Airport (less than 10 km from airport)

On final approach to Heglig Airport, at a height of about 60 feet, the aircraft collided with a flock of birds coming from the right side. The engine n°4 failed, the aircraft rolled to the right, lost height and struck the ground short of runway threshold. Upon impact, the undercarriage were torn off and the aircraft crash landed. All four crew members escaped uninjured while the aircraft was damaged beyond repair.

After landing on runway 24 at Kinshasa-N'Djili Airport in poor weather conditions, the aircraft went out of control, veered off runway to the right, lost its right main gear and came to rest few dozen metres further. All three crew members escaped with minor injuries while the aircraft was damaged beyond repair. Weather was poor at the time of the accident with heavy rain falls and crosswinds.

At 23:40 UTC / 08:40 LT (WIT) on Sunday April 21, 2002, the ES-NOP departed Sentani Airport, Jayapura, bound for Wamena. The aircraft, an Antonov AN-72, was being operated by PT Trigana Air Services as a cargo carrying charter transport flight. The flight crews of four included three cockpit crew personnel and a loadmaster. The flight was the third flight of eight flights planned for the day between Sentani Airport and Wamena airport. The first flight departed Sentani airport at 21:05 UTC / 06:05 LT. Arriving at Wamena at 21:40 UTC / 06:40 LT. The return flight from Wamena bound for Sentani, departing Wamena at 22:22 UTC/ 07:22 LT arrived at Sentani at 22:52 UTC/07:52 LT. The flights were reported normal, and the weather along the route was reported clear. The third return flight, from Sentani to Wamena departed Sentani at 23:40 UTC / 08:40 LT carrying a load of 7,481 kg. The weather at Jayapura and along the route was clear. The cruise altitude during the flight was 16,000 ft. After waypoint ‘Maleo’ the airplane over-flew the so called ‘north-gap’ and the descent was initiated while passing the ‘pass valley’. Three other airplanes were reported to be in the area, one Fokker F27 PK-YPQ which was enroute from Wamena airport to Jayapura, and two Antonov A26 aircraft, registration ER-AFQ and ER-AFE. Flying over ‘Yiwika’ 7 Nm from Wamena airport, and descending through 12,000 ft with speed of 330 km/hr, the ES-NOP overtook the ER-AFE. The flight crew had the runway in sight. The PIC acting as pilot flying, flew an ‘S’ approach pattern during the final flight path of Wamena airport. (arriving Wamena 24:15 UTC/09:15 LT). On final and at an altitude of 100 meters, the airplane was lined up to the runway 15-center line. The airplane touched down while still within the touchdown zone. The airplane bounced twice, the second and last bounce reported to be more severe than the first one. The airplane rolled down the runway, with the flight crew noticing an unusual nose down attitude. The PIC/Pilot Flying applied reverse power and brakes, controlling the aircraft by using rudder inputs. During the roll, the loadmaster, sitting behind the PIC’s seat saw black smoke coming from the floor of the forward side of the cargo compartment. The crew reported that the smoke hurt their eyes. The airplane decelerated with smoke emitted from the forward cargo compartment. After stopping, the loadmaster opened the airplane door taking the extinguisher to extinguish the fire. The PIC shut down the engines after the airplane came to a standstill then opened the left cockpit window. PIC then left the cockpit assisting the loadmaster extinguishing the fire, the F/O completed the shutdown procedure, as the smoke blocked out his vision. The Flight Engineer attempted unsuccessfully opened the overhead emergency exit. The F/O and Flight Engineer then evacuated through the left cockpit window, while the PIC and loadmaster exited through the door. Observing the occurrence, and as the crash bell was unserviceable, the ATC on duty called the Deputy Chief of the airport, and alerted the fire fighting brigade. The fire fighting personnel failed to start the fire truck, and after recharging the truck’s battery for about 10 minutes reattempt to start for a second time. This attempt again failed, and the battery was again recharged, while fire fighting personnel ran the airplanes final position carrying portable fire extinguisher. After another ten minutes of battery charging, the fire fighting truck was finally started, immediately proceeding to the accident site. After a refill of the fireextinguishing agent the fire was finally extinguished. Firefighting personnel extinguished the fire in about 30 minutes time. The airplane was seriously damaged, with the front side of the airplane completely burnt out, the fire cutting a hole from behind the cockpit roof until approximately the middle of the cabin in front of the roof. The cargo was totally consumed by fire. No one was injured during the accident. After the occurrence, Wamena airport was closed for Fokker 27 or bigger aircraft but opened for DHC-6 (Twin Otter) or smaller aircraft. The NTSC investigator team embarked to Wamena on that day (Sunday, April 21 2002). On Monday, April 22 2002, at 02.00 PM (LT), the investigator team give the clearance to remove the aircraft from the runway, at 05.00 PM (LT) the airport authority personnel started the efforts to removed the aircraft by big back hoe, at 08.30 PM (LT) ES-NOP has cleared from runway. On Tuesday April 23rd 2002, the Wamena airport activities back to normal as usual.

