全球航空器事故数据
时间区间
1902-2024
字段展示
全球航空器事故数据-英文字段 | 全球航空器事故数据-中文字段 |
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Year | 年份 |
Date | 日期 |
Time | 时间 |
Type | 机型 |
Owner/operator | 所有者/经营者 |
Registration | 飞机号 |
MSN | MSN |
Year of manufacture | 制造年份 |
Engine model | 发动机型号 |
Fatalities | 死亡人数 |
Other fatalities | 其他死亡人数 |
Aircraft damage | 飞机损坏情况 |
Category | 事件类型 |
Location | 地理位置 |
Phase | 出事阶段 |
Nature | 飞机用途 |
Departure airport | 始发机场 |
Destination airport | 到达机场 |
Confidence Rating | 信用评级 |
narrative | 事件说明 |
notes | 备注 |
Cycles | 飞行次数 |
Total airframe hrs | 总飞行时长 |
Report number | 报告编号 |
Investigating agency | 调查机构 |
Download report | 下载报告 |
Accident investigation PDF | 调查报告 |
Status | 调查进度 |
Duration | 调查时长 |
样本数据
Year | Date | Time | Type | Owner/operator | Registration | MSN | Year of manufacture | Engine model | Fatalities | Other fatalities | Aircraft damage | Category | Location | Phase | Nature | Departure airport | Destination airport | Confidence Rating | narrative | notes | Cycles | Total airframe hrs | Report number | Investigating agency | Download report | Accident investigation PDF | Status | Duration |
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年份 | 日期 | 时间 | 机型 | 所有者/经营者 | 飞机号 | MSN | 制造年份 | 发动机型号 | 死亡人数 | 其他死亡人数 | 飞机损坏情况 | 事件类型 | 地理位置 | 出事阶段 | 飞机用途 | 始发机场 | 到达机场 | 信用评级 | 事件说明 | 备注 | 飞行次数 | 总飞行时长 | 报告编号 | 调查机构 | 下载报告 | 调查报告 | 调查进度 | 调查时长 |
2020 | Saturday 25 April 2020 | 12:15 | Aeronca 7AC Champion | Private | N83216 | 7AC-1877 | 1946 | Continental A65-8F | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Enosburg, VT - United States of America | Landing | Private | South Hero, VT (VT26) | Enosburg, VT | Accident investigation report completed and information captured | The pilot reported that, during the landing roll on a private grass airfield, the main landing gear dug into soft grass, and the airplane nosed over. The airplane sustained substantial damage to the right-wing lift strut. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Probable Cause: The pilot's improper decision to land on unsuitable terrain, which resulted in a nose-over. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 4573 hours | ERA20CA159 | NTSB | Final report | dba924a4b33c6d6359c9baa63c062249 | Investigation completed | 3 months | |
2020 | Wednesday 5 August 2020 | Javelin Wichawk | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Lismore Airport, NSW (YLIS) - Australia | Unknown | Private | Lismore Airport, NSW (YLIS) | Information verified through data from accident investigation authorities | During landing in wet grass parallel to the runway, the wheels dug into soft ground and the aircraft pitched over coming to rest inverted. The aircraft was substantially damaged and the pilot sustained minor injuries. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ATSB | ||||||||||||||
2020 | Sunday 16 August 2020 | 14:54 UTC | Aerotechnik L-13SEH Vivat | Private | N334BA | 940517 | 1994 | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | William 'Tiny' Zehnder Field Airport (66G), Saginaw County, MI - United States of America | Take off | Private | Frankenmuth, MI (66G) | Frankenmuth, MI (66G) | Accident investigation report completed and information captured | The pilot reported that following a landing and back-taxi in a motor glider, he failed to stow the speed brake prior to attempting a subsequent takeoff. During the takeoff attempt, the glider would not climb out of ground effect. The motor glider departed the end of the runway and impacted terrain which resulted in substantial damage to the fuselage. Probable Cause: The pilot's failure to stow the speed brake prior to attempting takeoff. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | CEN20CA337 | NTSB | Final report | 333be449d713f47f063f5d8eb3392e47 | Investigation completed | ||||
2020 | Tuesday 27 October 2020 | 10:33 LT | Hughes 369D | Windward Aviation Inc | N58251 | 880317D | 1978 | Rolls Royce 250-C20B | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | near Nuuanu Reservoir, Honolulu, Oahu, HI - United States of America | En route | Cargo | Oahu-Dillingham Airfield, HI (HDH/PHDH) | Kahului Airport, HI (OGG/PHOG) | Accident investigation report completed and information captured | During longline operations, the helicopter lost partial power and the main rotor rpm decreased. The pilot jettisoned the external load and the helicopter impacted trees, resulting in substantial damage. The engine continued to run after impact, and the pilot performed an emergency engine shutdown. Examination revealed that the start fuel pump was damaged. The circlip and pin that held the flapper valve in place in the bypass inlet were missing, and the flapper valve was wedged against the sidewall of the bypass inlet, obstructing about 50% of the discharge port. The pin was located in the fuel line between the start fuel pump and the engine-driven fuel pump; the circlip was not found. No other mechanical malfunctions were found that would have precluded normal operation. The pin found in the fuel line and obstruction from the flapper valve located in the start fuel pump likely induced restricted fuel flow from the engine-driven fuel pump to the engine, which resulted in a partial loss of engine power. Based on the available evidence, the reason for the separation of the circlip from the pin could not be determined. Probable Cause: A partial loss of engine power due to an obstructed fuel line as a result of the separation of the circlip from the pin used on the fuel start pump. The reason for the circlip separation could not be determined based on the available evidence. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 20345 hours | ANC21LA003 | NTSB | Final report | 21e3d60d08948f010ee098e5ac7f175f | Investigation completed | 1 year and 8 months | |
2020 | Friday 21 August 2020 | Pilatus PC-12/45 | Fat City Air Service LLC | N8YU | 413 | 2001 | P&W Canada PT6A-67 | Fatalities: 0 / Occupants: | 0 | Unknown | Aspen Pitkin County Airport (ASE/KASE), CO - United States of America | Taxi | Unknown | Information is only available from news, social media or unofficial sources | Aircraft struck Raytheon Hawker 800, N489BM, while taxiing. