Crash of a Partenavia AP.68TP-300S Spartacus off El Segundo: 1 killed

Date & Time: Jan 9, 1996 at 0914 LT
Type of aircraft:
Operator:
Registration:
N3116C
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oxnard - San Diego
MSN:
8007
YOM:
1987
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8963
Captain / Total hours on type:
1000.00
Aircraft flight hours:
4540
Circumstances:
The aircraft was destroyed after an uncontrolled descent into the Pacific ocean about 14 miles west-southwest of El Segundo, California. The pilot was presumed to have been fatally injured. According to a company search pilot, visual meteorological conditions prevailed at the accident area about 1.5 hours after the time of the accident. No flight plan was filed for the positioning flight which originated at Oxnard, California, on the morning of the accident for a flight to San Diego, California. The aircraft departed Oxnard on a special VFR clearance. The tops of the clouds were reported to be about 1,200 feet msl. The aircraft transitioned southbound through the NAWS Point Mugu airspace. The Point Mugu radar approach control monitored the aircraft on radar for about 25 miles. The pilot was subsequently given a frequency change to SOCAL Tracon. There was no contact made with that facility. A search was initiated when the aircraft failed to arrive at the intended destination. A review of the recorded radar data revealed the aircraft was level at 1,800 feet msl and then climbed to about 2,000 feet msl, at which time it disappeared from radar.
Probable cause:
Loss of control for undetermined reasons.
Final Report:

Crash of a Partenavia P.68B in Tangalooma

Date & Time: Nov 22, 1995 at 2110 LT
Type of aircraft:
Registration:
VH-TLQ
Flight Phase:
Survivors:
Yes
Schedule:
Tangalooma – Coolangatta
MSN:
33
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
905
Captain / Total hours on type:
57.00
Circumstances:
The aircraft was the second to take off in a stream of six on a night flight from the Tangalooma Resort strip to Coolangatta aerodrome. Shortly after takeoff it struck the ground, nosed over and was consumed by a fuel-fed fire. The take-off run appeared normal but the initial climb was shallow according to the witnesses, some of whom were pilots waiting their turn to take off. At about 150 ft above ground level the aircraft entered a descent which continued until ground impact, 164 m beyond the departure end of the strip. The nose gear collapsed at impact but the aircraft remained upright and skidded along the ground on its main gear and front fuselage. It traversed a low sand dune, fell 10 ft to the beach and overturned. The aircraft came to rest 112 m beyond the first ground contact. All four passengers were able to evacuate the aircraft which had started to burn. The pilot was rescued by her passengers.
Probable cause:
The following factors were reported:
1. The takeoff direction was dark and had no visible horizon.
2. The elevator trim was not set for takeoff.
3. The elevator load on takeoff was high.
4. The pilot did not monitor the aircraft attitude after lift-off.
5. The flap was retracted in one movement, increasing the elevator load.
6. The pilot may have been affected by somatogravic illusion to the extent that she thought the climb attitude was adequate.
Final Report:

Crash of a Partenavia P.68C on Mt Geitarhilđ: 1 killed

Date & Time: Jun 30, 1995 at 1416 LT
Type of aircraft:
Operator:
Registration:
TF-VEN
Flight Phase:
Survivors:
No
Site:
Schedule:
Reykjavik - Selfoss
MSN:
284
YOM:
1983
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
800
Captain / Total hours on type:
15.00
Aircraft flight hours:
2824
Circumstances:
The twin engine aircraft departed Reykjavik Airport on a schedule flight to Selfoss, Southern Region. While flying under VFR mode in IMC conditions, the pilot failed to realize his altitude was too low when the aircraft struck the slope of Mt Geitarhilđ located near Lake Kleif, about 20 km south of Reykjavik. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole on board, was killed.
Probable cause:
Controlled flight into terrain.
Final Report:

Crash of a Partenavia P.68C-TC Victor in Kampenwand

Date & Time: Mar 13, 1995 at 0645 LT
Type of aircraft:
Operator:
Registration:
D-GITY
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Munich - Hanover
MSN:
362-42-TC
YOM:
1985
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While cruising by night, the pilot failed to realize his altitude was insufficient when the twin engine aircraft struck trees and crashed in a snow covered wooded area located in the Bavarian Alps, near Kampenwand. All five occupants were injured.

Crash of a Partenavia P.68C near Serres: 2 killed

Date & Time: Oct 10, 1994
Type of aircraft:
Operator:
Registration:
PH-VDO
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Cannes - Rotterdam
MSN:
354
YOM:
1984
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While cruising in poor visibility due to low clouds, the twin engine aircraft struck the slope of a mountain located near Serres. The wreckage was found a day later and both occupants were killed.

