Technical failure

Shortly after takeoff from Belo Horizonte-Pampulha Airport, while in initial climb, the left engine failed. The pilot lost control of the aircraft that rolled to the left, lost height and crashed onto four houses located in the district of São Bernardo near the airport. The aircraft and four houses were destroyed. All three occupants were killed and two other people on the ground were injured.

The twin engine aircraft departed La Paz-El Alto Airport on a flight to Santa Cruz, carrying two pilots and two technicians. After takeoff, the crew declared an emergency after the right engine failed during initial climb and was cleared to return. On final, the aircraft crashed 500 metres short of runway, bursting into flames. All four occupants were killed.

The Sky Cabs flight SCB701 originated in Colombo (Bandaranaike International Airport Colombo - hereinafter known as BIA Colombo), Sri Lanka at 1940 hours on 23rd March 2000. It landed in Bangkok, Thailand at 0120 hours on the following day after an uneventful flight. The alternate airport for Bangkok was Rayong/Ban U-Taphao (VTBU). The crew had recent experience in operating AN 12 flights between BIA Colombo and Bangkok International Airport, Thailand. The same flight crew made the return flight back to BIA Colombo after 4 hours and 20 minutes ground time in Bangkok. The crew had received the weather report from Aero Meteorological Division (AMD), prior to departure. An air traffic control flight plan was filed to BIA Colombo, the filed alternate airport was Male International (VRMM) in the Republic of Maldives. The aircraft was refueled adding 6681 kgs of fuel to the remaining 8300 kgs bringing the total fuel onboard to 14981 kg. Flight SCB702, cargo flight, departed Bangkok at 0540 hours on 24th March 2000 to BIA Colombo. The scheduled flight time for Bangkok – BIA Colombo was five hours and twenty minutes with a scheduled time of arrival of 1100 hours (17:00 hours Sri Lanka time). SCB702 made the first radio contact with Sri Lanka air traffic control at 1016 hours. The area controller passed SCB702 the latest weather report effective for BIA Colombo and later, a Sigmet valid at the time. When the control of the flight was handed to the approach radar controller (Director) by the area controller, at 1042 hours SCB 702 was asked to report his radial and DME from Colombo, (i.e. from “DVOR/DME KAT”). SCB702 reported as saying “074 radial and 55 DME ready for descent”, thus the two-way communication was established. Later, the flight SCB702 made two unsuccessful ILS approaches to runway 04. While on a radar heading to get established on the ILS to Runway 22 for a third attempt to land, the aircraft crashed 1.2 N.M. north-northwest of the threshold of Runway 22 (3.2 N.M. north-northeast of the DVOR/DME 'KAT') at BIA Colombo at 1204 hours (or 1804 hours in the evening, local time) on 24th March 2000. Six crew members and three people on the ground were killed.

During the takeoff roll on runway 25 at Randers Airport, the right engine lost power then failed. The pilot continued the takeoff procedure and completed the rotation. Just after liftoff, while in initial climb, smoke spread from the right engine into the cockpit. The pilot attempted an emergency landing when the aircraft crash landed, collided with trees and came to rest about 500 metres past the runway end. The pilot escaped uninjured and the aircraft was damaged beyond repair.

En route from Arequipa to Juliaca, the crew encountered technical problems with the right main landing gear that was jammed and remained blocked in its main wheel well. The crew attempted to lower the gear manually but as this was impossible, he decided to divert to Tacna for an emergency landing. The airplane landed 280 metres past the runway 20 threshold. After touchdown, the airplane veered to the right and came to rest 600 metres after landing. All 65 occupants evacuated safely. The airplane was not repaired.

