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Crash of a Short SC.7 Skyvan 3 Variant 100 in Empuriabrava: 1 killed

Date & Time: Dec 28, 1993 at 1635 LT
Type of aircraft:
Operator:
Registration:
G-OVAN
Survivors:
No
Schedule:
Empuriabrava - Empuriabrava
MSN:
1892
YOM:
1971
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The twin engine aircraft departed Empuriabravia Airfield on a local skydiving mission. After all skydivers jumped, the pilot returned to the airport. On final approach, the pilot encountered engine problems and initiated a go-around procedure when the aircraft lost height, struck trees and crashed short of runway threshold. The pilot, sole on board, was killed.
Probable cause:
Failure of both engines on final approach caused by a fuel exhaustion.

Crash of a Pilatus PC-6/B2-H2 Turbo Porter near Peterborough

Date & Time: Dec 18, 1983 at 1042 LT
Operator:
Registration:
G-BIZP
Flight Phase:
Survivors:
Yes
Schedule:
Peterborough - Peterborough
MSN:
812
YOM:
1981
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2350
Captain / Total hours on type:
700.00
Circumstances:
The aircraft took off on the first flight of the day with eight parachutists, and a reported fuel load of 70 US gallons. At an altitude of approximately 11,000 feet it was decided that the cloud cover at that time was obscuring the dropping zone to an unacceptable degree, and so the detail was cancelled. During the subsequent descent, on rolling out of a left turn at about 4,500 feet, a bang was heard, and the left aileron was seen to have become partially detached. After a violent lateral oscillation of the control column lasting a few seconds, the right aileron also became partially detached. At this stage the parachutists successfully abandoned the aircraft on the orders of the pilot. The aircraft then adopted an angle of bank to the right of approximately 45° despite the application of full left rudder. The descent was continued until the pilot realized that the aircraft was approaching the village of Yarwell; he therefore applied engine power to ensure that the aircraft would clear the houses. The bank angle then increased to 60° and the aircraft struck the ground right wing low, coming to rest upright, and facing the opposite direction. The pilot sustained minor injuries, and there was no fire.
Probable cause:
Subsequent examination showed that, on each aileron, the centre of the three attachments to the wing had suffered an in-flight failure, leading to the subsequent detachment of one half of each aileron control surface. Detailed inspection revealed the presence of fatigue in each of the rear angle brackets, located within the wing, to which are attached the aileron supports. Preliminary indications are that the point of primary failure occurred at the left aileron rear angle bracket; the remaining brackets had failed subsequently as a result of overload.
Final Report:

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

Date & Time: Feb 15, 1981 at 1450 LT
Operator:
Registration:
G-BHCR
Flight Phase:
Survivors:
Yes
Schedule:
Sibson - Sibson
MSN:
732
YOM:
1970
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
580
Captain / Total hours on type:
21.00
Aircraft flight hours:
3570
Circumstances:
The aircraft was making a parachuting flight in fine weather and was being flown by a pilot who held a Private Pilot's Licence. Almost immediately after becoming airborne the pilot found he had to use both hands on the control column to counter a strong nose-up out of trim force. The aircraft gained about 250 feet in a semi-stalled condition, then yawed to the left and lost height until it struck the ground, suffering serious damage but no catching fire. Three of the nine parachutists on board received serious injuries and the other occupants received minor injuries.
Probable cause:
The accident was the result of loss of control of the aircraft following a takeoff with an incorrect horizontal stabilizer trim setting. Contributory factors were the incorrect loading of the aircraft, the difficulty of re-trimming the horizontal stabilizer rapidly and an inadequate standard of aircraft operation.
Final Report: