Crash of a Piper PA-42-720 Cheyenne III off Grand Case: 4 killed

Date & Time: May 5, 2012 at 0240 LT
Type of aircraft:
Registration:
F-GXES
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Grand Case - Fort-de-France
MSN:
42-8001043
YOM:
1980
Flight number:
TIF520
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3950
Captain / Total hours on type:
513.00
Aircraft flight hours:
7593
Aircraft flight cycles:
7830
Circumstances:
The twin engine aircraft was engaged in an ambulance flight between Grand Case and Fort-de-France and was carrying a pilot, a nurse, a doctor and a patient, a Greek citizen in honeymoon in Saint Martin who suffered a heart attack. He normally should be transferred to Fort-de-France from Saint Martin-Princess Juliana Airport with another Operator but the aircraft suffered technical problem prior to departure and the patient was transferred to Grand Case Airport. Piper PA-42 left Grand Case-L'Espérance runway 12 at 02H39. One minute later, during initial climb, it lost height and crashed into the Caribbean Sea, some three NM off the airport, off Tintamarre Island. Around 1000LT in the morning, a wheel and some others debris were found floating in water and no trace of the four occupants was found. They were later considered as deceased.
Probable cause:
The French BEA said in its final report that no technical anomaly to affect significantly the performance of the airplane or its pitch control could be demonstrated. It appears that the pilot had consumed alcohol before the flight and was awake since 0630LT and did not sleep over 20 hours, which could affect his capabilities. In conclusion, the investigation did not determine the cause of the accident, but the following factors may have contributed:
- aircraft's operation with one pilot only,
- absence of regulation does not allow the Civil Aviation Authority to ensure the adequacy of the operational objectives of an operator and its capacity to maintain its activity. This failure could not ensure that the pilot was able to conduct the flight.
- the presence of a flight recorder would probably help to understand the circumstances of the accident with more precision. Important data failed to the investigation, which was not able to identify all possible measures to avoid a similar accident in the future.
Final Report:

Crash of a Socata TBM-700 in Cuers

Date & Time: Feb 10, 2012 at 1715 LT
Type of aircraft:
Operator:
Registration:
D-FALF
Flight Type:
Survivors:
Yes
Schedule:
Maribo – Cuers
MSN:
157
YOM:
1999
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8000
Captain / Total hours on type:
6000.00
Circumstances:
The pilot took off at around 14 h 45 from Maribo aerodrome (Denmark) bound for Cuers. He filed an IFR flight plan that he cancelled(2) at 17 h 15 near the St Tropez VOR (83). He explained that he had overflown the installations at Cuers at 1,500 ft and started an aerodrome circuit via the north for runway 11. He was visual with the ground and noted the presence of snow showers. He reckoned that these conditions made it possible to continue the approach. At about 600 ft, he went into a snow shower. At about 400 ft, he noticed that the horizontal visibility was zero and that he had lost all external visual references. He tried to make a go-around but didn’t feel any increase in engine power. At about 200 ft, he saw that he was to the right of the runway and decided to make an emergency landing. The aeroplane struck the ground on the right side of the runway. It slid for 150 metres and swung around before stopping. All three occupants escaped with minor injuries and the aircraft was damaged beyond repair.
Probable cause:
The accident was linked to the pilot’s to continue his approach under VFR, even though the meteorological conditions made it impossible. Coming out of an area of thick snowfall at 200 ft, he was unable to control the bank angle or the flight path of the aeroplane. The investigation was unable to determine if this bank angle was linked to inadequate control during an attempt to go around without external visual references(3) or a late attempt to reach the centre of the runway. Overconfidence in his abilities to pass through a snow shower, as well as a determination to land, may have contributed to the accident.
Final Report:

Crash of a Socata TBM-700 in Lyon: 1 killed

Date & Time: Nov 9, 2011 at 0912 LT
Type of aircraft:
Operator:
Registration:
N228CX
Flight Type:
Survivors:
No
Schedule:
Toussus-le-Noble - Lyon
MSN:
84
YOM:
1993
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2000
Circumstances:
The pilot departed Toussus-le-Noble Airport at 0810LT on an IFR flight to Lyon. After contacting ATC, the pilot was vectored for a LOC DME approach to runway 16 at Lyon-Bron Airport. He reported being established on localizer at 0907LT, then was transferred to the tower and was cleared to land. At 0910LT, he reported he was initiating a go-around procedure and was instructed to climb to 3,000 feet maintaining a straight-in path. ATC requested twice the pilot to confirm the approach interruption but he failed to respond. A few moments later, the pilot reported 'Now, I'm not good at all'. The airplane crashed in a retention basin located 1,500 meters short of runway 16 threshold, bursting into flames. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Loss of control while approaching at a speed close to stall speed in clouds without any external visual references, in a phase of flight where the pilot encountered difficulties. Investigations were unable to determine the exact cause of the loss of control and the reason why the pilot was unable to regain control.
Final Report:

Crash of a Piper PA-31T Cheyenne II in Toulouse: 4 killed

Date & Time: Oct 28, 2011 at 2135 LT
Type of aircraft:
Registration:
OE-FKG
Flight Type:
Survivors:
No
Schedule:
Kassel-Calden - Toulouse
MSN:
31-8020036
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1145
Captain / Total hours on type:
217.00
Aircraft flight hours:
7300
Aircraft flight cycles:
5434
Circumstances:
The pilot, accompanied by three passengers who were family members, took off at 1835LT from Kassel-Calden Airport (Germany) for a private flight under IFR to Toulouse-Blagnac. After about three hours of flight, he was cleared for approach and received radar vectoring for the runway 14R ILS. During the last exchange with the controller, as the aeroplane was on final at 900 feet, the pilot stated that he had a problem without specifying what type, as the message was interrupted. Shortly afterwards, radar and radio contact was lost. The wreckage was found close to the threshold of runway 14R. Two passengers were rescued while the pilot and another passenger were killed. The occupants were four members of the same family : the parents and two children, a boy aged nine and a girl aged 13. While the parents were killed upon impact, the daughter died from her injuries a day later and the boy died three days later.
Probable cause:
Causes of the Accident:
It is likely that during the final approach, a right engine anomaly, detected by the pilot, led to power asymmetry. As a result of a high workload, during the phase of deceleration and gear and flap extension, the pilot likely did not monitor the indicated airspeed, or noted a decrease in it. He may then have encountered difficulties in managing the power asymmetry before losing control of the aeroplane.
The following factors may have contributed to the accident:
- continuation of a fast arrival in a cloud layer, at night to a height of about 1,000 feet before configuring the aeroplane to land, which resulted in a significant increase in the pilot’s workload during processing of the anomaly;
- probable fascination with the objective given the proximity of the runway and the attraction induced by the approach lights;
- degraded type rating training to adapt to the pilot’s constraints during its renewal;
- absence of specific exercises relating to the conduct of a single engine approach at a speed close to VMCA, in the type rating training for single pilot multi-engine high performance aeroplanes.
Final Report: