Bucharest-Otopeni-Henri Coandă

Following an uneventful flight from Bucharest-Otopeni Airport, the crew started the approach to Oradea Airport in marginal weather conditions. On final approach, the pilot-in-command established a visual contact with the runway 19 and continued the descent. The aircraft landed 761 metres past the runway threshold. After touchdown, it was unable to stop within the remaining distance, overran and came to rest in a drainage ditch located 420 metres short of runway 01 threshold. All 13 occupants escaped uninjured while the aircraft was damaged beyond repair.

Following an uneventful flight from Timişoara, the crew initiated the approach to Bucharest-Otopeni-Henri Coanda Airport in poor weather conditions. After touchdown, the crew encountered difficulties to stop the aircraft. On a wet runway surface, the aircraft deviated to the right, causing the right main gear to be torn off while contacting soft ground. The airplane came to rest, straddling on the runway edge. All 73 occupants evacuated safely and the aircraft was damaged beyond repair.

Around 1100LT, an airport maintenance team consisting of four people in two cars (Kia minivan) was cleared to enter runway 08R to perform maintenance work on the runway lighting system. Two of the men were working at about 600 meters from the threshold and the two other men were working at about 1500 meters from the threshold. Visibility at the time was poor due to thick fog. At 11:04 the runway was vacated by both vehicles due to landing traffic. At 11:06 they were recleared to enter the runway. At 11:25:13 flight ROT3107, a Boeing 737-300, was cleared to enter runway 08R for takeoff. The flight was cleared for takeoff at 11:26:07. Between 11:26:40 and 11:26:50 the control tower asked the maintenance workers if the runway was clear but got no reply. During the takeoff roll, at a speed of 90 knots, the aircraft collided with one of the van that was 'parked' about 600 metres from the threshold with its left engine and left main gear. The van was totally destroyed upon impact and the aircraft veered off runway to the left and came to rest 137 metres to the left of the centerline and 950 metres from the threshold. All 123 occupants evacuated safely and there were no injuries with ground maintenance personnel.

Flight ROT 335, a BAC 111 coming from Bucharest, was about to land on runway 26 at Stockholm/Arlanda airport. The pilots had visual contact with the field and the landing was performed according to visual flying rules (VFR). The commander, who was pilot flying (PF), has stated the following. The approach was normal with occasional turbulence and wind gusts from the south. When the aircraft was on 8 nautical miles1 final, the air-traffic controller in the tower reported the wind 160°/13 knots. To begin with the aircraft was somewhat above the glide slope but was on the glide slope when it passed the threshold. The touchdown on the runway was in the normal touchdown zone on the left main gear and nose up. Shortly thereafter came a strong wind gust whereupon the right main gear touched down and the nose gear heavily hit the runway. The commander controlled the aircraft with rudder, reversed the engines and braked lightly. He did not notice anything special in the behavior of the aircraft at that point. When - after the speed had become so low that rudder steering was no longer possible - he reverted to nose wheel steering he noticed that it was not functioning. He continued the light wheel braking but could not prevent the aircraft from veering to the right. He then braked fully but the aircraft continued towards the right runway edge. It left the runway at a speed of around 60 knots out onto the grass field. The retardation was soft and the passengers disembarked through ordinary exit. The airport rescue service was speedily on the scene but no action was necessary. The accident occurred on 7 June 1997 at 1350 hours in position 5939N 1755E; 121 feet (37 m) above sea level.

The approach and landing at Istanbul-Atatürk was completed in marginal weather conditions with sleet, strong winds and turbulences. The copilot was the pilot-in-command. Upon touchdown on runway 36, the aircraft landed hard and bounced. On the second impact, the nose gear collapsed. The aircraft went out of control, veered off runway to the right at a speed of 60 knots and came to rest. All 81 occupants escaped uninjured while the aircraft was damaged beyond repair. The wind was gusting up to 29 knots at the time of the accident with a visibility limited to 4 km.

Tarom flight 371 was a scheduled passenger service from Bucharest Otopeni Airport (OTP) in Romania to Brussel Airport (BRU), Belgium. On board were 49 passengers and eleven crew members. The first officer was pilot flying, the captain was pilot monitoring. Following de-icing, the Airbus A310 taxied to runway 08R for departure. The flight was cleared via the Strejnic 'STJ' VOR/DME beacon and an initial climb to flight level 260. Takeoff was initiated at 09:04 hours local time. When airborne, the captain announced positive climb and co-pilot requested to retract the landing gear. At 09:07:20 the captain called the Otopeni Approach controller and received a clearance to turn left and proceed direct to STJ. The co-pilot asked the captain to select direct STJ on FMS. The captain confirmed a direct STJ selection and requested the co-pilot to move the control wheel slightly. At an altitude of 1700 feet and speed a 187 knots, with flaps 15/slats 15 and pitch angle of 17.6 degrees, the aircraft was turning left, with a bank angle of 12 degrees, flying towards STJ. At 09:07:36, when the aircraft crossed 2000 feet at 188 knots, an engine thrust asymmetry started developing with continuous decrease of the left engine thrust, approximately 1 degree TRA (throttle resolver angle)/second. At 09:07:53, when the aircraft was crossing 3300 feet altitude at 195 kts turning with a decreasing bank angle of 20 degrees, the first officer called "250 in sight" and asked the captain to retract the flaps. This was carried out. At that moment, the engine thrust asymmetry reached 14.5 TRA degrees and 0.19 for EPRs. The first officer then requested slats retraction, but this action which was not carried out by the captain. At this moment the aircraft was passing through 013 degrees magnetic heading, at 3800 feet altitude and a decreasing speed of 185 kts. The aircraft pitch angle was 16,5 degrees, decreasing, and the left bank angle was 18 degrees, also decreasing. At that time the thrust asymmetry reached was 28 TRA degrees and 0.27 for EPRs. At 09:08:02, the first officer asked the captain: "Are you all right?" The aircraft was passing through 330 degrees magnetic heading, 4200 ft altitude, a decreasing speed of 181 kts, and an increasing 17 degrees left bank angle. At 09:08:08, a noise like an uttering of pain or a metallic noise was heard. The aircraft was crossing 4460 ft altitude, 179 kts speed and an increasing bank angle of 22 degrees. At that time the engines thrust asymmetry reached 0.36 for EPRs. The bank angle continued to increase to 28 degrees and the engine thrust asymmetry reached 0.41 for EPRs. At 09:08:15, the first officer, with a stressed and agitated voice, requested engagement of autopilot no. 1. The aircraft was crossing 4620-ft altitude, continuing its turn at an increasing bank angle of 43 degrees and a steadily decreasing pitch angle of 3.5 degrees. One of the pilots attempted to engage autopilot no. 1 The aircraft started a descent with 45 degrees bank angle and the engine thrust asymmetry had reached the maximum value of 0.42 for EPRs, followed by a continuous thrust reduction of engine n°2. One second later, there was recorded autopilot disengagement followed by the aural warning a level 3 "cavalry charge" lasting several moments. From that moment on, the aircraft started diving, the speed increased and the aircraft performed a complete rotation around its roll axis. At 09:08.28, first officer cried out "THAT ONE HAS FAILED!" without any other comments. The aircraft was descending through 3600 ft at 258 kts speed and an increasing nose down pitch angle at 61.5 degrees. The aircraft continued until it impacted the ground at a nose down attitude of approximately 50 degrees pitch angle with both engines at idle power. The airplane was destroyed and all 60 occupants were sustained fatal injuries.

During the takeoff roll at Oradea Airport, the flight engineer under training prematurely retracted the landing gear. The aircraft sank on its belly and skidded on runway before coming to rest. All 11 occupants evacuated safely while the aircraft was damaged beyond repair.

The approach to Bucharest-Otopeni Airport was completed in poor weather conditions with a visibility reduced to 100 metres in fog. The aircraft landed slightly to the right of the runway 26L centerline, causing the right wing to struck a 60 cm high snow wall. The aircraft went out of control and eventually collided with an observation tower. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair.

The four engine aircraft departed Bucharest-Otopeni Airport at 2316LT on a cargo flight to Timişoara, carrying five crew members and four mechanics who were dispatched in Timişoara to repair another aircraft. En route, while cruising at an altitude of 6,100 metres, the crew reported his position and the ETA was fixed at 0003LT. After being cleared to descend to 2,440 metres, the crew changed his frequency and contacted Timişoara Approach. After passing over Faget, the crew was cleared to descend to 1,800 metres when radar and radio contacts were lost. The aircraft struck the slope of a mountain located in the Retezat Mountain Range, about 18 km northwest of Uricani and 130 km southeast of Timişoara Airport. The aircraft disintegrated on impact and all nine occupants were killed.

The Romanian Presidential Airplane was engaged in a series of tests prior to an official flight to China within two days. The crew consisting of pilots and engineers completed several circuits in the region of Bucharest-Otopeni Airport and was preparing to land when the aircraft rolled to the left on short final, causing both left engines n°1 and 2 to struck the runway surface. Fuel line ruptured and fuel ignited. The crew initiated an emergency braking procedure, vacated the runway by a taxiway and stopped the aircraft that was bursting into flames. All 13 occupants escaped uninjured while the aircraft was damaged beyond repair.