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2020 | Thursday 2 January 2020 | 10:25 | Cirrus SR22 GTS | Cornerstone Aviation LLC | N323SR | 2271 | 2006 | Continental IO-550-N | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | Kenansville, NC - United States of America | En route | Private | Worcester Airport, MA (ORH/KORH) | Elizabethtown-Curtis L Brown Jr Field, NC (KEYF) | Accident investigation report completed and information captured | The pilot reported that, during a cross-country flight, he heard a pop from the engine, and it subsequently stopped producing power; however, the engine continued to run, and the propeller continued to rotate. The pilot attempted to troubleshoot the loss of power; however, power was not restored. Subsequently, the pilot activated the airplane’s parachute system and the airplane impacted trees and terrain, resulting in substantial damage to the airframe. Postacccident examination of the engine revealed that the camshaft fractured at one of its four oil transfer holes. As a result, camshaft continuity was lost, and the engine was partially unable to produce power. Forensic examination of the fracture surface revealed that the fracture occurred due to fatigue that initiated from a burr at the corner of an oil transfer hole. The extent of fatigue crack growth through the cross-section suggested the overall torsion load on the camshaft was relatively low as the crack grew. However, a burr at the edge of a hole is a feature that is known to reduce component fatigue life. The burr was deformed and coated, consistent with forming during a peening operation and before the manganese phosphate coating had been applied. A similar burr was also observed on the adjacent oil transfer hole in the camshaft. The presence of a burr suggests the corner of the hole was not properly broken before the part was peened during manufacturing, leading to deformation of a sharp corner during the peening operation. Probable Cause: A fatigue failure of the camshaft due to a manufacturing defect, which resulted in a partial loss of engine power. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information. Corrections or additions? ... Edit this accident description | 3774 hours | ERA20LA064 | NTSB | Final report | 9bb962bf5514931a56ca757cc4cd45ca | Investigation completed | 2 years and 3 months | |
2020 | Saturday 9 May 2020 | 11:10 LT | Ayres S-2R-G1 Turbo Thrush | Farmers Services | N2245S | G1-106 | Airesearch TPE331 | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Imperial County Airport (KIPL/IPL), CA - United States of America | Landing | Agricultural | Imperial County Airport, CA (IPL/KIPL) | Imperial County Airport, CA (IPL/KIPL) | Accident investigation report completed and information captured | Shortly after landing, the airplane veered left. The pilot used right rudder and applied right brake to counteract the turn, and the airplane began to straighten out. Immediately after, he felt that the right brake was not working, and the airplane again made an immediate turn to the left. The airplane exited the left side of the runway, the left-wing tip impacted the ground, and the airplane spun to the left, which resulted in a collapse of the left main landing gear and substantial damage to the left wing. An examination of the right brake assembly revealed that the center piston O-ring was damaged, and the right brake hydraulic fluid reservoir was empty. These discrepancies resulted in the loss of brake pressure and subsequent failure of the right brake. Probable Cause: The pilot's loss of control during a landing roll due to a failure of the main O-ring in the right brake assembly, which resulted in a loss of brake pressure and subsequent brake failure. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | WPR20LA172 | NTSB | Final report | b5c6b969882f429aca48aedaaf224c9a | Investigation completed | 2 years 1 month | |||
2020 | Thursday 17 September 2020 | c. 10:21 | Cessna 152 II | Lahore Flying Club (LFC) | AP-BEO | 15285762 | Fatalities: 0 / Occupants: 1 | 0 | Minor | Accident | Lahore/Walton Airport (OPLH) - Pakistan | Landing | Training | Allama Iqbal International Airport Lahore | Lahore/Walton (OPLH) | Information is only available from news, social media or unofficial sources | The nose landing gear collapsed on touchdown. The first solo student pilot was not injured. Preliminary information suggests the pilot was making video/taking photos of the flight including landing. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||
2020 | Monday 8 June 2020 | Airbus A350-941 | LATAM Brasil | PR-XTI | 250 | 2018 | Rolls-Royce Trent XWB-84 | Fatalities: 0 / Occupants: | 0 | Minor | São Paulo-Guarulhos International Airport, SP (GRU/SBGR) - Brazil | Standing | Passenger | Information is only available from news, social media or unofficial sources | A LATAM Airlines Brasil Airbus A350-900 suffered minor damage to the no.2 engine fan cowl when a vehicle impacted the nacelle during ground operations. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2020 | Friday 10 January 2020 | 12:40 LT | Mil Mi-8T | KrasAvia | RA-22901 | 98420092 | 1984 | Fatalities: 0 / Occupants: 17 | 0 | Incident | Krasnoyarsk Krai, Siberia - Russia | En route | Passenger | Syndassko | Khatanga | Information verified through data from accident investigation authorities | The helicopter made an emergency landing after engine failure. There are said to be no fatalities. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information. Corrections or additions? ... Edit this accident description | ||||||||||
2020 | Monday 5 October 2020 | 11:15 | Cessna 180 Skywagon | Fatalities: 0 / Occupants: | 0 | Substantial | Accident | Saarmund Airport (EDCS) - Germany | Take off | Unknown | Saarmund | Information verified through data from accident investigation authorities | During takeoff roll, the aircraft collided with a deer running across the runway. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | BFU | |||||||||||||
2020 | Sunday 29 March 2020 | Luscombe 8A | Private | N71899 | 3326 | Fatalities: 0 / Occupants: 1 | 0 | Unknown | 24330 Snake River Rd, Asotin, WA - United States of America | Landing | Unknown | Information is only available from news, social media or unofficial sources | The aircraft experienced a loss of directional control and subsequent runway excursion upon landing at Snake River Rd, Asotin, Washington. The airplane came to rest inverted, sustaining unspecified damage, and the sole pilot onboard was not injured. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||||
2020 | Tuesday 4 August 2020 | Harbin Y-12-II | Kenya Air Force - KAF | KAF128 | 0097 | 1997 | Fatalities: 0 / Occupants: 10 | 0 | Substantial | Accident | Dhobley Airstrip - Somalia | Take off | Military | Dhobley Airstrip | Nairobi-Moi Air Base (HKRE) | A Kenya Air Force Harbin Y-12-II suffered an accident at Dhobley Airstrip in Somalia. There were no serious injuries to the 10 people on board but the aircraft was seriously damaged. The landing gear as well as the left-hand wing have collapsed. The accident happened after the aircraft had taken off from Dhobley Airstrip after delivering supplies to U.N. Amisom forces. | ||||||||||||
2020 | Monday 20 January 2020 | 12:20 | Cessna 150G | Private | N4763X | 15064813 | 1966 | Continental O-200 SERIES | Fatalities: 1 / Occupants: 1 | 0 | Destroyed | Accident | near Cherokee County Airport (JKV/KJSO), Jacksonville, TX - United States of America | En route | Private | Jacksonville-Cherokee County Airport, TX (JKV/KJSO) | Accident investigation report completed and information captured | On January 20, 2020, about 1220 central standard time, a Cessna 150G airplane, N4763X, was substantially damaged when it was involved in an accident near Jacksonville, Texas. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. Radar information showed that, after departing in day visual meteorological conditions, the pilot climbed the airplane to a maximum altitude of about 1,600 ft mean sea level (msl) before entering a gradual descent. The last radar return showed the airplane at a speed of 92 knots and altitude about 900 ft msl. The wreckage was found in the vicinity of a 1,586-ft-tall television tower, and its distribution was consistent with the left wing contacting one of the tower’s guy wires, resulting in a separation of the outboard section of the left wing. The airplane subsequently impacted terrain in a nose-down, near vertical attitude and was destroyed by impact. Examination revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation of the airplane or engine. The circumstances of the accident are consistent with the pilot’s failure to maintain clearance from tower guy wires while flying at low altitude. Probable Cause: The pilot’s failure to maintain clearance from guy wires associated with a tower while maneuvering at low altitude. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | WPR20FA067 | NTSB | Final report | b085a33513575b2602831c2fc024b777 | Investigation completed | 2 years and 4 months | |||
2020 | Friday 25 September 2020 | 17:30 LT | Piper PA-46R-350T Matrix | Coadmere Inc | N920X | 4692206 | 2014 | Lycoming TIO-540-AE2A | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | near Rogers Municipal Airport (ROG/KROG), Benton County, AR - United States of America | En route | Training | Rogers Municipal Airport-Carter Field, AR (ROG/KROG) | Rogers, AR | Accident investigation report completed and information captured | The pilot reported that while practicing slow flight and approach-to-stall maneuvers at 5,500 ft msl with the landing gear and flaps fully extended, the stall warning horn sounded, and the airplane began buffeting. The pilot advanced the throttle and lowered the nose of the airplane to recover from the maneuver, when the right wing dropped, the airplane rolled over inverted, and subsequently entered a right spiral dive. The pilot reported that after 5 to 7 turns he regained control of the airplane leveling at 500 to 700 ft agl. The pilot returned to the airport and landed without further incident. Postaccident examination revealed the airplane sustained substantial damage to the fuselage above the left wing's trailing edge, below and forward of the empennage, above the right horizontal stabilizer, and at the tail cone below the right and left horizontal stabilizers. The pilot reported there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Probable Cause: The pilot's inadvertent loss of aircraft control, resulting in substantial damage to the airframe during the spin recovery. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 815 hours | CEN20LA430 | NTSB | Final report | b19d985dc8ac7e587ad33e7ec2946c1f | Investigation completed | 12 months | |
2020 | Saturday 25 April 2020 | 11:00 | Fly Synthesis Storch | Aeroklub “Josip Križaj” Ajdovščina | S5-PFA | F1BC4940C32K | Fatalities: 0 / Occupants: 2 | 1 | Destroyed | Ajdovščina - Slovenia | En route | Private | Ajdovšcina Airport (LJAJ) | Ajdovšcina Airport (LJAJ) | Information is only available from news, social media or unofficial sources | A paraglider collided with a Fly Synthesis Storch ultralight. Both crashed. The aeroplane pilot pulled the rescue parachute however they were flying to low for the parachute to fully deploy. The two occupants of the ultralight plane suffered heavy casualties but survived the crash. The paraglider died in the crash. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | |||||||||||
2020 | Wednesday 2 December 2020 | 09:25 | Boeing 737-529 | Air Djibouti | EY-560 | 26538/2298 | 1992 | CFMI CFM56-3B1 | Fatalities: 0 / Occupants: 39 | 0 | Substantial, repaired | Accident | Garowe Airport (GGR) - Somalia | Landing | Passenger - Scheduled | Hargeisa Airport (HGA/HCMH) | Garowe Airport (GGR/HCMW) | Information verified through data from accident investigation authorities | An Air Djibouti Boeing 737-529, EY-560, suffered a right-hand main landing gear collapse on landing at Garowe Airport, Puntland, Somalia. The aircraft operated on a flight from Djibouti to Mogadishu, Somalia, with en route stops at Hargeisa and Garowe. The pilot conducted a visual approach and the aircraft was stable. At low altitude the aircraft experienced a windshear and hit the runway hard. The root cause of the accident is loss of control of aircraft. The contributory factor was windshear. | 42964 hours | ||||||||
2020 | Tuesday 7 July 2020 | 14:35 | Schleicher ASW-19B | OK-7984 | 19420 | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Hodkovice (LKHD) - Czech Republic | Landing | Private | Hodkovice nad Mohelkou Airport (LKHD) | Hodkovice nad Mohelkou Airport (LKHD) | Accident investigation report completed and information captured | On landing, the aircraft bounced several times and then touched down hard. This caused damage to the nose, the cockpit glazing and the tail. The cause of the accident was most likely the pilot changing the control lever of the aerodynamic brakes and the landing gear lever. As a result, the approach and landing took place at high speeds. The pilot did not successfully solve this situation. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | UZPLN | Final report | 13201a6d9baf3a4335cefcbd0a8e9e8d | Investigation completed | 8 months | ||||||
2020 | Saturday 30 May 2020 | 19:32 | Cessna 182C Skylane | SkyConcept | D-EYST | 52478 | 1959 | Fatalities: 0 / Occupants: 1 | 0 | Destroyed | Accident | Langenhahn, Rhineland-Palatinate - Germany | Approach | Parachuting | Ailertchen Airfield (EDGA) | Ailertchen Airfield (EDGA) | Accident investigation report completed and information captured | After dropping four parachutists, the engine failed during descent. Subsequently, the aircraft collided with an overhead power line and crashed into the roof of a residential building. The pilot was injured and the aircraft destroyed. Also the electricity of 50.000 people was cut off. Conclusions: The accident was caused by the pilot experiencing an engine failure due to an interrupted fuel supply, and the aircraft colliding with obstacles during the subsequent emergency landing. The following factors contributed to the accident: - Non-compliance with the manual requirements for the descent procedure with the low fuel quantity present in the wing tanks - Attempts to start the engine without first selecting and approaching an emergency landing area - Too low an altitude at the time of engine failure to safely reach the airport in a glide | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | BFU | Final report | bc49249ed207b196706bd1d8da40f09e | Investigation completed | 3 years and 3 months | ||||