On the day of the accident, the aircraft was engaged in a charter operation for the Central Bank of Nigeria. The first segment of the flight (Lagos - Abuja) was flown by the Commander. The aircraft departed Lagos about 0630 hours UTC and initially at cruise, the crew had a momentary problem setting power on the starboard engine after which the flight continued normally to Abuja. The aircraft which departed Abuja for Jos at 0900 hours UTC had 6 souls on board, 5 hours endurance with the first officer at the controls. At FL 90 and about 30NM from Abuja, the crew again had problems with the cruise power setting on the starboard engine. The torque remained at 1400. The crew retarded the right power lever to the minimum with the aim of achieving a cruise setting of 1300 but the gear warning came on. The Commander at this stage took over the controls from the first officer. At 0923 hours UTC, the aircraft contacted Kaduna Tower that it would be diverting to Kaduna as against its scheduled destination giving its flight level as 90 at a distance of 61 miles and estimating TMA at 24 miles, 'KC' at 41 miles, 6 souls on board and 5 hours endurance at departure. The tower then gave the aircraft an inbound clearance to 'KC' locator maintaining FL 90 and to expect no delay for a locator approach runway 05. Weather report at 0900 hours UTC was also passed to the aircraft as wind 090/05 knots, QNH 1014 and temperature 30°c. At 0928 hours UTC the airplane at about 42 miles, speed between 150-160 kts, requested descent and was cleared to 4,500H, QNH 1014. At about 0935 hours UTC, the pilots contacted tower that they would make a single engine approach because they were having problems controlling power on the starboard engine and it would be shut down. The tower in response, asked whether they would need fire coverage on landing to which the pilots affirmed. The commander then reviewed the single engine approach with the first officer estimating 4,500 ft at 8NM. Approaching 4,500 ft at 11 NM, the crew initiated right engine shut down after which the speed was decayed from 150 to 140 kts. At 0946 hours UTC, the pilot reported 6nm final and field in sight while the tower requested hire to report 4 miles final. Shortly, the controller reported having the aircraft in sight and subsequently cleared it to land on runway 05 giving wind as north easterly 06 knots. Descending at 500ft/min, the commander requested for 25% of flap when the first officer selected full flap. Shortly, the speed started decaying and bleeding faster. When the aircraft was at 2,700 ft high, the speed had already decayed to between 100 - 110 kts. The crew applied full power on the port engine to arrest the speed decay but to no avail . The pilot was trying to correct the descent rate, speed decay and the asymmetry when the stall warning came on. At this juncture, all effort by the controller to establish further contact with the airplane proved abortive. Suddenly, the controller observed a gust of dust in the atmosphere which gave him an indication that the aircraft had crashed. The aircraft crashed into the new VOR/DME site being constructed about 1175m from the threshold of runway 05. Time of accident was 0947 hours UTC.

En route from Gaborone to Maun, an oil leak occurred on the left engine. The pilot shut down the left engine and feathered its propeller. Unable to maintain a safe altitude, he elected to make an emergency landing but eventually crash landed in a wooded area located about 128 km southwest of Pandamatenga. All five occupants were injured and the aircraft was destroyed. It was reported that the left engine oil pressure dropped while its temperature increased.

On February 16, 2000, about 1951 Pacific standard time, Emery Worldwide Airlines, Inc., (Emery) flight 17, a McDonnell Douglas DC-8-71F (DC-8), N8079U, crashed in an automobile salvage yard shortly after takeoff, while attempting to return to Sacramento Mather Airport (MHR), Rancho Cordova, California, for an emergency landing. Emery flight 17 was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 121 as a cargo flight from MHR to James M. Cox Dayton International Airport (DAY), Dayton, Ohio. The flight departed MHR about 1949, with two pilots and a flight engineer on board. The three flight crew members were killed, and the airplane was destroyed. Night visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules (IFR) flight plan.

While taxiing for departure at Dakar-Yoff Airport, the left main gear unsafe alarm came on in the cockpit panel. The captain decided to return to the apron to proceed to an inspection when the left main gear collapsed. The engine n°1 struck the ground and partially torn off. A fire erupted and quickly spread to the left wing. All 182 occupants evacuated safely but the aircraft was considered as damaged beyond repair. It just came out from a C Check maintenance program.

The crew departed Mexico City-Benito Juarez Airport on a local post maintenance test flight. After takeoff, while in initial climb, both engines lost power simultaneously. The crew attempted an emergency landing on a soccer field when the aircraft crash landed near a motorway. Both pilots escaped uninjured while the aircraft was damaged beyond repair.