Crash of a Beechcraft King Air 90 in Londrina

Date & Time: Dec 12, 2010 at 2140 LT
Type of aircraft:
Registration:
PT-WUG
Flight Type:
Survivors:
Yes
MSN:
LJ-1511
YOM:
1998
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Londrina-Governador José Richa airport in poor weather conditions, aircraft encountered windshear. It hit a small hill and eventually crashed in a field short of runway. All seven occupants injured and aircraft destroyed by fire.

Crash of a Beechcraft C90 King Air in Saint-Antonin-sur-Bayon: 2 killed

Date & Time: Nov 4, 2010 at 1620 LT
Type of aircraft:
Operator:
Registration:
F-BVTB
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Aix-les-Milles - Aix-les-Milles
MSN:
LJ-579
YOM:
1973
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9925
Captain / Total hours on type:
2100.00
Copilot / Total flying hours:
499
Copilot / Total hours on type:
1
Aircraft flight hours:
9716
Circumstances:
The twin engine aircraft departed Aix-les-Milles Airport at 1520LT on a local training flight. The crew was cleared to fly between 5,000 and 6,000 feet. The aircraft overflew successively Marseille and Toulon then passed over Le Castellet. While cruising at an altitude of 6,000 feet and at a speed of 110 knots, the airplane entered an uncontrolled descent, dove into the ground with a rate of descent of 6,000 feet per minute and crashed in a near vertical position in a rocky zone located in the Sainte-Victoire Mountain Range, near Saint-Antonin-sur-Bayon. The aircraft was destroyed by impact forces and a post crash fire and both occupants were killed, one instructor and one pilot under supervision.
Probable cause:
Loss of control during an exercise at low speed and certainly in a single engine configuration.
Contributory factors:
- No reference methods to conduct the exercise, for instructors on this type of aircraft,
- Exercise conducted in a height which insufficient margin and lower than the one recommended by the manufacturer,
- Insufficient vigilance on part of the instructor (however with unanimous recognized skills) but whose instruction on Beechcraft King Air 90 could not be established.
Final Report:

Crash of a Beechcraft 65-A90 King Air in Jacmel

Date & Time: Jan 23, 2010
Type of aircraft:
Operator:
Registration:
N316AF
Flight Type:
Survivors:
Yes
MSN:
LJ-214
YOM:
1967
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was apparently completing a cargo flight from Florida. Upon landing at Jacmel Airport, the undercarriage collapsed. The twin engine aircraft went out of control, veered off runway and came to rest against trees. Both occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Beechcraft C90GTi King Air in Les Éplatures

Date & Time: Jan 15, 2010 at 1407 LT
Type of aircraft:
Operator:
Registration:
HB-GPL
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Les Éplatures - Dole
MSN:
LJ-1936
YOM:
2009
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
920
Captain / Total hours on type:
62.00
Aircraft flight hours:
89
Aircraft flight cycles:
68
Circumstances:
The crew was departing Les Eplatures Airport on a training flight to Dole-Tavaux, Jura. During the takeoff roll on runway 24, the pilot-in-command realized that the aircraft' speed did not increase after 88 knots then dropped to 85 knots. He decided to reject the takeoff procedure and initiated an emergency braking procedure. Unable to stop within the remaining distance, the aircraft overran and collided with concrete blocks and the ILS equipment. All four occupants were injured, two seriously. The aircraft was damaged beyond repair.
Probable cause:
The accident was caused by a collision with obstacles after the runway end due to a late take off run interruption decision, most probably due to an involuntary braking action on behalf of the pilot.
The following contributing factors were identified:
- Poor pilot experience on this aircraft model.
- Inadequate take off configuration (flaps).
- Initial multi engine training performed on a different aircraft model.
- Pilot not familiarized with short runway.
Final Report: