Date & Time:
May 30, 2008 at 1545 LT
Type of aircraft:
Pilatus PC-6 (Porter & Turbo Porter)
Operator:
Registration:
EC-JXH
Flight Phase:
Flight
Flight Type:
Skydiving / Paratroopers
Survivors:
Yes
Schedule:
Lillo - Lillo
MSN:
700
YOM:
1969
Country:
Spain
Region:
Europe
Crew on board:
1
Crew fatalities:
1
Pax on board:
10
Pax fatalities:
1
Other fatalities:
0
Total fatalities:
2
Captain / Total hours on type:
150
Aircraft flight hours:
15833
Aircraft flight cycles:
26931
Circumstances:
The airplane had taken off from runway 30 at the Lillo (Toledo) Aerodrome for a local parachute drop. On board were the pilot and 10 skydivers, six of whom consisted of instructor-student pairs doing tandem jumps. When at an altitude of approximately 14,000 feet and having sounded the acoustic signal indicating two minutes to go before the jump, the airplane was subjected to an instantaneous and sharp negative acceleration that pushed two occupants against the ceiling of the aircraft. As soon as the airplane regained a normal attitude, the left wing fractured and detached. As a result, the airplane started to fall to the ground. Nine of the parachutists were ejected out and were able to open their parachutes at a sufficient enough altitude to land normally. The airplane eventually impacted the ground and burst into flames at a site located 4.5 km north of the aerodrome. The fire destroyed the area between the firewall and the aft end of the passenger cabin. The pilot and one parachutist were unable to exit the aircraft and died on impact. Several components, including the detached wing and its control surfaces, as well as part of the horizontal stabilizer, were thrown off and found between 1.5 km and 2.5 km to the northeast of the main crash site.
Probable cause:
The accident took place as the aircraft was entering an area of strong turbulence inside a storm. The aircraft was turning left to align with the heading used for the parachuting run, and as a result of the turn both the wing and the tail were subjected to loads in excess of design loads. This caused several of their components to fracture, resulting in the detachment of the left wing and the horizontal stabilizer. Contributing significantly to the accident is the fact that neither the company that operated the aircraft nor the jump supervisors were aware of the violent storm present to the north of the aerodrome, exactly over the area where the flight and the skydiving activity were going to take place.
Final Report:
EC-JXH.pdf2.95 MB