2020 | Sunday 11 October 2020 | 14:42 | Cessna FRA150L Aerobat | Private | G-CIIR | FRA15000187 | 1973 | Continental O-240-A | Fatalities: 1 / Occupants: 1 | 0 | Destroyed | Accident | North of Troutbeck, between Keswick and Penrith, Cumbria - United Kingdom | Take off | Private | Troutbeck Airfield, Keswick, Cumbria | Repton/Gamston Airport (EGNE) | Accident investigation report completed and information captured | The aircraft, a Cessna FRA150L Aerobat (G-CIIR) landed at Troutbeck Airfield with its pilot and a passenger without the required permission. As the conditions on the day meant the aircraft’s takeoff performance from Troutbeck would be marginal, the airfield owner instructed the pilot to depart solo in order to improve the aircraft’s performance by reducing its takeoff weight. On the subsequent takeoff the aircraft was seen to depart controlled flight seconds after getting airborne and strike the ground. The pilot was fatally injured. The investigation identified a number of shortcomings with the preparation for the flight that contributed to the accident. In addition, opportunities were missed to prevent the accident because the pilot did not heed the advice not to operate into grass, performance-limiting airfields, did not obtain PPR and was probably not on the correct radio frequency on arrival. It is likely that the pilot did not fasten his shoulder harness, against the strong advice of his instructor, and this action may have meant the accident became unsurvivable. Flying for any pilot is a continual learning process whether they are newly qualified or very experienced. However, newly qualified pilots should be very careful to make sure they fly within the limits of their experience. This accident highlights the fact that thorough preparation is essential for every flight, and accidents can happen if short cuts are taken or good advice is not heeded. =Damage sustained to airframe= Per the AAIB Report the airframe was "Destroyed". The CAA agreed with this conclusion, as the registration G-CIIR was cancelled, and the airframe de-registered, on 18 May 2021 as "destroyed" | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | AAIB-26991 | AAIB | Final report | 117fca6eda4446b661c31e1c7c2016b0 | Investigation completed | 1 year 1 month | ||
2020 | Wednesday 18 March 2020 | 13:30 | Boeing 737-33A | Aerolínea Estelar | YV-642T | 27267/2600 | 1994 | CFMI CFM56 | Fatalities: 0 / Occupants: 118 | 0 | Cacique Aramare Airport (SVPA), Puerto Ayacucho, Amazonas - Venezuela | En route | Passenger - Scheduled | Buenos Aires/Ezeiza-Ministro Pistarini Airport, BA (EZE/SAEZ) | Caracas-Simón Bolívar International Airport (CCS/SVMI) | Information is only available from news, social media or unofficial sources | Estelar Flight ES-8568 with 118 passengers on board, (crew members not available) was diverted to Puerto Ayacucho’s Cacique Aramare Airport due pressurisation system issues, according to airline statements. Landed safely at 13:30 local time (17:30 Z). | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||
2020 | Friday 28 August 2020 | c. 1045 UTC | de Havilland Canada DHC-8-402Q Dash 8 | SpiceJet | VT-SUL | 4400 | P&W Canada PW150 | Fatalities: 0 / Occupants: | 0 | Serious incident | Cochin International Airport (COK/VOCI) - India | Approach | Passenger - Scheduled | Bengaluru (Bangalore) International Airport (BLR/VOBL) | Cochin International Airport (COK/VOCI) | Information verified through data from accident investigation authorities | SpiceJet flight SG7077, a DHC-8-402Q (VT-SUL) and Qatar Airways flight QR7477, an Airbus A320-232 (A7-AHA) were involved in a serious airprox incident while on approach to Cochin Airport, India. Minimum separation was reduced to 2 NM horizontally and 500 feet vertically. Probable Cause of the Incident. Non adherence to ATC instructions by the crew of SEJ7077. Contributory factor: During descent to 3000 ft , pilot flying did not engage ‘ALT SEL’ and the same was not monitored by Pilot monitoring also. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | AAIB India | Final report | c59c52e0ef151797c749880cb481ef46 | Investigation completed | 6 months | |||||
2020 | Monday 28 December 2020 | 20:45 LT | Beechcraft B80 Queen Air 8800 | Bemidji Aviation Services | N134BA | LD-202 | 1964 | Lycoming IGSO-540-B1A | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Chandler Field Airport, Alexandria, MN - United States of America | Take off | Unknown | Chandler Field (AXN/KAXN), Alexandria, MN | Minneapolis-St. Paul International Airport, MN (MSP/KMSP) | Accident investigation report completed and information captured | The pilot reported that the takeoff was conducted below the airplane's maximum gross weight. Although his written statement and interviews indicated that there was no frost on the airplane during his preflight examination, the police report of the accident stated that the pilot told the responding officer immediately after the accident that there could have been frost on the wings of the airplane. The airport manager who responded to the accident scene reported that all airplane surfaces were covered with frost when he arrived a short time after the accident. The pilot reported that during the takeoff the rotation speed was between 82 and 85 knots. The pilot's reports of what happened after rotation were consistent, indicating that the airplane began to veer to the right and began shaking. The pilot stated that he did not hear a stall warning and that the airplane did not feel like it was in a stall. While the pilot tried to correct the veering to the right, the airplane pitched down, turned left, and the left wing struck the ground. The airplane then bounced, the right wing struck the ground, and the right main landing gear collapsed. The left wing sustained substantial damage. Airplane performance data indicated that the proper rotation speed for a maximum gross weight takeoff was 96 knots. The power-on stall speed at maximum gross weight for the airplane with landing gear extended and flaps retracted was not specifically listed but would have been between 78 and 91 knots based on available performance data from the airplane owner's manual. In addition, the performance data would have been for an airplane without frost on it; frost would have increased the speed. Based on the available evidence it is likely that the airplane had frost contamination, which the pilot ignored. He then rotated the airplane during the maximum gross-weight takeoff at a speed below the airplane manufacturer's recommended rotation speed. The slower speed in combination with degraded performance due to frost contamination of the airplane's flying surfaces resulted in exceedance of the critical angle of attack, resulting in an aerodynamic stall and subsequent impact with the ground. Probable Cause: The pilot's decision to attempt takeoff with frost covering the airplane and rotating below the published rotation speed, which led to exceedance of the airplane's critical angle of attack and an aerodynamic stall. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 18126 hours | CEN21LA101 | NTSB | Final report | 501eed514ef6664c97e0abb0c88f6acf | Investigation completed | ||
2020 | Saturday 31 October 2020 | 14:00 | Robin DR.400/140B | Vliegclub Rotterdam (VCR) | PH-NSC | 2611 | 2006 | Fatalities: 0 / Occupants: | 0 | Minor | Accident | Rotterdam/The Hague Airport (RTM/EHRD) - Netherlands | Landing | Unknown | Rotterdam/The Hague Airport (RTM/EHRD) | Rotterdam/The Hague Airport (RTM/EHRD) | Information verified through data from accident investigation authorities | During landing the pilot lost control of the aeroplane, whereupon it veered off the runway and hit a PAPI light unit with the left wing, before it came to a stop. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | Dutch Safety Board | ||||||||