Crash of a Partenavia P.68B Victor in Bodmin

Date & Time: Feb 7, 1993 at 1345 LT
Type of aircraft:
Operator:
Registration:
G-LOUP
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bodmin - Plymouth
MSN:
182
YOM:
1989
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9531
Captain / Total hours on type:
210.00
Circumstances:
The aircraft was attempting to takeoff from the grass runway 32 at Bodmin, for a flight to Plymouth. The commander reported that the ground was soft and wet, with the grass surface longer than normal, and that no flap was selected. The flight manual for the aircraft stated that performance takeoffs should be carried out with 15° flap selected. The aircraft failed to achieve sufficient airspeed to become airborne in the distance available, and overran the runway into an area of thick gorse and moorland. There was no fire, and both occupants, who were wearing lap and diagonal shoulder harnesses, were uninjured, and vacated the aircraft by the normal means.
Final Report:

Crash of a Partenavia P.68B Victor in Kalundborg

Date & Time: Sep 28, 1991 at 1110 LT
Type of aircraft:
Operator:
Registration:
OY-CEW
Flight Phase:
Survivors:
Yes
Schedule:
Kalundborg - Kalundborg
MSN:
30
YOM:
1974
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft successfully completed three sortie in the morning. With six skydivers on board, the pilot prepared for a fourth mission when, during the takeoff roll, he realized he could not make it. He aborted the takeoff procedure and saw people at the end of the runway so he voluntarily veered off runway to the right. While contacting soft ground, the nose gear collapsed and the aircraft came to rest with its left wing partially torn off. All six passengers were evacuated safely while the pilot was slightly injured.
Probable cause:
Takeoff interruption on part of the pilot due to an insufficient speed. The exact cause of the mishap remains unclear.

Crash of a Partenavia P.68C-TC Victor in Munich: 2 killed

Date & Time: Feb 10, 1991
Type of aircraft:
Operator:
Registration:
D-GANS
Flight Type:
Survivors:
No
MSN:
342-30-TC
YOM:
1984
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
On approach to Munich Airport, the pilot encountered strong crosswinds when the twin engine aircraft went out of control and crashed few hundred meters short of runway. Both occupants were killed.

Crash of a Partenavia P.68B in East Midlands: 1 killed

Date & Time: Oct 20, 1990 at 0332 LT
Type of aircraft:
Operator:
Registration:
G-BMCB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
East Midlands – Manchester
MSN:
156
YOM:
1985
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
926
Circumstances:
The twin engine aircraft departed East Midlands runways 27 on a ferry flight to Manchester. During initial climb by night, the aircraft entered an uncontrolled descent and crashed at a speed of 160 knots and disintegrated in a field near the airport. The pilot, sole on board, was killed.
Probable cause:
Loss of control during initial climb by night after the pilot suffered a spatial disorientation due to the combination of a poor visibility (night and low clouds) and the possible malfunction of the horizontal stabilizer due to water in the vacuum system.
Final Report:

Crash of a Partenavia P.68B Victor in Kolane

Date & Time: Oct 14, 1988 at 1845 LT
Type of aircraft:
Operator:
Registration:
VH-PFQ
Flight Type:
Survivors:
Yes
Schedule:
Kolane - Taroom - Kolane
MSN:
95
YOM:
1977
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Taroom aerodrome had recently been equipped with a pilot activated lighting (PAL) system which was due to be commissioned on the evening of 15 October 1988. The pilot, who is a local Council member had flown from his property "Kolane" to Taroom late in the afternoon, to check that the PAL system was functional. He had intended to fly to Taroom the following evening to activate the lights for the official opening celebration, which was planned to be held at the aerodrome. After checking that the system was working the pilot decided to take the opportunity to practice some night circuits and landings before returning to his property. Before departing Taroom he arranged to have two vehicles positioned at his property landing area to illuminate the strip which is 850 metres long, aligned 235/055 degrees magnetic, and 1000 feet above sea level. He apparently intended to check the suitability of the strip for a night landing on his return. The aircraft was observed to fly over the strip in a north-easterly direction and then make a left turn. The aircraft was then seen to descend and the sound of impact was heard by the occupant of a vehicle near the strip. The aircraft had impacted the ground whilst in a descending left turn at a ground speed of approximately 125 knots. Initial impact was in a clearing near trees. The aircraft slid 91 metres before the left wing struck a large tree and was torn off. The aircraft slid another 45 metres before coming to rest and catching fire. The pilot was thrown from the aircraft while still strapped to his seat and was able to move himself away from the immediate vicinity of the fire before help arrived.
Probable cause:
The pilot has no recollection of events immediately prior to the accident. There is no indication that the aircraft was not functioning normally at the time of the accident. The weather was fine, there was a light northerly breeze, and there was no moonlight. Indications are that the pilot may have become disorientated whilst attempting to carry out a visual circuit when there was no visual horizon. The landing area did not meet the requirements for night operations published in the Visual Flight Guide.
The following factor was considered relevant to the development of the accident:
The pilot was attempting to carry out a night visual circuit when there was no visual horizon.
Final Report: