11 years ago today Polish Presidential plane crashed killing all 96 onboard including President Lech Kaczynski

11 years ago today Polish Presidential plane crashed killing all 96 onboard including President Lech Kaczynski
PLF 101, the aircraft involved in the accident, seen in 2008 – Credits:  Dmitry Karpezo 

The Smolensk air disaster occurred 11 years ago on 10 April 2010, when a Tupolev Tu-154 aircraft of the Polish Air Force crashed near the Russian city of Smolensk, killing all 96 people on board.

Among the victims were the President of Poland Lech Kaczyński and his wife Maria, the former President of Poland in exile Ryszard Kaczorowski, the chief of the Polish General Staff and other senior Polish military officers, the president of the National Bank of Poland, Polish Government officials, 18 members of the Polish Parliament, senior members of the Polish clergy and relatives of victims of the Katyn massacre.

The group was arriving from Warsaw to attend an event commemorating the 70th anniversary of the massacre, which took place not far from Smolensk.

Smolensk air disaster

The Tupolev Tu-154M airplane departed Warszawa-Okecie Airport (WAW), Poland at 07:27 local time, carrying Polish President Lech Kaczynski, his wife, several Members of Parliament, President of the National Bank of Poland Slawomir Skrzypek, Chief of General Staff Franciszek Gagor, the Deputy Minister of Foreign Affairs Andrzej Kremer and a number of passengers and crew members.

During the flight, the crew was in contact with air traffic controllers in Minsk, Moscow, and Smolensk. The crew also was in contact with the crew of a Polish Air Force Yakovlev 40 passenger plane that had landed at Smolensk Air Base 90 minutes ahead of the Presidential flight.

At about 10:14 the flight descended through an altitude of 7500 m. Minsk Control radioed that the visibility at Smolensk Air Base was 400 m due to fog. The same conditions were transmitted to the crew when they contacted the controller at Smolensk.

About 10:25 the pilot of the Yak-40 on the ground at Smolensk radioed that horizontal visibility was 400 m and vertical visibility about 50 m. Shortly afterward they reported that an Ilyushin 76 transport plane had diverted to an alternate airfield after two attempts to land.

The crew continued preparations for an approach to runway 26 at the Smolensk Air Base. The cockpit door was open and during the approach, there were two passengers present on the flight deck.

Meanwhile, visibility worsened to 200 m. This information was transmitted to the crew at 10:37. The crew requested permission to carry out a ‘trial’ approach to decision height (100 m) and asked the controller to expect a go-around.

About 18 seconds before impact the terrain awareness and warning system (TAWS) sounded: “Pull up”, followed by an aural warning: “TERRAIN AHEAD”.

About 5 seconds before impact the autopilot and autothrottle were disconnected in order to execute a go-around.

The airplane contacted upsloping terrain at a distance of about 1100 meters from the runway and 40 m to the left of the extended centreline. The aircraft height at that point was 15 m below the level of the runway threshold.

The left-wing struck a large tree causing the airplane to roll inverted.

The Tu-154 crashed and broke up.

11 years ago today Polish Air Force Tu-154M jet crashed killing all 96 onboard including Polish President Lech Kaczynski
2010 Polish Air Force Tu-154 crash

Various conspiracy theories about the crash have since been in circulation, and are promoted by Law and Justice’s leaders Jarosław Kaczyński (twin brother to Polish President Lech Kaczyński) and his deputy, Antoni Macierewicz, who claim the crash was a political assassination. Polish and international investigations did not find any evidence supporting this claim.

Probable Cause of Smolensk air disaster

The immediate cause of the accident was the failure of the crew to take a timely decision to proceed to an alternate airdrome although they were not once timely informed on the actual weather conditions at Smolensk “Severny” Airdrome that were significantly lower than the established airdrome minima; descent without visual contact with ground references to an altitude much lower than minimum descent altitude for go around (100 m) in order to establish visual flight as well as no reaction to the numerous TAWS warnings which led to controlled flight into terrain, aircraft destruction and death of the crew and passengers.

According to the conclusion made by the pilot-experts and aviation psychologists, the presence of the Commander-in-Chief of the Polish Air Forces in the cockpit until the collision exposed psychological pressure on the PIC’s decision to continue descent in the conditions of unjustified risk with a dominating aim of landing at any means.

Contributing factors to the accident were:

  • long discussion of the Tu-154M crew with the Protocol Director and crew of the Polish Yak-40 concerning the information on the actual weather that was lower than the established minima and impossibility (according to the Tu-154M crew opinion) to land at the destination airdrome which increased the psychological stress of the crew and made the PIC experience a psychological clash of motives: on the one hand he realized that landing in such conditions was unsafe, on the other hand, he faced strong motivation to land exactly at the destination airdrome.
    In case of proceeding to an alternate airdrome the PIC expected a negative reaction from the Main Passenger;
  • lack of compliance to the SOP and lack of CRM in the crew;
  • a significant break in flights in complicated weather conditions (corresponding to his weather minima 60×800) that the PIC had had as well as his low experience in conducting non-precision approach;
  • early transition by the navigator to the altitude callouts on the basis of the radio altimeter indications without considering the uneven terrain;
  • conducting flight with engaged autopilot and autothrottle down to altitudes much lower than the minimum descent altitude which does not comply with the FCOM provisions;
  • late start of final descent which resulted in an increased vertical speed of descent the crew had to maintain.

The systematic causes of the accident involving the Tu-154M tail number 101 aircraft of the Republic of Poland were significant shortcomings in the organization of flight operations, flight crew preparation and arrangement of the VIP flight in the special air regiment.

In a separate investigation , the Polish Committee for Investigation of National Aviation Accidents concluded the following:

Cause of Accident:

The immediate cause of the accident was the descent below the minimum descent altitude at an excessive rate of descent in weather conditions which prevented visual contact with the ground, as well as a delayed execution of the go-around procedure. Those circumstances led to an impact on a terrain obstacle resulting in separation of a part of the left-wing with aileron and consequently to the loss of aircraft control and eventual ground impact.

Circumstances Contributing to the Accident:

1) Failure to monitor altitude by means of a pressure altimeter during a non-precision approach;
2) failure by the crew to respond to the PULL-UP warning generated by the TAWS;
3) attempt to execute the go-around maneuver under the control of ABSU (automatic go around);
4) Approach Control confirming to the crew the correct position of the airplane in relation to the RWY threshold, glide slope, and course which might have affirmed the crew’s belief that the approach was proceeding correctly although the airplane was actually outside the permissible deviation margin;
5) failure by LZC to inform the crew about descending below the glideslope and delayed issuance of the level-out command;
6) incorrect training of the Tu-154M flight crews in the 36 Regiment.

Conducive circumstances:

1) incorrect coordination of the crew’s work, which placed an excessive burden on the aircraft commander in the final phase of the flight;
2) insufficient flight preparation of the crew;
3) the crew‘s insufficient knowledge of the airplane’s systems and their limitations;
4) inadequate cross-monitoring among the crew members and failure to respond to the mistakes committed;
5) crew composition inadequate for the task;
6) ineffective immediate supervision of the 36 Regiment’s flight training process by the Air Force Command;
7) failure by the 36 Regiment to develop procedures governing the crew’s actions in the event of:
a) failure to meet the established approach criteria;
b) using radio altimeter for establishing alarm altitude values for various types of approach;
c) distribution of duties in a multi-crew flight.
8) sporadic performance of flight support duties by LZC over the last 12 months, in particular under difficult WC, and lack of practical experience as LZC at the SMOLENSK NORTH airfield.

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