2020 | Sunday 14 June 2020 | Schempp-Hirth Ventus 2B | OY-HXB | 72 | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Hammer (EKHM)r - Denmark | Take off | Private | Hammer (EKHM) | Hammer (EKHM) | Information verified through data from accident investigation authorities | During the winch launch for a thermal flight the glider got a strong crosswind shortly after take off in about 2 meters height. One wing got ground contact and the glider turned and hit the ground hard. The AIBN has identified the following factors that are presumed to have influenced the course of events: - A language barrier, between the winch driver (who was of foreign origin and had limited Danish skills) and the pilot, may have resulted in a misunderstanding about the pilot's intention of a good acceleration at the beginning of the start but a minor move later. - The winch manager's current training condition is estimated during the course of events to have affected the winch operator's operation of the winch. - The glider had a smaller rear rudder effect at low speeds compared to other types of gliders. - Poor acceleration resulted in a long starting run at low speed. The fact that the glider got into the air, at a relatively low speed, may have made it more difficult for the pilot to control the glider. - The glider may have been in lateral imbalance. The center of gravity of the left wing was possibly further located than the center of gravity of the right wing, due to water that had moved outwards in the wing. - A markedly variable headwind component, due to offensive winds from changing directions, probably caused the glider to unexpectedly lose lift. - A subsequent skewed winch move led to loss of control of the glider from low flight altitude. - The pilot did not interrupt the start of the winch launch in time and disconnected from the starting wire. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | HCLJ | Final report | 30d3a195c0d482dc124d0c32666dc73e | Investigation completed | 8 months | |||||||
2020 | Wednesday 30 September 2020 | 16:28 | Robinson R22 | Private | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Hawkwood, W of Maryborough, QLD - Australia | En route | Agricultural | Information verified through data from accident investigation authorities | During aerial mustering operations, the engine lost power and the helicopter was unable to maintain height. The helicopter made contact with trees and subsequently collided with terrain resulting in substantial damage. The pilot was uninjured. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ATSB | |||||||||||||
2020 | Saturday 31 October 2020 | Cessna TU206C Super Skywagon | private | C-FMQG | U2061101 | 1968 | Continental TSIO-520-C | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | 28 nm NNW of Bella Coola (CYBD), BC - Canada | En route | Private | Anahim Lake (CAJ4), BC | Bella Coola (CYBD), BC | Information verified through data from accident investigation authorities | A privately operated Cessna 206 aircraft, was conducting a flight from Anahim Lake (CAJ4), BC to Bella Coola (CYBD), BC with a sole pilot on board. While the aircraft was flying at approximately 2000 feet ASL, over the Dean Channel, the engine (Teledyne Continental TSIO-520 -C) experienced a complete power loss. The aircraft was ditched into the channel near the mouth of the Dean River. Upon entry into the water the aircraft began to sink and the pilot quickly exited. The pilot was wearing a manual inflation PFD which he inflated upon exit from the aircraft. The aircraft then sank below the water surface while the pilot, wearing his PFD, swam to the shore line where he was able to summon assistance from a nearby cabin. The pilot sustained minor injuries. An ELT signal was not received. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | TSB | ||||||||
2021 | Tuesday 24 August 2021 | 10:09 LT | Pilatus PC-21 | Pilatus Flugzeugwerke | HB-HZD | 102 | 2005 | Fatalities: 0 / Occupants: 2 | 0 | Serious incident | Emmen - Switzerland | Unknown | Training | Buochs Airport (BXO/LSZC) | Buochs Airport (BXO/LSZC) | Information verified through data from accident investigation authorities | A Pilatus PC-21 (HB-HZD) and a Cessna 182T (HB-TLM) were involved in a serious airprox incident near Emmen, Switzerland. The two aircraft were at approximately the same altitude with converging flight paths, leading to a dangerous airprox. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | STSB | |||||||||
2021 | Thursday 10 June 2021 | 19:10 | Piper PA-32-260 Cherokee Six | G&M Aircraft Inc | N3793W | 32-720 | 1966 | Lycoming O-540-E4B5 | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | near Lafayette, CO - United States of America | En route | Training | Broomfield-Rocky Mountain Metropolitan Airport, CO (BJC/KBJC) | Lafayette, CO | Accident investigation report completed and information captured | The purpose of the instructional flight was for the pilot to receive a checkout in the airplane. Before the flight, the right wing main fuel tank contained 16-18 gallons of fuel, the left wing main fuel tank contained less than 10 gallons of fuel, and both wingtip tanks were completely full (17 gallons each). The pilot and his flight instructor discussed the fuel status before departure and had agreed to operate the engine on the right wing main tank to correct the fuel imbalance between the tanks during the flight. The flight consisted of visual flight rules maneuvers and touch-and-go landings, and about 1.1 hour into the flight the airplane had a loss of engine power about 1,000 ft above the ground while in cruise flight. A forced landing was completed to a nearby field, but shortly after touchdown the airplane collided with a berm that caused the airplane to become airborne again. The nose landing gear collapsed and both wings were substantially damaged when the airplane landed hard the second time. The pilot and his flight instructor both reported that the entire flight had been flown using fuel from the right wing main fuel tank. Neither the pilot nor his flight instructor switched fuel tanks after the loss of engine power because they were focused on the forced landing. The pilot stated that based on the airplane’s performance data, the loss of engine power was likely due to fuel starvation. An onsite examination of the wreckage revealed that the right wing main fuel tank was intact and contained less than ¼ gallon of fuel. According to the airplane’s owner’s handbook, there was about 1 pint of unusable fuel in each of the 4 fuel tanks. The remaining 3 fuel tanks contained usable fuel. Additionally, there were no mechanical malfunctions identified with the airplane’s fuel system or the engine that would have precluded normal operation. Probable Cause: The flight crew’s improper fuel management that resulted in fuel starvation and the loss of engine power. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 3420 hours | CEN21LA261 | NTSB | Final report | c9c2c7383592781ec2676b5075225098 | Investigation completed | 6 months | |
