Dash8100
26th Sep 2002, 13:48
Does anyone have additional info/links to info about this tragic accident? What happened to the power levers and where was the captain?
Date: 31 March 1995
Airline: Tarom
Flight No.: 371
Aircraft: Airbus A310-324
Location: Bucharest, Romania
Fatalities: 60:60
The aircraft departed Bucharest-Otopeni runway 08R at 9:08am local time for a flight to Brussels. At 9:11, climbing through 4500ft, the Airbus began to descend again and finally entered a steep dive (80° nose-down) before crashing into a field. While climbing through 2000ft at 189 knots, the crew retracted flaps. At that time the auto throttles (on 'climb' mode) should have reduced power to the pre-determined climb setting on both engines. But the right power lever (no.2 engine) remained in takeoff power setting. It took the no.1 power lever 42 seconds to move to idle power. During these 42 seconds an asymmetric thrust situation developed. The aircraft by then had passed the 'OTR' VOR beacon and the crew had, according to SID procedures, begun a 25° left turn onto a 327° heading for the Strejnic 'STJ' VOR/DME beacon. Due to the thrust asymmetry, the nose-up pitch of 18° decreased to 0°. The aircraft rolled through 170° laterally and finally crashed into an open field and exploded on impact. The accident was likely caused bya lack of crew response to an extreme nose-down attitude. The investigation committee concluded that the Captain was either incapacitated or absent from his seat, because he had not said anything while the critical situation was developing. Just before impact the First Officer expressed his concern about the situation (either the Captain's condition or the aircraft's attitude) and attempted a recovery.
Date: 31 March 1995
Airline: Tarom
Flight No.: 371
Aircraft: Airbus A310-324
Location: Bucharest, Romania
Fatalities: 60:60
The aircraft departed Bucharest-Otopeni runway 08R at 9:08am local time for a flight to Brussels. At 9:11, climbing through 4500ft, the Airbus began to descend again and finally entered a steep dive (80° nose-down) before crashing into a field. While climbing through 2000ft at 189 knots, the crew retracted flaps. At that time the auto throttles (on 'climb' mode) should have reduced power to the pre-determined climb setting on both engines. But the right power lever (no.2 engine) remained in takeoff power setting. It took the no.1 power lever 42 seconds to move to idle power. During these 42 seconds an asymmetric thrust situation developed. The aircraft by then had passed the 'OTR' VOR beacon and the crew had, according to SID procedures, begun a 25° left turn onto a 327° heading for the Strejnic 'STJ' VOR/DME beacon. Due to the thrust asymmetry, the nose-up pitch of 18° decreased to 0°. The aircraft rolled through 170° laterally and finally crashed into an open field and exploded on impact. The accident was likely caused bya lack of crew response to an extreme nose-down attitude. The investigation committee concluded that the Captain was either incapacitated or absent from his seat, because he had not said anything while the critical situation was developing. Just before impact the First Officer expressed his concern about the situation (either the Captain's condition or the aircraft's attitude) and attempted a recovery.