783, year of manufacture 1974.
Fatalities
Total
520
Crew
14
Passengers
506
Other
0
Crash Summary
JA8119 was a Japan Air Lines Boeing 747SR, a short range variant of the Boeing 747 Series 100. The was aircraft specifically configured for domestic flights with a high density seating arrangement. On June 2, 1978 the aircraft operated on a flight to Osaka (ITM). It floated after touchdown and on the second touchdown the tail struck the runway. The aircraft sustained substantial damage to the rear underside of the fuselage. The rear pressure bulkhead was cracked as well. The aircraft was repaired by Boeing. Engineers replaced the lower part of the rear fuselage and a portion of the lower half of the bulkhead. Seven years later, on August 12, 1985, JA8119 had completed four domestic flights when it landed at Tokyo-Haneda (HND) at 17:17. The next flight was to be flight 123 to Osaka (ITM). The aircraft took off from Tokyo-Haneda at 18:12. Twelve minutes later, while climbing through 23900 feet at a speed of 300 knots, an unusual vibration occurred. An impact force raised the nose of the aircraft and control problems were experienced. A decompression had occurred and the crew got indications of problems with the R5 door. In fact, the rear pressure bulkhead had ruptured, causing serious damage to the rear of the plane. A portion of its vertical fin, measuring 5 m together with the section of the tail cone containing the auxiliary power unit (APU) were ripped off the plane. Due to the damage, the hydraulic pressure dropped and ailerons, elevators and yaw damper became inoperative. Controlling the plane was very difficult as the airplane experienced dutch rolls and phugoid oscillations (unusual movement in which altitude and speed change significantly in a 20-100 seconds cycle without change of angle of attack). The aircraft started to descend to 6600 feet while the crew tried to control the aircraft by using engine thrust. Upon reaching 6600 feet the airspeed had dropped to 108 knots. The aircraft then climbed with a 39 degree pitch-up to a maximum of approx. 13400 feet and started to descend again. At 18:56 JAL123 finally brushed against a tree covered ridge, continued and struck the Osutaka Ridge, bursting into flames. A stewardess, one female passenger and two little girl survived while 520 other occupants were killed.
Cause: Human factor
Occupants & Outcome
Crew On Board
15
Passengers On Board
509
Estimated Survivors
4
Fatality Rate
99.2%
Known people on board: 524
Operational Details
Schedule / Flight
Tokyo - Osaka
Operator
Japan AirlinesFlight Type
Scheduled Revenue Flight
Flight Phase
Flight
Crash Site
Mountains
Region / Country
Asia • Japan
Aircraft Details
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