2021 | Thursday 30 December 2021 | 22:00 UTC | ATR 72-202 (QC) | Calm Air | C-FJCQ | 311 | P&W Canada PW124B | Fatalities: 0 / Occupants: | 0 | Unknown | 150 nm WSW of Rankin Inlet (CYRT), NU - Canada | En route | Unknown | Gjoa Haven Airport, NU (YHK/CYHK) | Thompson Airport, MB (YTH/CYTH) | Information verified through data from accident investigation authorities | An ATR 72-200 operated by Calm Air, was conducting flight CAV468 from Goa Haven (CYHK), NU to Thompson (CYTH), MB. When the flight was approximately 150 nm west southwest from Rankin Inlet (CYRT), NU, the crew observed an intermittent low oil pressure warning light on the left engine (Pratt & Whitney Canada PW124B). The crew referred to the QRH and decided to divert to CYRT. While enroute to CYRT, the master caution light for the engine low oil pressure illuminated. The crew shut down the left engine as a precautionary measure and continued to CYRT where they carried out an uneventful landing. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | TSB | |||||||||
2021 | Thursday 24 June 2021 | 11:15 LT | Piper PA-28-161 Warrior II | Trident Aircraft Inc | N2143G | 28-7916176 | 1978 | Lycoming O-320-D3G | Fatalities: 0 / Occupants: 1 | 0 | Destroyed | Accident | near Easton/Newnam Field Airport (ESN/KESN), Easton, MD - United States of America | Approach | Training | Easton/Newnam Field Airport (ESN/KESN), Easton, MD | Easton/Newnam Field Airport (ESN/KESN), Easton, MD | The student pilot was conducting his first solo flight. After his second takeoff, while turning onto the downwind leg of the airport traffic pattern, he heard the engine lose power. At an altitude of 700 ft above ground level, he did not think he could make it back to the airport, so he maneuvered the airplane for a forced landing to a field. During the approach, the airplane stalled and impacted a construction area before reaching the field. A postcrash fire ensued. Flight control cable continuity for the aileron, stabilator, and rudder cables were continuous from the cockpit to the respective control surfaces, except for separations consistent with recovery cuts near the wing roots and the tailcone. The engine cylinders were examined with a borescope and minor scoring was noted. No anomalies were noted with the airframe or engine that would have precluded normal operation; however, due to the extent of the postcrash fire damage, the ignition and fuel systems could not be examined or tested, and the reason for the loss of engine power could not be determined. Probable Cause: A total loss of engine power for reasons that could not be determined. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 8649 hours | ERA21LA267 | NTSB | Final report | 01d79b500e2f2db5408f291583367dff | Investigation completed | |||
2021 | Thursday 15 April 2021 | 10:00 LT | Piper PA-22-160 Pacer | Private | N3551Z | 22-7462 | 1960 | Lycoming O-320 SERIES | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Cottonwood Airport (P52), Cottonwood, AZ - United States of America | Landing | Private | Calnevar, NV (1L4) | Cottonwood, AZ | Accident investigation report completed and information captured | The pilot of a tailwheel equipped airplane reported that, during the landing roll, while adjusting the flap handle, he briefly stepped on the right rudder and the airplane veered to the right. While attempting to correct with left rudder input, the airplane continued to veer to the right, exited the runway, ground looped to the right and collapsed the left main landing gear. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Probable Cause: The pilot's failure to maintain directional control during landing, which resulted in a ground loop. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 3400 hours | WPR21LA160 | NTSB | Final report | afa529e4c143c5bf50ea9a6ae1168f91 | Investigation completed | 5 months | |
2021 | Thursday 4 February 2021 | 13:20 UTC | Diamond DA62 | Private | PS-EBI | 62.089 | 2018 | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | Fazenda Chapadão, Barreiras, BA - Brazil | Landing | Private | Fazenda Vitória (SITH) Aerodrome, Luís Eduardo Magalhães, BA | Fazenda Chapadão, Barreiras, BA | Accident investigation report completed and information captured | The aircraft took off from the Fazenda Vitória (SITH) Aerodrome, Luís Eduardo Magalhães, BA, bound for the Agricultural Landing Area of Fazenda Chapadão, Barreiras, BA, at approximately 13:05 (UTC), with one pilot and one passenger on board. During the rollout after landing, while trying to divert from a mud puddle, the left wing collided with a corn field, resulting in loss of aircraft control. After a yaw of approximately 90 degrees to the left, the aircraft came to a stop with its front end in the cornfield.The aircraft had substantial damage. All on board were unharmed. Contributing factors. - Control skills – undetermined. It is possible that, during the reported deviation attempt, an inadequacy in the use of the controls resulted in the contact of the left-wing tip with the existing vegetation on the side of the runway, which caused an abrupt left turn, whose correction could not be performed because of the conditions prevailing at the time of landing (soft, wet, slippery terrain with accumulations of water). - Piloting judgment – a contributor. The fact that it had rained the day before and the slippery condition of the runway, in which there were still puddles of water, as well as the non-compliance with the requirements established in the RBACs 91 and 137, led the investigators to conclude that the inadequate assessment of the risks associated with the operation conducted under such conditions contributed to this accident. In addition, the requirements established in the RBACs 91 and 137 which prevented the operation in that location, were not considered. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | CENIPA | Final report | 279bfaa2d75a874f10032e694c195a9a | Investigation completed | 1 year and 8 months | ||||
2021 | Monday 8 November 2021 | 16:15 LT | Cub Crafters CC18-180 Top Cub | U.S. Department of the Interior | N413CC | CC18-0065 | 2013 | Lycoming O-360-C4P | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Yukon Charlie River, AK - United States of America | Landing | Unknown | Eagle Airport, AK (EAA/PAEG) | Yukon Charlie River, AK | Accident investigation report completed and information captured | The pilot reported that he had completed one high to mid-level reconnaissance flight over the snow-covered runway in his tundra tire tailwheel-equipped airplane. Before landing, he intended to fly a low pass and drag the main landing gear along the surface of the runway to determine the depth of the snow. As the main landing gear wheels touched down atop the snow, he stated it initially felt okay but also felt deeper than what he had anticipated. He applied full power and began to apply back stick pressure, but he felt the snow consistency change to a punchy feeling, and the airplane's tail began to rise. Subsequently, the airplane nosed over and sustained substantial damage to the rudder and right-wing lift strut. The pilot reported that there were no preimpact mechanical failures or malfunctions with the airplane that would have precluded normal operation. Probable Cause: The pilot's selection of an unsuitable landing site, which resulted in a nose-over. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 1388 hours | ANC22LA006 | NTSB | Final report | 2b2c26ccaa4c02318a4719ab5e388cd1 | Investigation completed | ||
