Ambulance

The airplane departed U-Tapao Airport, Thailand, in the early morning, on an ambulance flight to Moscow-Zhukovsky Airport. Chartered by Gazpromavia, it was carrying four passengers and two crew members. A first fuel stop was made in Gaya, Bihar, and a second fuel stop was scheduled in Tashkent. After three hours and 45 minutes into the flight, while cruising at FL380 over the Afghan mountains, the crew declared an emergency and elected to divert to Kulob, southeast Tajikistan. Few minutes later, one of the engine failed, followed shortly later by the second one. In such conditions, the crew attempted an emergency landing when the airplane crashed on the slope of Mt Topkhana located in the province of Badakhshan, bursting into flames. Four people were rescued and two passengers were killed.

The airplane was operated on an ambulance flight from Valledupar to Bogotá-Guaymaral Airport, carrying six people, a mother and son, a doctor, a nurse and two pilots. After takeoff from runway 02/20, the airplane reached the altitude of 50 metres then stalled and crashed near trees, bursting into flames. Five occupants were injured and the doctor was killed. The airplane was destroyed by a post crash fire.

The crew of flight JL516 from Sapporo-New Chitose Airport was on a night approach to Tokyo-Haneda Airport Runway 34R when he was informed about traffic holding by taxiway C5. Weather conditions were considered as good. A De Havilland DHC-8-315Q MPA of the Japan Coast Guard was dispatched from Tokyo to Niigata, carrying a crew of six who were on a support mission of the victims of the recent earthquake in the north Peninsula. This crew was instructed by ground ATC to hold short at taxiway C5. After touchdown on runway 34R, the Airbus A350 collided with the Dash-8 that was aligned on the runway centerline. Upon impact, the nose gear of the Airbus was torn off and a violent explosion occurred. The Airbus caught fire, slid for approximately 2,400 meters then veered to the right and came to rest in a grassy area located near taxiway C11, about 200 meters from runway 16L threshold, bursting into flames. All 379 occupants evacuated the airplane, among them 15 were injured. The Airbus was later consumed by fire and totally destroyed. The Dash-8 was also totally destroyed by impact forces and a post crash fire. Among its crew of six, only the captain survived, critically injured. The five other crew members were killed. According to preliminary report released by the Japan Minister of Transport, the crew of JL516 have been cleared to land on runway 34R and the crew of the Japan Coast Guard Dash-8 have been instructed to hold short at taxiway C5. It was also reported that the stop bar lights for taxiway C1 to C14 were unserviceable since December 25 as per Notam published.

