Country
code

Haute-Savoie

Crash of a Cessna T303 Crusader in Annecy

Date & Time: Dec 4, 2020 at 1550 LT
Type of aircraft:
Operator:
Registration:
HB-LUV
Flight Type:
Survivors:
Yes
Schedule:
Marseille - Annecy
MSN:
303-00058
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1077
Circumstances:
The twin engine airplane departed Marseille-Provence Airport on a private flight to Annecy. En route, while cruising at FL110, the pilot was informed about the weather conditions at destination with a braking coefficient considered as medium due to a wet runway. After being cleared to land on runway 04, the pilot continued the approach but landed half way down the runway at a speed of 119 knots. After touchdown, he initiated the braking procedure but the airplane suffered an aquaplaning and was unable to stop within the remaining distance. It overran, impacted an embankment, went trough a fence and came to rest on a road. While both passengers aged 26 and 28 were slightly injured, the pilot aged 70 was seriously injured. The aircraft was destroyed.
Probable cause:
The accident was the result of the combination of the following factors:
- The pilot initiated the descent too late, causing the aircraft to approach well above the glide,
- The pilot continued the approach with an unstabilized airplane nor in speed nor on the glide,
- The airplane landed halfway down the runway, reducing the landing distance available,
- The speed upon touchdown was recorded at 119 knots, 30 knots above the recommended speed in the flight manual,
- The braking coefficient was considered as medium because of a wet runway surface,
- The airplane suffered an aquaplaning effect when the pilot initiated the braking procedure.
Final Report:

Crash of a Raytheon 390 Premier I in Annemasse: 2 killed

Date & Time: Mar 4, 2013 at 0839 LT
Type of aircraft:
Operator:
Registration:
VP-CAZ
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Annemasse - Geneva
MSN:
RB-202
YOM:
2007
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7050
Captain / Total hours on type:
1386.00
Aircraft flight hours:
1388
Aircraft flight cycles:
1404
Circumstances:
On Monday 4 March 2013, the pilot and two passengers arrived at Annemasse aerodrome (France) at about 7 h 00. They planned to make a private flight of about five minutes to Geneva airport on board the Beechcraft Premier 1A, registered VP-CAZ. The temperature was -2°C and the humidity was 98% with low clouds. The aeroplane had been parked on the parking area of the aerodrome since the previous evening. At 7 h 28, the Geneva ATC service gave the departure clearance for an initial climb towards 6,000 ft with QNH 1018 hPa towards the Chambéry VOR (CBY). At about 7 h 30, when the CVR recording of the accident flight started, the engines had already been started up. At about 7 h 34, the pilot called out the following speeds that would be used during the takeoff roll:
- V1 : 101 kt
- VR : 107 kt
- V2 : 120 kt.
At about 7 h 35, the pilot performed the pre-taxiing check-list. During these checks, he called out “anti-ice ON”, correct operation of the flight controls, and the position of the flaps on 10°.
Taxiing towards runway 12 began at 7 h 36. At 7 h 37 min 43, the pilot called out the end of the takeoff briefing, then activation of the engine anti-icing system. At 7 h 38 min 03, the pilot called out the start of the takeoff roll. Fifteen seconds later, the engines reached takeoff thrust. The aeroplane lifted off at 7 h 38 min 37. Several witnesses stated that it adopted a high pitch-up attitude, with a low rate of climb. At 7 h 38 min 40, the first GPWS “Bank angle - Bank angle” warning was recorded on the CVR. It indicated excessive bank. A second and a half later, the pilot showed his surprise by an interjection. It was followed by the aural stall warning that lasted more than a second and a further GPWS “Bank angle - Bank angle” warning. At about 7 h 38 min 44, the aeroplane was detected by the Dole and Geneva radars at a height of about 80 ft above the ground. Other “Bank Angle” warnings and stall warnings were recorded on the CVR on several occasions. Several witnesses saw the aeroplane bank sharply to the right, then to the left. At 7 h 38 min 49 the aeroplane was detected by the radars at a height of about 150 ft above the ground. At 07 h 38 min 52, the main landing gear struck the roof of a first house. The aeroplane then collided with the ground. During the impact sequence, the three landing gears and the left wing separated from the rest of the aeroplane. The aeroplane slid along the ground for a distance of about 100 m before colliding with a garden shed, a wall and some trees in the garden of a second house. The aeroplane caught fire and came to a stop. The pilot and the passenger seated to his right were killed. The female passenger seated at the rear was seriously injured. According to the NTSB and BEA, the airplane was owned by Chakibel Associates Limited n Tortola and operated by Global Jet Luxembourg.
Probable cause:
The pilot’s insufficient appreciation of the risks associated with ground-ice led him to take off with contamination of the critical airframe surfaces. This contaminant deposit then caused the aerodynamic stall of the aeroplane and the loss of control shortly after lift-off.
Final Report:

Crash of a Pilatus PC-6/B2-H2 Turbo Porter in Annemasse

Date & Time: Jun 26, 2001 at 1705 LT
Operator:
Registration:
F-GUAS
Survivors:
Yes
Schedule:
Annemasse - Annemasse
MSN:
557
YOM:
1963
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
919
Captain / Total hours on type:
520.00
Aircraft flight hours:
13000
Circumstances:
The pilot took off from Annemasse Airfield with nine skydivers on board. After dropping them at FL125, five to six seconds after initiating the descent, he felt strong vibrations. He reduced speed and saw the right out aileron separating from the wing. The pilot managed to maintain control of the aircraft by keeping the stick fully to the right and used the rudders to return to his departure aerodrome. He landed the airplane on the grass near the paved runway 30. During a hard landing, the right main landing gear broke off and damaged the fuselage. The pilot escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The accident was due to the loss of the right outboard aileron in flight. This loss was probably following the crack noticed by the pilot at the base of the right aileron balancing weight, which would have propagated in flight and would have then leads to tearing off the balancing weight. The accident resulted from the club pilots' decision to continue flying despite they have noticed the crack and that the manufacturer had advised them to stop flights.
Final Report:

Crash of a Piper PA-31P Pressurized Navajo in Annemasse

Date & Time: Dec 1, 1999
Type of aircraft:
Registration:
N38RG
Flight Type:
Survivors:
Yes
MSN:
31-7530007
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Too low on approach to Annemasse Airport, the twin engine aircraft struck the ground short of runway, lost its undercarriage and came to rest. The pilot, sole on board, was uninjured and the aircraft was damaged beyond repair.