Country
code
Masovian Voivodeship (Mazowieckie)
Crash of a Rockwell Grand Commander 690A in Warsaw
Date & Time:
Nov 29, 1995 at 0220 LT
Registration:
EC-FFE
Survivors:
Yes
MSN:
690-11344
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Warsaw-Okecie Airport runway 33 by night, the pilot reported engine problems when the aircraft lost height and crashed in the district of Mysiadło, about six km short of runway threshold. All four occupants were injured and there were no victims on the ground. The aircraft was destroyed. It was reported that both engines lost power on approach, maybe after being taken over by frost. At the time of the accident, icing conditions were present in Warsaw.
Crash of an Airbus A320-211 in Warsaw: 2 killed
Date & Time:
Sep 14, 1993 at 1643 LT
Registration:
D-AIPN
Survivors:
Yes
Schedule:
Frankfurt - Warsaw
MSN:
105
YOM:
1990
Flight number:
LH2904
Crew on board:
6
Crew fatalities:
Pax on board:
64
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total hours on type:
1440.00
Copilot / Total hours on type:
1595
Aircraft flight hours:
7546
Aircraft flight cycles:
6721
Circumstances:
Following an uneventful flight from Frankfurt, the crew started the descent to Warsaw-Okecie Airport in poor weather conditions with thunderstorm activity, wind shear, rain falls and CB's. After being cleared to land on runway 11, the wind component changed during the last seconds. The right main gear touched down 770 metres past the runway threshold (aircraft's speed was 170 knots). The left main gear touched down 9 seconds later, 1,525 metres past the runway threshold. On a wet runway, the crew started the braking procedure and activated the thrust reversers and spoilers but the remaining distance was insufficient. At a speed of 72 knots, the aircraft overran, went down an embankment, lost its left engine and came to rest 90 metres further, bursting into flames. A female passenger and the captain were killed while all other occupants were rescued, among them 51 were seriously injured. The aircraft was destroyed by a post crash fire.
Probable cause:
Cause of the accident were incorrect decisions and actions of the flight crew taken in situation when the information about windshear at the approach to the runway was received. Wind shear was produced by the front just passing the aerodrome; the front was accompanied by intensive variation of wind parameters as well as by heavy rain on the aerodrome itself. Actions of the flight crew were also affected by design features of the aircraft which limited the feasibility of applying available braking systems as well as by insufficient information in the aircraft operations manual (AOM) relating to the increase of the landing distance.
Final Report:
Crash of a Douglas DC-9-32 in Warsaw
Date & Time:
Dec 17, 1991 at 1749 LT
Registration:
I-RIBN
Survivors:
Yes
Schedule:
Rome - Warsaw
MSN:
47339
YOM:
1969
Flight number:
AZ552
Crew on board:
6
Crew fatalities:
Pax on board:
90
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While descending to Warsaw-Okecie Airport, the crew encountered poor weather conditions with thunderstorm activity. On final approach, the copilot suggested the captain to abandon the landing procedure and to initiate a go-around maneuver. The captain dismissed the copilot's suggestion, disengaged the autopilot system and continued the approach when visual contact with the ground was established at an altitude of 400 feet. In a nose-down attitude and at an excessive speed of 155 knots (about 25-30 knots above the recommended speed), the aircraft struck the runway 33 surface nose gear first. The aircraft bounced then veered off runway to the left, rolled on soft ground for about 860 metres and lost its nose gear before coming to rest. All 96 occupants were evacuated, among them three passengers were slightly injured. The aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the flying crew who decided to continue the descent while the aircraft was unstable and misaligned with the runway. The following contributing factors were reported:
- Failure of the crew to initiate a go-around procedure,
- Unstabilized approach,
- Excessive approach speed,
- Touchdown completed in a nose-down attitude,
- Poor crew coordination,
- Poor weather conditions with thunderstorm activity.
- Failure of the crew to initiate a go-around procedure,
- Unstabilized approach,
- Excessive approach speed,
- Touchdown completed in a nose-down attitude,
- Poor crew coordination,
- Poor weather conditions with thunderstorm activity.
Crash of an Ilyushin II-62 in Warsaw: 183 killed
Date & Time:
May 9, 1987 at 1112 LT
Registration:
SP-LBG
Survivors:
No
Schedule:
Warsaw - New York
MSN:
3344942
YOM:
1973
Flight number:
LO5055
Crew on board:
11
Crew fatalities:
Pax on board:
172
Pax fatalities:
Other fatalities:
Total fatalities:
183
Captain / Total hours on type:
5546.00
Copilot / Total hours on type:
1966
Aircraft flight hours:
6972
Aircraft flight cycles:
1752
Circumstances:
At 10:18 flight LO5055 took off from Warsaw runway 33 for a flight to New York-JFK. The aircraft headed for the GRU VOR, which it passed at FL265, climbing to FL310. Two minutes later (at 10:41) the n°2 engine Low Pressure turbine shaft broke loose, followed by the failure of the turbine disc. Debris punctured the aft fuselage, causing a fire in the cargo hold. The elevator control system was severed and the n°1 engine had to be shut down. The flight crew immediately started an emergency descent to 4,000 metres. After shutting down both n°1 and n°2 engine the crew mistakenly thought the fire was extinguished. They had decided to land at Modlin airport, but still unaware of the fire, changed to Warsaw-Okecie runway 33 because of better rescue equipment there. The flight started a left turn for runway 33 at 11:09 at an altitude of 1,450 metres and an airspeed of 480 km/h. The crew lost control during the turn and the Il-62 crashed into a forest, 6 km from the runway at an airspeed of 465 km/h and an 11° left bank and 12° nosedown. The aircraft disintegrated on impact and all 183 occupants were killed.
Probable cause:
The cause of the accident was the destruction of engine no.2 resulting in disconnection of the longitudinal control system from the control column, cabin depressurisation, damage to the electric system and fire. At the end stage of flight the fire caused the loss of the aircraft longitudinal control and the impact with the ground after 31 minutes as counted from the beginning of the emergency situation. The destruction of engine no.2 occurred without any signal from the warning/testing system. Under the circumstances the crew members were not able to stop the engine in good time, consequently an emergency situation was created on board the aircraft.