The crew was preparing for instrument flight rules (IFR) flight THU890 from Thunder Bay Airport (CYQT), Ontario, to Sault Ste. Marie Airport (CYAM), Ontario. The flight included a stop at Wawa Aerodrome (CYXZ), Ontario, to pick up a patient for a medical transfer to CYAM. As part of the pre-flight preparations, one of the flight crew members contacted CYXZ at 0549 to check the runway conditions and spoke with an aerodrome employee who was on duty for after-hour inquiries. During the call, the flight crew member learned of ongoing light snowfall and understood that the runway would be plowed by about 0730. At approximately 0653, during the hours of darkness, the aircraft departed CYQT for CYXZ with 2 flight crew members and a paramedic on board. The cruise portion of the flight was uneventful. The flight crew maintained radio contact with air traffic control (ATC) and received clearance for the approach to CYXZ. At about 0726, ATC instructed the flight crew to switch to the Wawa aerodrome traffic frequency (ATF). Between 0715 and 0730, aerodrome staff, including the employee to whom the flight crew member had spoken and a trainee, arrived at CYXZ. An ambulance carrying the patient who would be transferred also arrived at the aerodrome in that time. It had snowed overnight, and aerodrome staff were aware of the potential arrival of flight THU890, but had not yet plowed the runway. The staff began their morning duties, which included preparing the snow removal vehicles to clear the runway. There was no radio communication between aerodrome staff and the occurrence flight crew. The approach to CYXZ occurred during civil twilight,Footnote3 before sunrise. The flight crew activated the runway lights using the aircraft radio control of aerodrome lighting system and performed the RNAV (GNSS) [area navigation (global navigation satellite system)] approach to Runway 03. They visually spotted the runway when they were about 10 nautical miles away on final approach. As the aircraft approached the runway, the flight crew had a clear view of the runway lights and saw that the runway was covered in snow. The aircraft touched down on Runway 03 at 0739, and shortly after, it suddenly began sliding to the right. The flight crew attempted to correct this using rudder pedals, as well as differential propeller and power control, but were unsuccessful. The aircraft rotated almost 180° before sliding off the runway’s right side. The aircraft continued sliding sideways off the runway while facing the opposite direction of landing and came to rest on its left side in a drainage ditch, about 78 feet from the runway’s edge. The aircraft was extensively damaged; the right engine propeller blades penetrated the cabin before the engines were shut down. After the engines were shut down, the occupants began evacuating. The right emergency exit was damaged and would not open, so they egressed through the aircraft’s main door, which was located at the rear, on left side of the aircraft. A significant fuel leak was noted. The occupants walked the short distance to the runway, where the snow was between 6 to 8 inches deep on the runway surface. The flight crew called 911 and the London Flight Information Centre (FIC) to report the accident. The aerodrome staff observed the aircraft land and slide off the runway. They drove the snow removal vehicle down the runway, plowing snow along the way. They stopped to check on the occupants and then continued down the remaining runway length before turning around at the end and continuing to plow snow back toward the terminal building. Another vehicle transported the aircraft occupants to the terminal building, where they were assessed by emergency medical services and then transported to the local hospital for examination. There were only minor injuries.

The airplane departed Toluca-Licenciado Adolfo López Mateos International Airport on a positioning flight (Ambulance) to Cuernavaca, carrying two doctors and two pilots. After landing on runway 20 at Cuernavaca Airport, the crew initiated the braking procedure but the airplane was unable to stop within the remaining distance. It overran, went down a steep embankment and crashed in bushes, bursting into flames. The airplane was totally destroyed by impact forces and a post crash fire and all four occupants were killed. It is believed that the airplane landed too far down the runway, causing the landing distance to be insufficient.

The pilot, two medical crew members, and two passengers departed on the medical transport flight, which was operating on an instrument flight rules (IFR) flight plan in night instrument meteorological conditions (IMC). Onboard data and ADS-B flight track information showed that, between 1 and 3 minutes after takeoff, the autopilot disengaged and then reengaged; however, the airplane continued to fly a course consistent with the published departure procedure. About 11 minutes after takeoff, the airplane turned about 90° right, away from the next waypoint along the departure procedure, and remained on that heading for about 47 seconds. Around this time, the airplane’s autopilot was disengaged again and was not reengaged for the remainder of the flight. Also, about this time, the airplane’s previously consistent climb rate stopped, and the airplane maintained an altitude of about 18,300 ft mean sea level (msl) for about 20 seconds, even though the pilot had been cleared to climb to 25,000 ft msl. The airplane subsequently turned left to a northeasterly heading and climbed to about 19,400 ft msl before entering a descending right turn. Shortly after entering the right turn, the airplane’s rate of descent increased from about 1,800 ft per minute (fpm) to about 13,000 fpm, and the rate of turn increased before ADS-B tracking information was lost at an altitude of about 11,100 ft msl, in the vicinity of the accident site. The airplane crashed in a snow covered area located 32 km southeast of Reno-Tahoe Airport. The aircraft was destroyed and all five occupants were killed.

