Landing (descent or approach)

The crew departed Madrid-Torrejón AFB on a training flight to Valladolid-Villanubla Airport. While descending to Valladolid Airport, the twin engine aircraft struck the slope of a hill located near La Cistérniga, about 20 km southeast of Villanubla Airport. All three crew members were killed.

After takeoff from La Ceiba-Goloson Airport, while in initial climb, the right engine failed. The crew was cleared for an emergency landing and initiated a circuit to return. At low height, one of the wing struck the roof of a house and the airplane crashed on a road. All 17 occupants were injured and the aircraft was damaged beyond repair.

On March 4, 1998, at 1350 hours Pacific standard time, a Learjet 23, N37BL, was substantially damaged when it landed gear up at the Oakdale, California, airport. The airline transport pilot and check pilot, the sole occupants, were not injured and no property damage occurred. The flight was operating under 14 CFR Part 91 on a familiarization and training flight. Visual meteorological conditions prevailed and no flight plan was filed. The pilot stated in his report "the landing gear was never extended and the aircraft was landed with the gear retracted."

After takeoff from Hoskins Airport, the stewardess informed the pilots about an explosion in the rear of the cabin. The crew returned to the airport for an emergency landing. After touchdown, the aircraft deviated to the left, veered off runway and came to rest in a ravine. All 13 occupants escaped uninjured while the aircraft was damaged beyond repair.

The pilot was performing a night VOR/DME approach during which instrument meteorological conditions prevailed. The airplane was equipped with VOR, LORAN, and RNAV receivers. There were two step-downs fixes on the approach. At 13 DME the minimum altitude was 1,800 feet. At 10 DME the minimum altitude was 1,040 feet. The missed approach point was at 6 DME, and the VOR/DME transmitter was located 5.5 miles beyond the airport. Radar data revealed a descent profile based upon distances from the end of the runway, rather than DME from the VOR. The airplane reached an altitude of 1,000 feet when it was 13.52 miles from the VOR, and 7.58 miles from the approach end of the runway. It subsequently impacted rising terrain at an altitude of about 900 feet, about 11.5 miles from the VOR, and 5.5 miles from the approach end of the runway. Impact damage and a post-crash fire precluded a check of the radio set up at the time of the accident. According to FAR 135 a pilot-in-command was required to have 1,200 hours total time. The investigation documented the pilot's total time as about 1,057 hours.

After landing at Mogadishu Airport, the propeller on the right engine went into fine pitch. The crew lost control of the airplane that veered off runway to the right. While contacting soft ground, the aircraft lost its undercarriage and its tail before coming to rest, broken in two. All 23 occupants evacuated safely and the aircraft was damaged beyond repair.

Few minutes after a night takeoff from Barcelona Airport, en route to Brussels, the copilot informed ATC about technical problems and was cleared to return for an emergency landing. After been cleared for an approach to runway 07, the crew descended to 6,000 feet and 3,000 feet successively. At 0000:15 seconds, the aircraft passed over the outer marker at an altitude of 1,500 feet and a speed of 170 knots. At a distance of six km from the runway threshold, the aircraft started to deviate from the approach path to the right and one minute later, it struck the ground at a speed of 130 knots, crashing in a palmgrove located 3,2 km short of runway and bursting into flames. The aircraft was destroyed by a post crash fire and both pilots were killed.

Following an uneventful flight from Denpasar-Ngurah Rai Airport, the aircraft was approaching Taipei-Taoyuan Airport by night and marginal weather conditions with a limited visibility of 2,400 feet, an RVR of 3,900 feet and 300 feet broken ceiling, 3,000 feet overcast. On final approach to runway 05L in light rain and fog, at the altitude of 1,515 feet, the aircraft was 1,000 feet too high on the glide so the captain decided to initiate a go-around procedure. The automatic pilot system was disconnected but for unknown reasons, the crew failed to correct the pitch up attitude. The aircraft passed the runway threshold at an altitude of 1,475 feet, pitched up go around thrust was applied. The aircraft rapidly pitched up, reaching +35° and climbed through 1,723 feet at an airspeed of 134 knots. The gear had just been raised and the flaps set to 20°. The aircraft continued to climb to 2,751 feet when the speed dropped to 43 knots. At this point, the aircraft stalled, entered an uncontrolled descent (pitched down to 44,65°). The crew was apparently able to regain control when the aircraft rolled to the right at an angle of 20° 2-3 seconds prior to final impact. The aircraft struck the ground 200 feet to the right of the runway 05L centerline and 3,7 km from its threshold and eventually crashed on 12 houses. The aircraft disintegrated on impact and all 196 occupants were killed, among them five US citizens, one Indonesian and one French. On the ground, seven people were killed.

While descending to Bursa Airport by night, the twin engine aircraft struck the slope of a mountain and was destroyed upon impact. All three occupants were killed.

The single engine aircraft was returning to Nairobi with one pilot and eight passengers who were returning to the capital city following a three-day safari and cinema trip. While descending to Nairobi-Wilson Airport, the pilot encountered poor visibility due to mist and failed to realize his altitude was insufficient when the aircraft struck the slope of a mountain located in the Ngong Hills, about 20 km southwest of Wilson Airport. The aircraft was destroyed upon impact and all nine occupants were killed.