Warsaw-Okęcie-Frederic Chopin

On November 1, 2011 a passenger LO 16 flight of B767-300ER airplane, registration marks SP-LPC, was scheduled from KEWR to EPWA. The Pre-Departure Check of the airplane was carried out by a ground engineer from a contracted service organization in accordance with Operator’s requirements. The ground engineer was responsible for conducting PRE-DEPARTURE CHECK and ETOPS CHECK. The above procedures did not include cockpit check. The ground engineer did not find any failures or irregularities and did not notice anything unusual. The flight crew arrived at Newark Liberty Airport at a time specified by Operator and in accordance with its operating procedures. When commencing the flight duty period the crew members were rested, refreshed, in a good psychophysical condition. They did not report overload by air operations. Upon arrival at the aircraft stand each flight crew member performed his duties as provided for in the operating procedures of the airline. CPT conducted Exterior Walk Around while FO conducted cockpit check. FO checked on-board equipment and the cockpit preparation for the flight. According to the flight crew statement no failures or irregularities were found. The crew deemed the airplane fully operational for the flight to Warsaw. The ground engineer from the contracted maintenance organization was not present in the cockpit during the flight crew preparation. During the flight CPT was PF and FO was PM. At 03:58:11 hrs the crew started the engines. The take-off took place at 04:19:08 hrs. After the take-off, during the retraction of landing gear and flaps the hydraulic fluid from the center hydraulic system (C system) flew out, which consequently led to pressure drop in this system. The pressure drop in the C system was signaled on the hydraulic panel – SYS PRESS and on EICAS - C HYD SYS PRESS and recorded by on-board flight data recorders. After completion HYDRAULIC SYSTEM PRESSURE (C only) procedure contained in QRH and consultation with the Operator's MCC, the flight crew decided to continue the flight to Warsaw. The flight proceeded without significant distortions. Landing in Warsaw was to be carried out with the alternate landing gear extension system. This situation was well known to pilots due to numerous exercises carried out in a flight simulator. Taking advantage of the available time, the CPT and FO developed a plan for landing in accordance with the procedure contained in QRH and discussed an anticipated sequence of events. At 12:17 hrs, during approach to landing on EPWA aerodrome the flight crew performed the procedure of the lading gear extension using the alternate landing gear extension system. However, after the anticipated time the landing gear was not extended. The crew checked the correctness of execution of the procedure against QRH and again attempted to extend the landing gear. After failure of the second attempt to extend the landing gear with the alternate system the approach to landing was abandoned. At 12:22 hrs the crew reported to ATC inability to extend the landing gear and requested the Operator’s MCC assistance. Around 12:25 hrs the flight crew declared EMERGENCY. The airplane was directed to a holding zone. The Operator’s Operations Centre enabled the crew to communicate with experts. FO executed expert recommendations and checked the alternate landing gear extension switch and circuit breakers on P-11 and P6-1 panels. After that FO reported to Operations Centre and to CPT that the circuit breakers had been checked. FO also cycled (pulled and reset) the ALT EXT MOTOR circuit breaker as indicated by an expert. However, the landing gear was not extended. In the meantime pilots of two F-16s of the Polish Air Force inspected SP-LPC from the air and informed the crew that the landing gear was still in the retracted position but the tail skid was extended. After that information the crew attempted to extend the landing gear in a gravitational way, but it also ended in failure. After a series of unsuccessful attempts to extend the landing gear and due to low fuel quantity, the crew decided to carry out an emergency gear up landing. CC1 was instructed by Captain to prepare the cabin and passengers for emergency landing. During the preparation the passengers were calm, they carried out the crew instructions, there was no panic. Prior to the landing firefighters distributed foam over RWY 33 at a distance of about 3000 m. External services arrived at the airport (PSP and emergency ambulances). The plane touched down on RWY 33 of EPWA aerodrome (Figure 7) at 13:39 hrs. At the time of touchdown about 1600 kg of fuel (1939 liters at a density of 0.825 kg/l) was in its tanks, the engines were running and their recorded speeds were N1ACTL = 57%, N1ACTR = 38%. The plane was moving on RWY 33 along its centre line and stopped 42 m after the intersection with RWY 29. When the aircraft was moving, sparks were coming out of the right engine, and they were suppressed by the applied foam; then the engine caught fire. When the airplane came to rest, the crew evacuated the passengers and LSP extinguished the fire. During the evacuation none of the passengers or crew suffered any injuries. During the landing the aircraft sustained substantial damage, which caused its withdrawal from service.

On 14 July, 2011 ATR 72 flight crew after landing at EPWA aerodrome received the clearance for taxiing to parking stand 41 via taxiways: "S", "O" and "M". When the airplane was on taxiway "M2", "Mulag" type tractor was moving by the service road, passing perpendicularly to taxiway “M2”. The tractor driver did not give the right of way to ATR 72 and the tractor collided with the airplane. As a result, the airplane and the tractor sustained substantial damages. The flight crew stopped the airplane and shut down the engines. Airport Fire Brigade and an ambulance were called. The tractor operator suffered some injuries and was taken to hospital. the airplane passengers and the flight crew did not suffer any injuries. The impact caused a fuel leakage from the airplane of 200 m2 in area, which was removed along with other elements of the damaged aircraft by the Airport Fire Brigade. The airplane and the "Mulag" tractor were withdrawn from the further service. During the accident there were adverse weather conditions at the airport - heavy rain and lightning which caused reduction in visibility.

On approach to Smolensk Airport in poor weather conditions, crew was forced to make a go-around and approach was abandoned three times. On the fourth approach, at a speed of 260 km/h, aircraft went beyond the minimum safe altitude, hit tree tops, lost its left wing and crashed in a huge explosion. All 96 occupants were killed, among them the President of the Polish Republic Lech Kaczyński and his wife. He was flying to Smolensk to take part to the commemoration of the 70th anniversary of Katyn massacre when Soviet Army killed 20,000 Polish officers. Among the delegation were also members of the Polish Senate and Government; the ex President, the vice-president of low Chamber, the Senate vice-president, the president of the polish central bank, the chief of military staff, the chief of ground forces, the chief of the Air Force, the chief of special forces, the chief of Marines, the personal assistant of President, the chief of National Security, the vice-Minister of Defense and the vice-Minister of Foreign Affairs.

En route from Hurghada to Warsaw, while cruising over Turkey, the crew contacted ATC and reported electrical and hydraulic problems. The crew was cleared to divert to Istanbul-Atatürk Airport for an emergency landing. After touchdown, the aircraft was unable to stop within the remaining distance. It overran and came to rest near the ILS antenna after both main gears collapsed. All 163 occupants evacuated safely and the aircraft was damaged beyond repair.

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.

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.

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.

While descending to Rzeszów-Jasionka Airport, one of the engine failed. Unable to maintain a safe altitude, the captain decided to attempt an emergency landing in a field located in Łańcut, about 14 km southeast of Rzeszów Airport. After landing, the aircraft slid for few dozen meters then came to rest, bursting into flames. Five occupants were injured while 23 others escaped uninjured. A passenger aged 69 was killed. The aircraft was totally destroyed by a post crash fire.

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.

The single engine airplane departed Budapest-Ferihegy on a ferry flight to Warsaw. En route, the crew encountered icing conditions and poor weather. He was cleared to return to Budapest and was instructed to maintain 4,000 feet minimum altitude. Few minutes later, the aircraft lost height and crashed on the slope of a hill located near Pilisszentlélek. Both occupants were killed.