Landing (descent or approach)

Crashed in unknown circumstances in a dry lake located in the region of Cabo San Lucas, while engaged in an illegal contraband flight. Nobody was found in the airplane that was carrying a load of cocaine. At the time of the accident, the aircraft had a false registration HK-4029X.

The crew was completing a local training flight at Shymkent Airport. On approach, at an altitude of about 300 metres, the instructor shut down one engine to simulate a failure. The pilot-in-command requested full power on the remaining engine but the flight engineer misinterpreted the instruction and shut down the second engine. The aircraft lost speed and height and struck the ground with a positive acceleration of 2,6 g before coming to rest in a field 1,100 metres short of runway threshold. All four occupants were injured and the aircraft was damaged beyond repair.

On October 29, 1995, about 2152 Universal Coordinated Time, a Cessna 340, N5736M, collided with the ground during an instrument landing system approach at Vienna, Austria. The airplane was operated by Austrian Cessna Aviation, Inc. under the provisions of 14 CFR Part 91, and instrument flight rules. Instrument meteorological conditions prevailed. An instrument flight rules flight plan was filed for the personal flight. The private, instrument-rated pilot, and the five passengers had minor injuries, and the airplane was destroyed by a post-crash fire. The flight departed Barcelona, Spain, about 1810 on the same day.

The aircraft was completing a cargo flight from Tyumen to Ufa, carrying seven passengers, six crew members, a car and a container. On approach to Ufa Airport, the crew encountered poor weather conditions (night, sleet and low clouds) and limited visibility. On short final, the aircraft struck trees 1,098 metres short of runway, lost height and crashed in a wooded area, some 179 metres to the right of the extended centerline, bursting into flames. Eight occupants were killed and five others were injured.

On final approach to Addis Ababa-Bole Airport, the twin engine aircraft collided with a white backed vulture of 5,4 kg. The windshield was broken and both pilots were seriously injured. Nevertheless, they elected to make an emergency landing when the aircraft crashed 300 metres short of runway. All 20 occupants were rescued, among them nine were injured.

While receiving radar vectors for an approach to land, the airplane (a Cessna 421C) departed controlled flight and impacted the terrain. Witnesses reported that they heard the engines operating before the plane crashed. During an investigation, no mechanical anomalies of the airplane were found. The pilot of a Boeing 727 reported that his airplane accumulated a 'quick load' of ice during his descent to land at the same airport within an hour of the accident.

Following an uneventful flight from Kadhdhoo Airport, the crew initiated the approach to Male Intl Airport. The copilot was the pilot-in-command. The aircraft landed on runway 36 at the speed of 95 knots some 600 metres past the runway threshold. After touchdown, the aircraft deviated from the centerline to the left and the copilot overcorrected, causing the aircraft to veer to the right. The captain took over control but this was too late. The aircraft overran, struck a concrete wall and crashed in the sea. All eight occupants were injured and the aircraft was destroyed.

Following an uneventful flight from Bern, the pilot started the descent to Zurich-Kloten Airport in relative good weather conditions (scattered 7,000 feet, visibility 5 km, wind from 340° at 4 knots and OAT 20° C). On short final to runway 14, the single engine aircraft entered an uncontrolled descent, struck the ground, lost its left wing and came to rest about 500 metres short of runway threshold. The pilot, sole on board, was killed.

The twin engine aircraft was completing a liaison flight from Campo de Mayo AFB in Buenos Aires and General Villegas. On approach to General Villegas Airport, the crew encountered very bad weather conditions with thunderstorm activity, heavy rain falls and turbulences. Control was lost and the aircraft crashed few km from the airfield, killing all four occupants. The aircraft had the dual registration GN-705 and LV-OIF (civil).

The single-engine turbine Otter on amphibious floats departed Triumph Bay, British Columbia, at 1634 Pacific daylight saving time (PDT) with one pilot and nine passengers on board for a visual flight rules (VFR) flight to Campbell River. At 19:01:59 the pilot called Campbell River Flight Service Station (FSS) and reported that he was seven nautical miles (nm) northwest of the airport, inbound for Campbell River. Radar data from Comox indicate that, when this call was made, the aircraft was actually 11 nm northwest of Campbell River, just south of the Narrows (see map, Appendix A). At 19:02:40, the pilot was given the 1900 PDT Campbell River weather observation, which was as follows: ceiling 300 feet overcast and visibility two miles in light rain and fog. The pilot requested a special VFR (SVFR) clearance to enter the Campbell River control zone. Clearance for SVFR was delayed by Comox air traffic control (ATC) until an instrument flight rules (IFR) aircraft on approach to Campbell River had landed. At 19:03:54, the IFR aircraft reported breaking clouds at 900 feet above sea level (asl), which would be approximately 550 feet above ground level, on the ILS approach to runway 11 at Campbell River (airport elevation is 346 feet). This information was acknowledged by the turbine Otter pilot. The IFR aircraft landed at 1904, and the turbine Otter was issued an SVFR clearance at 19:04:45. Radar data indicate that, at that time, the aircraft was about one mile northwest of Tyee Spit, a frequently used, alternate landing site (water) for company aircraft when weather conditions preclude landing at Campbell River airport. Radar data indicate that, at 1906, after passing by Tyee Spit, the aircraft turned southbound and flew directly toward the airport. At about 2 1/2 miles from the airport, at 19:07:40, the aircraft turned right to a heading of approximately 310/ magnetic and flew in that general direction for about two minutes. The aircraft was on a track that was approximately parallel to the extended runway centre line, tracking outbound from the airport with the localizer and the Campbell River (YBL) non-directional beacon (NDB) to the left. The aircraft passed abeam the YBL NDB, which serves as the final approach fix (FAF) for the ILS approach to runway 11, and continued outbound. At 19:09:40, at about three miles outside the beacon, the aircraft turned left to a southerly heading toward the localizer and the YBL NDB. At 19:10:08, the pilot radioed that he was seven miles northwest; this was the last transmission received from the aircraft. At 19:10:25, radar contact was lost. The aircraft crashed into the northwest side of a 1,047-foot mountain at about the 860-foot level, in straight-and-level flight on a heading of 183/ magnetic. The pilot and seven of the passengers received fatal injuries. The two remaining passengers received serious injuries. The accident occurred at 1910 PDT during the hours of official daylight, at latitude 50/01'N, longitude 125/22'W. Official sunset in Campbell River was at 1908, and night was at 1940 PDT.