Airport (less than 10 km from airport)

The single engine airplane departed Cremona-Migliaro Airport in the morning on a local skydiving flight, carrying eight skydivers and one pilot. This was the second sortie of the day. Once the altitude of 4,000 metres was reached, all eight skydivers successfully jumped out and the pilot started the descent to return to the airport. While descending to runway 11, the airplane collided with the eighth skydivers that hit the left wing and the vertical stabilizer. A large section of the left wing separated, causing the airplane to enter an uncontrolled descent and to crash in a cornfield located in Livrasco, about two km north of the airport. The pilot and the skydiver were killed. The airplane was totally destroyed.

While the airplane was in cruise flight and being flown by the copilot, the left engine fuel pressure fluctuated, which was followed by a brief loss of engine power. Concerned that the airplane might have a failed engine-driven fuel pump, the pilot turned the boost pumps to high and asked the passenger (the airplane’s mechanic) to open the fuel cross-feed valve. As the airplane approached its intended destination, both fuel pressure needles began to fluctuate. The pilot assumed that fuel starvation to the engines was occurring and decided to make an off-airport landing to a field behind their airplane’s position due to residential areas located between the airplane’s location and the airport. The pilot stated that he took control of the airplane from the copilot and initiated a right turn toward the field, and that, shortly afterward, both engines lost total power. During the landing roll, the pilot observed a ditch in front of the airplane and was able to get the airplane airborne briefly to avoid the first ditch; however, he was not able to avoid a second, larger ditch. Subsequently, the airplane struck the second ditch, became airborne, and impacted the ground, which resulted in substantial damage to the fuselage. Recovery company personnel reported that, during recovery of the wreckage, about 1 gallon of fuel was removed from the two forward and the two aft wing fuel tanks. Postaccident examination of the airplane revealed no evidence of any pre-existing anomalies that would have precluded normal operation of either engine except that all four main fuel tank fuel gauges displayed erroneous indications after each tank was filled with water. No leaks were observed throughout the fuel system. The airplane was last refueled on the day before the accident with 497.7 gallons. When the airplane was last refueled, the fuel tanks were reportedly filled to about 3 inches below the fuel filler neck. The investigation could not determine, based on the available evidence for this accident, how much of the airplane’s fuel load (maximum capacity was 670 gallons) the airplane had onboard after it was refueled. Additionally, the pilot reported that he commonly used a fuel burn rate of 150 gallons per hour for flight planning purposes; that figure included takeoff fuel burn. Recorded automatic dependent surveillance broadcast data showed that the airplane had flown for 4 hours 1 minute since refueling and included six takeoffs and five landings (but did not include taxi times). As part of the investigation, the pilot estimated that 485.9 gallons of fuel had been used since the last refueling. However, on the basis of the pilot’s initial planned fuel load and recorded flight times, the airplane would have used about 600 gallons of fuel. The pilot later submitted an estimated fuel burn for the flights since refueling of 485.9 gallons. The flight manual did not have fuel burn references for the exact power settings and altitudes flown; thus, the hourly fuel burn could not be determined. The pilot, copilot, and passenger did not visually verify the fuel levels in all four main fuel tanks before the accident flight. The pilot also underestimated the amount of fuel that would be used for the planned flights. As a result, fuel exhaustion occurred, which led to a total loss of engine power.

The aircraft departed Mogadishu-Aden Abdulle Airport on a cargo flight to Beledweyne, carrying four crew members and various goods on behalf of the AMISOM, the African Union Mission in Somalia. After takeoff, the crew informed ATC about hydraulic problems and was cleared to return. After touchdown on runway 05, the aircraft went out of control, veered off runway to the right and collided with a concrete wall. Two crew members were slightly injured while both pilots were seriously injured after the cockpit was severely damaged on impact.