2021 | Monday 14 June 2021 | day | Gulfstream American AA-5B Tiger | Private | G-BIPV | AA5B-0981 | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Sandown Airport, Sandown, Isle of Wight - United Kingdom | Landing | Private | Sandown Airport (EGHN) | Information verified through data from accident investigation authorities | Gulfstream American AA-5B Tiger G-BIPV substantially damaged 14 June 2021 in a landing accident at Sandown Airport, Sandown, Isle of Wight. The incident was the subject of an AAIB Correspondence-only investigation, published on 14 October 2021 and the following is the summary from that... "14 Jun 2021 Gulfstream AA-5B G-BIPV Sandown Airport, Isle of Wight, Hampshire Following an uneventful approach to land in very little wind, with full flap deployed, the aircraft floated over the grass strip for an “unusually long” time before touching down. The brakes were applied but the pilot was unable to bring the aircraft to a safe stop. It overran the end of the runway into rough terrain and gravel, during which the nose gear collapsed". | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2021 | Wednesday 14 July 2021 | Cessna U206G Stationair 6 II | Aero Jomacha | XA-KCH | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Morelos, Chihuahua - Mexico | En route | Ferry/positioning | Information is only available from news, social media or unofficial sources | A Cessna U206G Stationair 6 II crashed under unknown circumstances in Morelos, Chihuahua. The pilot was not injured. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | |||||||||||||||
2021 | Wednesday 30 June 2021 | c. 18:45 UTC | Piper PA-23-250 Aztec F | Pacific Fleet Aviation LLC | N1715Y | 27-7654096 | 1976 | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | Kona-Keahole Airport, HI (KOA/PHKO) - United States of America | Taxi | Private | Kona-Keahole Airport, HI (KOA/PHKO) | Information is only available from news, social media or unofficial sources | A Piper PA-23-250 Aztec F sustained substantial damage when it collided with Dassault Falcon 900C N917JF at Kona-Keahole Airport (KOA/PHKO), Hawai, USA. There were no injuries. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | NTSB | |||||||||
2021 | Monday 29 March 2021 | 16:03 UTC | Progressive Aerodyne SeaRey LSA | Progressive Aerodyne Inc | N847SR | 1096 | Fatalities: 0 / Occupants: 1 | 0 | Unknown | Flagler County Airport, FL (FIN/KFIN) - United States of America | Landing | Private | Flagler County Airport, FL (FIN/KFIN) | Information is only available from news, social media or unofficial sources | Aircraft landed and veered off runway into the grass, became airborne again, returned to land and veered off the runway into the grass. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2021 | Monday 15 November 2021 | Van's RV-3 | Private | I-1174 | Fatalities: 1 / Occupants: 1 | 0 | Destroyed | Accident | near Ano Amygdali, Larissa - Greece | En route | Private | Drama | Athens | Little or no information is available | The aircraft crashed into a heavily wooded steep ravine, killing the pilot. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2021 | Friday 10 December 2021 | 13:10 | Air Tractor AT-802 | Fatalities: 0 / Occupants: | 0 | Substantial | Accident | 49.8 km 286 degrees from Wee Waa, NSW - Australia | Unknown | Agricultural | Information verified through data from accident investigation authorities | During agricultural spraying operations, the aircraft struck a powerline and the pilot diverted the aircraft to Moree. The aircraft sustained substantial damage. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ATSB | ||||||||||||||
2021 | Saturday 3 April 2021 | c. 15:21 | Robinson R22 Beta | Spitzer Helicopter LLC | N74347 | 3759 | 2005 | Fatalities: 0 / Occupants: 2 | 0 | Unknown | Martin State Airport (MTN/KMTN), Baltimore, MD - United States of America | Manoeuvring (airshow, firefighting, ag.ops.) | Private | Baltimore-Glenn L. Martin Airport, MD (MTN/KMTN) | Baltimore-Glenn L. Martin Airport, MD (MTN/KMTN) | Information is only available from news, social media or unofficial sources | The aircraft experienced a tail rotor strike during hover at Martin State Airport (MTN/KMTN), Baltimore, Maryland. The helicopter sustained unreported damage and the two pilots onboard were not injured during the incident. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||
2021 | Sunday 9 May 2021 | 09:04 | Airbus A320-214 | Trade Air | 9A-BTH | 1454 | 2001 | CFMI CFM56-5B4/P | Fatalities: 0 / Occupants: | 0 | Unknown | Ljubljana Airport (LJU/LJLJ) - Slovenia | Take off | Passenger | Ljubljana-Brnik Airport (LJU/LJLJ) | Madeira-Cristiano Ronaldo International Airport (FNC/LPFU) | Information is only available from news, social media or unofficial sources | Trade Air flight C3125, a Airbus A320-214, returned to land at Ljubljana Airport after suffering a bird strike. The Ljubljana Tower controller reported that airport operations located a harrier on the runway. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | |||||||||
2021 | Wednesday 13 January 2021 | Mil Mi-24? | Sudan Armed Forces | Fatalities: 0 / Occupants: 3 | 0 | Destroyed | Wad Zayed Airport, al-Showak, al-Qadarif province - Sudan | Take off | Military | Wad Zayed Airport, al-Showak, al-Qadarif province | Information is only available from news, social media or unofficial sources | The Sudanese military helicopter crashed upon takeoff under unknown circumstances. All three crew members survived the crash. *media reported an Apache helicopter. Impossible as the SAF has not this helicopter and it can't carry 3 POB! | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | |||||||||||||||
2021 | Wednesday 13 October 2021 | 07:55 | Boeing 737-8AS (WL) | Ryanair | EI-EKR | 38503/3202 | 2010 | CFMI CFM56-7B | Fatalities: 0 / Occupants: | 0 | Minor | near Manchester Airport, Ringway, Manchester - United Kingdom | Take off | Passenger - Scheduled | Manchester International Airport (MAN/EGCC) | Lanzarote Airport (ACE/GCRR) | Information is only available from news, social media or unofficial sources | Ryanair flight FR2131, a Boeing 737-8AS, suffered a bird strike on departure from Manchester Airport, U.K. The flight crew stopped the climb at 3625 feet and entered a holding pattern over Warrington, north of Liverpool before safely diverting to Liverpool Airport, where it landed safely on runway 27 about 55 minutes after departure. Ground observers at Manchester reported the engines (CFM56) sounded rough, almost like a helicopter, as the aircraft climbed out. A spokesperson for Ryanair said: "“This flight from Manchester to Lanzarote (13th Oct) diverted to Liverpool airport following a minor bird strike. The aircraft landed normally, and customers were transferred to a replacement aircraft which departed to Lanzarote following a short delay of approximately one hour. "Ryanair sincerely apologised to all affected customers." A Liverpool John Lennon Airport confirmed the Ryanair flight's unscheduled landing: "A Ryanair flight that took off from Manchester Airport bound for Arrecife (Lanzarote) requested to land here at Liverpool John Lennon Airport at 08:45 this morning landing safely and without incident at 08:53." | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | |||||||||
