Executive/Corporate/Business

The approach to Mumbai-Chhatrapati Shivaji Airport was completed in poor weather conditions with reduced visibility due to heavy rain falls. On short final, the airplane was in a nose down attitude and rolling to the right when it impacted the runway surface. It went out of control, veered off runway and came to rest in a grassy area, broken in two. A small fire was quickly extinguished. All eight occupants were injured.

Shortly after takeoff from runway 18 at Little Rock-Bill & Hillary Clinton (Adams Field) Airport, while in initial climb in marginal weather conditions, the twin engine airplane went out of control and crashed in a wooded area located about 1,500 metres past the runway end, near a stone quarry, bursting into flames. The airplane was totally destroyed by impact forces and a post crash fire and all five occupants were killed. Employees of the CTEH Company, they were en route to Columbus responding to an emergency response plan. At the time of the accident, weather conditions were marginal with a visibility of 2 SM due to rain. Four minutes prior to the accident, the wind was 19 knots gusting to 27 knots and five minutes after the accident, the wind was gusting to 40 knots.

The twin engine airplane departed Legazpi-Bicol Airport in the early morning on an executive flight to the capital City. Few minutes after takeoff, while climbing to an altitude of 6,000 feet, it impacted the rocky slope of Mt Mayon located about 16 km north of Legazpi Airport. The wreckage was found the next day near the crater of the volcano. The airplane disintegrated on impact and all four occupants were killed.

The pilot encountered an unexpected situation and elected to make an emergency landing in an open muddy field. He lowered the landing gear and upon touchdown, the airplane overturned and came to rest upside down. All five occupants were rescued and the airplane was destroyed.
Crew:
Zvikomborero Nyamakura, pilot,
Passengers:
Salfina Karimazondo, Murowa Diamonds’ security officer,
Obey Mabvundwi, constable of CID Minerals Flora and Fauna Unit,
Petros Chaguruka, Fawcett's guard,
Fredrick Maroyi, Fawcett's guard.

On September 20, 2022, about 0709 Pacific daylight time, a Cessna 525B, jet airplane, N528DV, was destroyed when it was involved in an accident near Pasco, Washington. The pilot and 9 passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 business flight. The pilot reported that the flight to Tri-Cities Airport, (PSC), Pasco, Washington, was uneventful; he reported to the tower controller that the airport was in sight and requested to land on runway 3L. While on left base, the pilot further reported that he started to lower the flaps and extended the gear handle. He did not recall confirming whether the gear was down and locked but reported that there were no landing caution annunciation or aural warnings. Before making contact with the runway, the pilot noticed that the airplane floated longer than expected and upon touchdown realized that the landing gear was not extended. The airplane slid down the runway and came to a stop near the departure end of the runway. The pilot secured the engines and assisted the passengers evacuate the airplane. During the evacuation, the pilot reported that the airplane was on fire near the right engine. Shortly thereafter, the airplane was engulfed in flames.

The student pilot, who was the new owner of the multi-engine airplane, and a private pilot flew commercially to Lubbock, Texas, utilized a ride-hailing service to drive to Portales, New Mexico; they met with the former owner of the airplane to finalize the purchase of the airplane and flew it back to Georgia the same day. The next day, the student pilot commenced flight training with the private pilot who offered to provide flight instruction to the student pilot in the student pilot’s newly acquired multi-engine airplane, even though he did not possess a flight instructor’s rating or a multi-engine airplane rating. Radar data showed that the track of the accident airplane's route consisted of their departure airport, a midway stop, and the third leg of the flight, where it crashed during the approach to their destination airport. Witnesses observed a sharp right turn before the airplane’s spiraling descent and impact with terrain and unoccupied semi-trailers. Surveillance footage from a parking lot security camera captured the airplane in a right spiral turn just before the accident. The airplane was destroyed by impact forces and the postimpact fire. The postaccident examination of the airframe, engines, and propellers revealed no anomalies that would preclude normal engine and airplane performance. Additionally, a review of the maintenance logbook revealed that the airplane was overdue for its annual maintenance inspection; no special flight permit (ferry permit) was obtained from the Federal Aviation Administration (FAA) for its return flight to Georgia. Toxicological testing of the student pilot revealed the presence amphetamine, a prescription Schedule II controlled substance that may result in cognitive deficits that pose a risk to aviation safety; however, its effect, if any on the accident flight could not be determined. It is likely that the private pilot’s failure to maintain aircraft control was exacerbated by his lack of a multi-engine airplane rating, his lack of a flight instructor rating, and his poor decision making.

The flight crew of the jet obtained weather information for the destination airport, which indicated quartering tailwind conditions for the runway in use at the time, with wind at 3 knots gusting to 16 knots. The crew determined the wind to be within limitations. The cockpit voice recorder transcript and airport surveillance video indicated that the landing approach was normal. The captain, who was the pilot flying, stated that, after touchdown, the thrust reversers were deployed and the airplane turned “sharply to the right.” He reported that remedial control inputs were ineffective in maintaining directional control. Airport surveillance video footage of the landing roll and accident sequence showed that, about 9 seconds into the landing roll, the airplane turned sharply to its right. The airplane departed the runway, its left wingtip struck the ground, the entire wing structure (left wing/right wing/wingbox) separated from the airplane as one assembly, and the fuselage continued a short distance before it came to rest upright. The thrust reversers on each engine were deployed and their extended positions were about equal. A windsock could be seen in the surveillance video footage nearly parallel to the ground, indicating nearly a direct crosswind to the landing runway that would have been towards the airplane’s right side. Recorded wind shortly after the accident was consistent with a 90° right crosswind for the landing runway at 6 knots with gusts to 14 knots. A detailed examination of the airplane and system components revealed that all flight control, steering, and braking systems and their actuator components operated as designed. Although the copilot's yaw force sensor did not meet manufacturer acceptance testing during post accident examination, this would not have affected the directional controllability of the airplane. Based on the available information, it is likely that the pilot’s compensation for the crosswind conditions was inadequate, which resulted in a loss of directional control and runway excursion.

Shortly after takeoff from Piracicaba Airport Runway 35, while climbing, the twin engine aircraft entered a right turn, descended to the ground and crashed in a eucalyptus forest located about 1,5 km north of the airport. The aircraft exploded on impact and was totally destroyed. All seven occupants were killed among them the Brazilian businessman Celso Silveira Mello Filho aged 73 who was travelling with his wife and three kids.
Crew:
Celso Elias Carloni, pilot,
Giovani Dedini Gulo, copilot.
Passengers:
Celso Silveira Mello Filho,
Maria Luiza Meneghel,
Celso Meneghel Silveira Mello,
Camila Meneghel Silveira Mello Zanforlin,
Fernando Meneghel Silveira Mello.

Following an uneventful flight from Cancún, the crew encountered technical problems with the undercarriage while on approach to Toluca-Licenciado Adolfo López Mateos. Decision was taken to complete a belly landing on runway 15/33. The airplane slid for few dozen metres before coming to rest, bursting into flames. All 9 occupants evacuated safely and the aircraft was damaged beyond repair.

After a 30-minute uneventful instrument flight rules (IFR) flight, the business jet landed in the rain on the 4,311ft-long runway. The pilot reported, and runway skid marks corroborated, that the airplane touched down about 1,000 ft from the approach end of the runway. The pilot reported braking action was initially normal and the anti-skid system cycled twice before it stopped working and he was unable to slow the airplane using the emergency brakes. The airplane continued off the departure end of the runway where it traveled through wet grass and a fence before coming to rest with the landing gear collapsed. A video of the airplane during the landing roll indicated there was a significant amount of water on the runway. No mechanical anomalies were found with the brake/antiskid systems during the postaccident examination of the airplane. Marks on the runway indicated functionality of the antiskid system. Stopping performance calculations estimated the distance required to stop the airplane on the runway was about 4,127 ft. The runway length remaining after the airplane touched down was about 3,311 ft. The pilot was aware of the runway length and weather conditions prior to departure and reported that he should have not accepted the trip.