The instructor pilot reported that while practicing an engine-out landing in the traffic pattern, the pilot-rated student overshot the turn from base leg to final rolling out to the right of the runway centerline. The student pilot attempted to turn back toward the runway and then saw that the airplane’s airspeed was rapidly decreasing. The instructor reported that when he realized the severity of the situation it was too late to do anything. The student attempted to add power for a go-around but was unable to recover. The airplane stalled about 10 ft above the ground, impacted the ground right of the runway, and skidded onto the runway where it came to rest. Both wings and the forward fuselage were substantially damaged. Both pilots stated there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

The crew was completing a local training flight at Belo Horizonte-Pampulha Airport, consisting of touch-and-go maneuvers. After landing on runway 13, the pilot-in-command decided to abort the takeoff. Unable to stop within the remaining distance, the aircraft overran, lost its landing gear and came to rest near a concrete block. All three occupants evacuated, among them the captain was slightly injured.

At 1541 hrs, the airplane took off from Marl-Lohmühle Airfield with the pilot and 2 passengers on board to a VFR flight to Arnsberg-Menden Airfield which is located approximately 30 NM to the south-east. One of the passengers was seated in the right-hand seat next to the pilot and the other in the passenger seat behind the pilot. The radar recording of the air navigation service provider showed that the airplane climbed up to 2,200 ft AMSL. Ten minutes after take-off, the pilot established radio contact with Dortmund Tower with the request to cross Dortmund Airport control zone via the reporting point WHISKEY towards reporting point ECHO on his way to Arnsberg. At 1552:14 hrs, the tower controller answered: “[…] melden Sie WHISKEY und dann erwarten Sie Durchflug nach Arnsberg oder ECHO, wie Sie möchten, QNH eins null null eins (report WHISKEY and then expect cross flight to Arnsberg or ECHO, as you like, QNH one zero zero one)“. The pilot confirmed QNH and approach point. At 1555:22 hrs, the pilot reported having reached reporting point WHISKEY at 2,200 ft AMSL. The controller approved the flight through the control zone towards the south. The GPS and radar data showed that at 1556 hrs, the airplane turned tight towards 120° to a direct heading to Arnsberg. At 1559 hrs, as the airplane had left the control zone the controller issued the clearance to leave Tower frequency. At 1600 hrs, about 2.5 NM west of the destination aerodrome, the airplane turned left towards the east. About one minute later the airplane intersected the extended runway centre line of runway 23 at a distance of 0.7 NM from the threshold with an eastern heading. At the time, ground speed was approximately 150 kt. At 1601:39 hrs, the airplane turned left towards the final approach of runway 23. At 1602 hrs, about 1 NM from the threshold of runway 23 at about 1,500 ft AMSL, the airplane reached the extended runway centre line. The Flugleiter (A person required by German regulation at uncontrolled aerodromes to provide aerodrome information service to pilots.) stated that during final approach flaps and landing gear of the airplane had been extended. The approach looked normal. For a short time he had no longer observed the airplane because he had made some entries in the computer. His colleague had then addressed him and drew his attention to the speed of the airplane. The Flugleiter saw that the airplane had an upward large pitch angle, then plunged and disappeared from his sight. The airplane impacted the ground and the 3 occupants suffered severe injuries. The Flugleiter stated he had tried in vain to contact the pilot twice and then raised the alarm. His colleague and other first aiders had driven to the accident site immediately.

Shortly after takeoff from Juba Airport runway 31, while climbing, the aircraft lost height and crashed in a prairie located near Referendom, about 4 km northwest of Juba Airport, bursting into flames. The aircraft was destroyed by impact forces and a post crash fire. A passenger was seriously injured while seven other occupants were killed. The aircraft was on its way to Aweil with an intermediate stop in Wau, carrying a load of foods and money for wages on behalf of the World Food Programme (WFP). It was reported that the aircraft was loaded with 8 tons of cargo while the maximum allowable would be 5,5 tons.