The medical transport flight was en route to pick up a patient on a neighboring island on an instrument flight rules (IFR) flight plan in dark night conditions over the ocean. About 13 minutes after departure, at 13,000 ft mean sea level (msl), the airplane’s vertical gyro failed, which subsequently failed the pilot’s Electric Attitude Director Indicator (EADI), which also caused the autopilot to disconnect. The failure of the EADI and autopilot disconnect required the pilot to manually fly the airplane using the copilot’s attitude gyro for his horizon information (bank angle and pitch attitude) for the duration of the flight. The pilot did not declare an emergency, nor did he inform air traffic control (ATC) that his electric attitude indicator had failed and that his autopilot had disengaged. After the instrumentation failure and autopilot disconnect, the airplane entered a series of right banks before being brought back to level, followed by a left turn, and then subsequent right banks. ATC asked the pilot to change course and the pilot agreed. The copilot attitude indicator indicated that the airplane entered a descending, steep right bank turn. Over the next 5 minutes, ATC issued varying instructions to the pilot. During this time, the airplane entered several right- and left-hand banks and rolls and descended 1,000 ft per minute (fpm), which increased to -3,500 fpm as the airplane’s airspeed increased. About 7 minutes after the instrumentation failure, the airplane was in a 65° bank angle when ATC asked the pilot to verify his heading. As the pilot responded, the airplane bank angle increased to 90° and the airspeed exceeded 260 knots. The bank angle and airspeed continued to increase; a loud metallic bang was recorded that was consistent with an in-flight separation of the empennage from the fuselage before impacting with the water. After an extensive underwater search, the main wreckage was located on the seabed at a depth of about 6,420 ft. The wreckage was recovered and transported to a facility for examination.

The airplane was returning to its base in San Fernando following an ambulance flight from Comodoro Rivadavia to Río Grande. Shortly after takeoff from Río Grande-Gobernador Ramón Trejo Noel Airport Runway 26, while in initial climb, the airplane rolled to the left, stabilized momentarily then rolled again to the left, lost lift and crashed in a huge explosion 1,870 metres pas the runway end and 300 metres to its left. The airplane was destroyed by impact forces and a post crash fire and all four occupants were killed.
Crew:
Claudio Canelo, pilot,
Héctor Vittore, copilot.
Passengers:
Diego Ciolfi, doctor,
Denise Torres Garcá, nurse.

The single engine airplane departed Kyzylorda on an ambulance flight to Aralsk, carrying one doctor and two pilots. En route, the crew encountered an unexpected situation and apparently attempted to make an emergency landing when the aircraft crashed in a desert area, coming to rest upside down and bursting into flames. All three occupants evacuated with minor injuries while the aircraft was totally destroyed by a post crash fire. Registration UP-A0279?

Beechcraft Super King Air B200GT aircraft, VT-MPQ belonging to the Directorate of Aviation, Government of Madhya Pradesh (DoA,GoMP) was involved in an accident on 06.05.2021 while operating a flight from Indore Airport to Gwalior. The flight was under the command of an ATPL holder with another CPL holder as Co-Pilot. There was one passenger on board in addition. The flight crew contacted ATC Indore for clearance to operate the flight to Gwalior. The aircraft was cleared for Gwalior via airway W10N and FL270. Aircraft departed from RWY25 at Indore and climbed to FL 270. Aircraft descended into Gwalior in coordination with Delhi and Gwalior. Approaching Gwalior the crew were advised by the ATC that RWY24L was in use. ATC then asked the crew if they would like to carry out a VOR approach for the opposite RWY 06R. The crew requested for a visual approach for RWY 06R in the night time and were cleared to descend 2700 ft and called field in sight at 25 NM. Crew then requested for right base RWY 06R and were cleared to circuit altitude. Crew called turning right base with field visual and were cleared to land which the crew acknowledged. Just before landing the aircraft and short of the threshold, the main gear collided with the raised arrester barrier and came to a halt on the Runway 06R just beyond the threshold markings at 1515 UTC. The aircraft was substantially damaged, however there was no post impact fire. The 2 crew and 1 passenger received minor to serious injuries.