Landing (descent or approach)

The aircraft was completing a humanitarian flight on behalf of the United Nations and was carrying 28 passengers, 4 crew members and various goods. On short final, at low height, the aircraft nosed down and struck the ground few metres short of runway threshold. Out of control, the aircraft came to rest few dozen metres further. Fifteen occupants were injured, 16 others escaped uninjured and one passenger died.

After landing on wet runway 09, the aircraft was unable to stop within the remaining distance. It overran, lost its nose gear and came to rest 100 metres further. All 58 occupants escaped uninjured while the aircraft was damaged beyond repair. A thunderstorm just passed over Yogyakarta Airport before the flight SG416 arrived from Jakarta and the approach was completed in a 30° flaps down configuration. Apparently, the braking action was poor.

A Cessna 208B struck a ridge line about 14 miles from the destination airport. The pilot reported to atc he had the airport in sight from 7,000 feet msl more than 30 miles away. A weather reporting station located 5 miles east of the accident site was reporting two cloud layers; a scattered layer at 1,500 feet agl, and a broken layer at 5,000 feet agl. The airplane was descending after the pilot was cleared for a visual approach. The airplane collided with a tree and the ground in a wings level attitude at an elevation of 1,500 feet msl. There was no evidence of mechanical failure or malfunction found with the airplane.

On 11 January 1995, at 0035 Pacific standard time (PST), the twin-engine Learjet 35 departed Vancouver International Airport, British Columbia, on a night, instrument flight rules (IFR), medical evacuation (MEDEVAC) flight to the Masset aerodrome, on the northern end of the Queen Charlotte Islands. On board the Learjet were a flight crew of two pilots, and a medical team consisting of two attendants and a doctor. Their mission was to evacuate a patient from Masset and deliver her to Prince Rupert for treatment; the aircraft was then to return to Vancouver. The flight-planned route was at flight level (FL) 390, direct to Sandspit then direct to Masset. Following routine communications with Air Traffic Services (ATS), at about 0144, the aircraft reported "outbound" from the Masset non-directional beacon (NDB) on the published NDB "A" instrument approach procedure to runway 12. Air Traffic Control (ATC) radar, situated near Sandspit, tracked the aircraft as it flew the approach. Radar data shows that the aircraft began a descent about 10 seconds after it had completed the procedure turn and was established on the final inbound approach track. Forty-three seconds later, at a point 8.8 nautical miles (nm) from the threshold of runway 12 and on the final, inbound track, the aircraft disappeared from radar. Department of National Defence (DND) Search and Rescue (SAR) aircraft began searching the area shortly after the aircraft was declared missing, and were later assisted by other private and military aircraft and vessels. On the second day of the search, flotsam from the aircraft was found in the area. Extensive underwater searching using sonar and underwater cameras found the aircraft wreckage on 31 January 1995, in 260 feet of water, near the last known position. The aircraft had been destroyed. The bodies of two occupants were found several days after the accident, but the other three occupants have not been found and are presumed to have been fatally injured. The accident occurred at latitude 54/08NN and longitude 131/58NW, at about 0149 PST, during the hours of darkness in unknown weather conditions.

During an international cross country flight the private pilot, certificated single engine land, experienced a dual engine power loss as he was being vectored to the Brownsville Airport. Following the accident the aircraft was examined by a Federal Aviation Administration inspector who found that there was fuel in the left fuel tank and that the fuel selector was in the right tank position. The pilot had reported, prior to loss of engine power, that he had low fuel indications in the right tank and that he needed a vector to Brownsville. The aircraft was landed in rough and uneven terrain, resulting in damage to the structure and wings, approximately 1/2 mile short of the runway.

During climb to cruise the pilot reported a power loss on one engine and received vectors for a return to the departure airport. The pilot was subsequently cleared for the VOR-A approach and reported intercepting the inbound radial. The impact site was right of the inbound radial and short of the extended runway centerline. Weather at the airport was VFR. Post impact fire damaged the airplane. The left engine propeller was in the feather position. Visual and metallurgical examination confirmed the turbocharger shaft separated due to fatigue. The shaft contained chromium. The aircraft overhaul manual states that 'chrome plating...restoration of the shaft...are not permitted.' Metallographics revealed a microstructure of grey iron (automotive application) in the center housing. The turbocharger was overhauled and installed on the left engine in october 1989. All three occupants were killed.

The approach to Kinshasa-N'Djili Airport was completed in poor weather conditions. For unknown reasons, the aircraft landed hard and nose first. Upon impact, the nose gear collapsed and the aircraft came to rest. There were no casualties but the aircraft was damaged beyond repair.

The approach to Sarajevo was completed in marginal weather conditions with strong winds and rain falls. After touchdown, the aircraft was unable to stop within the remaining distance, overran and eventually collided with military installations. All six crew members escaped uninjured while the aircraft was damaged beyond repair.

While descending to Van-Ferit Melen Airport, the crew encountered poor weather conditions with a limited visibility due to heavy snow falls. While on a VOR/DME approach to runway 03, the crew was unable to establish a visual contact with the runway and decided to initiate a go-around. Due to general conditions at destination, the captain decided to return to Ankara but eventually attempted a second approach. Few minutes later, as the visibility dropped to 300 metres, the crew was forced to initiate a second go-around. During the third approach, the crew failed to realize his altitude was too low when the aircraft struck a snow covered hill (70 metres high) located about 4 km from runway 03 threshold and crashed. Five crew members and 52 passengers were killed while 19 other occupants were seriously injured. The aircraft was destroyed. At the time of the accident, the visibility was below minimums.

The Boeing 737, named "Oasis" was owned and operated by Air Algerie and had been leased by Phoenix Aviation in order to operate a series of live animal export flights from the UK to France and the Netherlands. On December 21, at 06:42 the plane departed from Amsterdam for a flight to Coventry. Weather at Coventry worsened and when arriving near Coventry, the RVR for runway 23 was 700 metres. The aircraft was not able to receive the Coventry runway 23 ILS as its dual navigation receiver system was not to an updated 40 channel ILS standard, so an SRA approach was flown. The radar guidance was completed at 0,5 miles from touchdown; the commander decided to discontinue the approach and execute a go-around. A holding pattern was then taken up at 07:44. When holding, the RVR further reduced to 600 m and the flight diverted to East Midlands to wait on the ground for weather improvement. The aircraft landed there at 08:08. At around 09:00 weather conditions improved to 1200 m visibility and an overcast cloud base at 600 feet. The flight departed East Midlands at 09:38 and climbed to FL40. Approaching Coventry, the crew received radar vectors for a runway 23 approach. After some initial confusion about the heading (the controller wanted the crew to turn left for 010°, while the crew understood 100°) the turn was continued to 260° and the SRA approach started at 12 miles from touchdown. The aircraft descended below the Minimum Descent Height (MDH) for the approach procedure and collided with an 86 feet high (291 feet ams) electricity transmission tower (pylon) which was situated on the extended centreline of the runway, some 1.1 miles from the threshold. The collision caused major damage to the inboard high lift devices on the left wing and the left engine. The consequent loss of lift on the left wing and the thrust asymmetry, caused the aircraft to roll uncontrollably to the left. When passing through a wings vertical attitude, the left wingtip impacted the gable end of a house. The aircraft continued rolling to an inverted attitude and impacted the ground in an area of woodland close to the edge of the housing conurbation. An intense fire ensued.