On August 20, 2020, about 1542 central daylight time, a Beech B200 airplane (marketed as a King Air 200), N198DM, was destroyed when it was involved in an accident near Rockford, Illinois. The private pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 positioning flight. The purpose of the flight was to relocate the airplane to the pilot's home base at the DuPage Airport (DPA), West Chicago, Illinois. The airplane had been at Chronos Aviation, LLC (a 14 CFR Part 145 repair station), at the Rockford International Airport (RFD), Rockford, Illinois, for maintenance work. Multiple airport-based cameras recorded the accident sequence. The videos showed the airplane taking off from runway 19. Shortly after liftoff, the airplane started turning left, and the airplane developed a large left bank angle as it was turning. The airplane departed the runway to the left and impacted the ground. During the impact sequence, an explosion occurred, and there was a postimpact fire. A video study estimated the airplane’s maximum groundspeed during the takeoff as 105.5 knots (kts). Data recovered from an Appareo Stratus device onboard the airplane showed that about 1538, the airplane began taxing to runway 19. At 1540:34, the airplane crossed the hold short line for runway 19. At 1541:19, the airplane began a takeoff roll on runway 19. At 1541:42, the airplane began to depart the runway centerline to the left of the runway. Subsequent tracklog points showed the airplane gaining some altitude, and the tracklog terminated adjacent to a taxiway in a grassy area. The Appareo Stratus data showed the airplane began to increase groundspeed on a true heading of roughly 185° about 1541. Airplane pitch began to increase at 1541:41 as the groundspeed reached about 104 kts. The groundspeed increased to 107 kts within the next 2 seconds, and the pitch angle reached around 4° nose-up at this time. In the next few seconds, pitch lowered to around 0° as the groundspeed decayed to around 98 kts. The pitch then became 15° nose-up as the groundspeed continued to decay to about 95 kts. A right roll occurred of about 13° and changed to a rapidly increasing left roll over the next 5 seconds. The left roll reached a maximum of about 86° left as the pitch angle increasingly became negative (the airplane nosed down). The pitch angle reached a maximum nose down condition of -73°. The data became invalid after 1541:53.4. An airplane performance study based on the Appareo Stratus data showed that during the takeoff from runway 19, the airplane accelerated to a groundspeed of 98 kts and an airspeed of 105 kts before rotating and lifting off. The airplane pitched up, climbed, and gained height above the ground. Then, 4 seconds after rotation, the airplane began descending and slowing, consistent with a loss of power. A nose-left sideslip, a left side force, and a left roll were recorded, consistent with the loss or reduction in thrust of the left engine. The sideslip was reduced, likely due to opposite rudder input, and the airplane briefly rolled right. The airplane pitched up and was able to begin climbing again; however, it continued to lose speed. The sideslip then reversed, and the airplane rolled left again and impacted the ground. One witness reported that he observed the accident sequence. He did not hear any abnormal engine noises, nor did he see any smoke or flames emit from the airplane before impact. The airplane came to rest on a flat grass field to the east of runway 19 on airport property. The airplane sustained fire damage and was fragmented from impacting terrain.

The single engine aircraft completed a humanitarian flight from Juba to Fangak on behalf of the NGO 'Nile Hope'. On board were five passengers and two pilots. During the takeoff roll on a muddy airstrip, the aircraft went out of control, veered off runway and collided with a tree. The right wing was torn off and the aircraft came to rest upside down. Two passengers were slightly injured.

Then twin engine airplane departed Perpignan-La Llabanère Airport on a private flight to Orléans, carrying one passenger and one pilot. On final approach to Orléans-Loiret Airport (ex Saint-Denis-de-l’Hôtel), the pilot encountered a loss of power on the left engine. He attempted an emergency landing when the airplane impacted trees and crash landed in a wooded area located about 3 km short of runway 23, bursting into flames. Both occupants escaped uninjured while the airplane was totally destroyed by a post crash fire.