The aircraft was chartered to transfer groups of prisoners from Medellín to Popayán on behalf of the National Penitentiary and Prison Institute. Fifty prisoners just disembarked at Popayán Airport when the crew departed on a ferry flight to Medellín for a second similar rotation. Popayán Airport is located at an altitude of 1,733 metres and its runway is 1,906 metres long. For unknown reasons, the crew decided to start the takeoff procedure from the intersection, reducing the available takeoff distance to 910 metres. Also, the flaps were deployed to an angle of 25° instead of 15° and the engine power was set at 95% instead of 100% as stipulated in the company procedures for airport located above the altitude of 1,400 metres. During the takeoff roll, at a distance of 150 metres from the runway end, the pilot realized he could not make it so he rejected the takeoff procedure and started an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, struck trees and came to rest, broken in two. Three passengers were killed while five other occupants were injured.

During the takeoff roll from a dirt strip (3,900 feet long) at Ngerende, an impala crossed the runway. To avoid a collision, the crew pulled up the control column and started the rotation. Because the airspeed was insufficient, the pilot-in-command put the nose down to gain speed when the aircraft struck the ground and crash landed in a field. All 17 occupants were rescued, among them a passenger was slightly injured. The aircraft was damaged beyond repair.

During the flight from Skukuza to Pilanesberg the aircraft developed a hydraulic problem, resulting in a complete hydraulic failure. However, a safe landing was carried out at Pilanesberg on Runway 23. Shortly after the landing the pilot shut down both engines, but maintained the runway heading for approximately 2000m, before the aircraft veered off to the left of the runway where it entered a ditch, 75m from the runway edge, where it finally stopped. There were no injuries, but the aircraft sustained extensive damage and substantial damage was caused to the perimeter fence around the airport. Both the pilot and the co-pilot were correctly licenced and type rated on the aircraft. Apart from the CVR, which was inoperative at the time of the accident and a leaking L/H hydraulic pump, it would appear that the aircraft was correctly maintained. Fine weather conditions prevailed at the time of the accident. The pilot informed Pilanesberg ATC of a complete hydraulic failure, but did not declare an emergency. The pilot failed to switch off the Nose Wheel Steering after touchdown and also shut down both hydraulic cut-off switches. The Emergency Checklist does not provide for a complete hydraulic failure.

On April 15, 2002, about 11:21:17, Air China flight 129, a Boeing 767-200ER, operated by Air China International (Air China hereinafter), en route from Beijing, China to Busan, Korea, crashed during a circling approach, on Mt. Dotdae located 4.6 km north of runway 18R threshold at Busan/Gimhae International Airport (Gimhae airport hereinafter), at an elevation of 204 meters. The flight was a regularly scheduled international passenger service flight operating under instrument flight rules (IFR) within Korean airspace, according to the provisions of the Korean Aviation Act and Convention on International Civil Aviation. One captain, one first officer and one second officer, eight flight attendants, and 155 passengers were on board at the time of the accident. The aircraft was completely destroyed by impact forces and a post crash fire. Of the 166 persons on board, 37 persons including the captain and two flight attendants survived, while the remaining 129 occupants including two copilots were killed.

A series of parachute flights had been planned from Weston-on-the-Green. The forecast conditions were good, predicting a surface wind of 360°/10 kt, visibility 30 km, with no significant weather and some strato-cumulus cloud with a base of 3,000 feet. The first flight, which consumed 144 lb of fuel, was completed successfully with 12 parachutists jumping from 12,000 feet. Thirteen parachutists boarded for the second flight and the aircraft was cleared to take off from the dry surface of grass Runway 01 (take off run available 3,194 feet). The surface wind at the time was 360°/15 kt with no significant weather and the temperature was 15°C. The pilot subsequently reported that he checked the condition levers were set to 100% N2, the flaps were set to 10° and that the trim was set in the take off range. He also reported that the company recommended power of 738°C turbine outlet temperature (TOT), and 89 pounds per square inch (psi) manifold pressure were set and achieved during the take off run. This power setting was equivalent to the 'Max Cruise Rating' as specified in the 'Operating Limits' section of the aircraft manual and no take off performance charts or data concerning 'take off distance required' (TODR) and 'accelerate stop distance required' (ASDR) information was available. The maximum take off power available (5 minute limit) was 810°C TOT and 102 psi. At approximately 80 to 83 kt (scheduled rotation speed 71 kt) the pilot pulled back on the control column. He reported that, 'the aircraft felt more nose heavy', 'the aircraft nose did not rise and he perceived that the aircraft was no longer accelerating'. He decided to abort the take off, commenced braking and set the condition levers to the full reverse position. As the aircraft decelerated he turned it to the right in order to avoid trees and bushes ahead. The aircraft struck a small earth mound, whilst still travelling at about 15-20 kt, and came to an abrupt halt. The pilot shut down both engines and selected the fuel and the battery to OFF. The crew and passengers evacuated the aircraft unaided.

The twin engine aircraft departed Madrid-Barajas Airport at 0338LT on a cargo flight to Palma de Mallorca, carrying two pilots and a load of 1,340 kilos consisting of various goods. On a night approach to Palm Airport runway 24L, the crew completed a last turn when the aircraft stalled and struck the runway surface. Out of control, it veered to the right, collided with a lightning system and came to rest upside down in a grassy area. The aircraft was destroyed and both pilots were killed.

Crashed upon takeoff for unknown reasons. There were no casualties.