Airport (less than 10 km from airport)

After takeoff from Estancia Las Cruces Airport, while climbing in foggy conditions, the aircraft lost height and impacted ground in a wooded area located about 3 km from the airfield. The aircraft was destroyed and the pilot, sole on board, was killed.

The aircraft departed Jaffna-Palaly Airport on a flight to Colombo, carrying mostly Marines officers. While in cruising altitude, the pilot reported an engine fire and diverted to Anuradhapura Airport. On approach, the aircraft went out of control and crashed in a wooded area located 14,5 km from the airport. The aircraft was totally destroyed and all 40 occupants were killed.

The flight was approaching a private airport (elevation 983 feet msl), that did not have an instrument approach system, during instrument meteorological conditions. The pilot informed the air traffic controller that he had the airport in sight, and cancelled his instrument flight plan. The twin turbofan airplane impacted a tree approximately 4,000 feet northeast of the airport in an upright position. The airplane then impacted the ground in an inverted position approximately 200 yards from the initial impact with the tree. The weather observation facility located 16 miles northeast of the accident site was reporting an overcast ceiling at 400 feet agl, and visibility 4 statute miles in mist. The weather observation facility elevation was 541 feet msl. Local residents in the vicinity of the accident site stated that there was heavy fog and drizzle at the time of the accident. The pilot had filed an alternate airport (with a precision instrument approach); however, he elected not to divert to the alternate airport. Examination of the wreckage did not reveal any evidence of pre-impact anomalies that would have prevented operation of the airplane.

During the takeoff roll at Huambo-Albano Machado Airport, the pilot-in-command made a manoeuvre to avoid a hole in the runway when control was lost. The aircraft veered off runway, struck a ditch and came to rest, broken in two. Three passengers 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.

The captain was the flying pilot for the night landing on runway 01 in instrument meteorological conditions (IMC), with a right cross wind from 110 degrees at 14 gusting 18 knots, drizzle, and a wet runway. Prior to starting the approach, the flightcrew determined that the landing approach speed (Vref) and the approach speed (Vapp) were 122 and 128 knots, respectively. DFDR data showed the airplane flying on autopilot as it passed the middle marker at 200 feet AGL at 130 knots on the ILS approach. Approximately 3 seconds after the first officer called "runway in sight twelve o'clock," the captain disconnected the autopilot, while at a radio altitude of 132 feet and on a heading of approximately 18 degrees. Within approximately 11 seconds after the autopilot disconnect, the glideslope and localizer deviation increased. The first officer called "runway over there." Approximately 5 seconds before touchdown, the airplane rolled right, then left, then right. DFDR data-based performance calculations showed the airplane crossed the threshold at an altitude of 35 feet and 130 knots. The airplane touched down 2,802 feet from the approach end of the 5,495-foot runway (844- foot displaced threshold) at 125 knots on a heading of 10 degrees. The airplane overran the runway and struck a ditch 175 feet beyond the departure end of the runway. Landing roll calculations showed a ground roll of 2,693 feet after touchdown, consisting of 1,016 feet ground roll before braking was initiated and 1,677 feet ground roll after braking was initiated until the airplane exited the pavement. According to Saab, for a wet runway, the aircraft would have needed 1,989 feet from the time of braking initiation to come to a complete stop. The American Eagle Airlines, Inc., FAA approved aircraft operating manual (AOM), states in part: Stabilized approaches are essential when landing on contaminated runways. Landing under adverse weather conditions, the desired touch-down point is still 1,000 feet from the approach end of the runway. Touchdown at the planned point. Cross the threshold at Vapp, then bleed off speed to land approximately Vref -5. Use reverse, if needed. To achieve maximum braking effect on wet runway, apply maximum and steady brake pressure. In 1992, the City of Killeen submitted a proposal that included extending the north end of runway 01 by 194 feet. The FAA originally disapproved the proposal, in part, because the runway extension decreased the length of the runway safety area (RSA) which was already shorter than the recommended 1,000 feet for a 14 CFR Part 139 certificated airport. The proposal was subsequently approved and a drainage ditch was installed in the north RSA, perpendicular to the runway and approximately 175 feet north of the departure end of runway 01. In 1993, the airport received FAA Part 139 certification. The 1998 and 1999, FAA airport certification inspection reports noted the inadequate RSA; however, neither letter of correction, sent from the FAA to the City of Killeen following the inspections, mentioned the RSA. Following this accident, the ILS runway 01 was flight checked by the FAA and all components were found to be operating within prescribed tolerances. Examination of the airplane found no anomalies that would have prevented it from operating per design prior to departing the runway and encountering the ditch.

On final approach to Bursa-Yenisehir Airport, the pilot encountered poor weather conditions. Due to low visibility, he was unable to establish a visual contact with the approach and runway lights and initiated a go-around procedure. While completing a circuit, the twin engine aircraft struck the top of a hill located near the airport and crashed. A passenger was killed while four other occupants were injured.

The aircraft was completing a humanitarian flight to Goma on behalf of the United Nations Organization. On final approach, at a distance of 1,000 metres from the runway threshold, the aircraft encountered windshear. The captain initiated a go-around procedure but the aircraft continued to descent until it struck the ground and crashed to the right of the runway. All 10 occupants were injured and the aircraft was destroyed.

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.