2021 | Wednesday 12 May 2021 | 15:30 | Aérospatiale AS 350B2 Ecureuil | US Customs and Border Protection (CBP) | N841BP | 2036 | 1987 | Turbomeca Arriel 1D1 | Fatalities: 0 / Occupants: 2 | 0 | Destroyed | Accident | Clarence E Page Municipal Airport (RCE/KRCE), Oklahoma City, OK - United States of America | Manoeuvring (airshow, firefighting, ag.ops.) | Training | Oklahoma City-Will Rogers Airport, OK (OKC/KOKC) | Clarence E Page Municipal Airport, OK (RCE/KRCE) | Accident investigation report completed and information captured | On May 12, 2021, about 1530 central daylight time, an Aerospatiale (Airbus) AS350 B2 helicopter, N841BP, was destroyed when it was involved in an accident near Yukon, Oklahoma. The pilot receiving instruction and the flight instructor were not injured. The helicopter was operated as a 14 CFR Part 91 public aircraft instructional flight. The pilot receiving instruction (pilot) and the flight instructor were conducting a training flight in the helicopter. They performed several simulated emergencies, each of which required the helicopter’s hydraulic system to be turned off and then turned back on at the conclusion of the procedure. The hydraulic system was turned off and on using the hydraulic cut-off switch, an unguarded push-button switch mounted on the end of the pilot’s collective stick. After completing the emergency procedures, the pilot performed four quick stop maneuvers. The flight instructor reported that on the last quick stop, the helicopter slowed normally but then started a left yaw about 25 ft above ground level. The pilot noted the left yaw and attempted to correct it, but his pedal inputs did not stop the yaw. As the pilot tightened his grip on the collective, the hydraulic system turned off, likely due to the pilot inadvertently pressing the hydraulic cut-off switch, and the left yaw rapidly increased to a left spin. According to the flight instructor, the control loads “instantly became excessive,” and he noticed the hydraulic light on the caution warning panel was illuminated. The pilot intentionally pressed the hydraulic cut-off switch a total of three times, but hydraulic pressure was never restored. The flight instructor told the pilot that he was taking control of the helicopter. However, the pilot did not relinquish control. The flight instructor attempted to regain control of the helicopter but was unable to overcome the high control loads. The helicopter continued to spin, impacted the ground, rolled over, and came to rest on its right side. A postimpact fire consumed most of the helicopter. Although examination of the helicopter was limited due to fire damage, no preimpact abnormalities were identified with helicopter’s airframe and engine. The US Customs and Border Protection Air and Marine Operations Division reported that the agency’s selection process for the Air Interdiction Agent Program failed to properly identify that the pilot was not qualified for the program. Because the pilot did not have the qualifications and experience required for the Air Interdiction Agent Program, he did not have the prerequisite skill necessary to critically assess the situation given by the flight instructor. This resulted in the pilot applying improper corrective actions and failing to relinquish control of the helicopter to the flight instructor when directed, which contributed the accident. Probable Cause: The pilot receiving instruction’s untimely and unidentified inadvertent activation of the hydraulic cut-off switch, which turned off the hydraulic system while the helicopter was at slow airspeed followed by a rapid power increase, which resulted in a loss of control. Contributing was the pilot’s failure to relinquish control of the helicopter to the flight instructor when directed. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 15261 hours | CEN21LA216 | NTSB | Final report | 7baa4e156c49947f85e901d3a2db324c | Investigation completed | ||
2021 | Saturday 10 April 2021 | 14:30 LT | Cessna 150M | Private | N439WT | 15077917 | 1976 | Continental O-200 | Fatalities: 0 / Occupants: 2 | 0 | Substantial | Accident | Tishomingo, Oklahoma - United States of America | Take off | Private | Tishomingo, OK | Tishomingo, OK | Accident investigation report completed and information captured | The pilot reported he was taking off on personal flight when a gust of wind lifted the airplane's wing, and the airplane became airborne during his corrective control input. The pilot continued the climbout and attempted to gain airspeed, but the airplane did not accelerate and seemed to slow. The pilot elected to land the airplane to avoid trees that were ahead of him. The airplane touched down on a grass area just beyond the end of the runway but impacted in a drainage ditch about 100 ft. beyond the departure end of the runway that collapsed the nose landing gear. The airplane sustained substantial damage to the engine mounts at the nose landing gear. A Federal Aviation Administration inspector reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operations and that the engine was making power at impact. At the time of the accident, the pilot was taking off on runway 35 with a quartering wind from the northwest. The pilot reported that he may have encountered wind shear over the treetops which might have kept him low and slow to accelerate. Probable Cause: The pilot's decision to abort the takeoff on encountering a wind gust and his landing beyond the end of the runway that resulted in the airplane impacting a ditch collapsing the nose landing gear. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 5976 hours | CEN21LA188 | NTSB | Final report | 9ba0231e686c740160cb24824582fd89 | Investigation completed | 6 months | |
2021 | Tuesday 6 April 2021 | 11:30 | Beechcraft A36 Bonanza | 394 LLC | N18394 | E-1121 | 1977 | Continental IO520BA | Fatalities: 0 / Occupants: 1 | 0 | Substantial | Accident | near Arcadia Municipal Airport (X06), Arcadia, FL - United States of America | En route | Private | Arcadia Municipal Airport, FL (X06) | Venice Municipal Airport, FL (VNC/KVNC) | Accident investigation report completed and information captured | On April 6, 2021, about 1130 eastern daylight time, a Beech A36, N18394, was substantially damaged when it was involved in an accident near Arcadia, Florida. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. Shortly after takeoff, the pilot noticed the engine rpm had increased and oil pressure was zero. While returning to the airport the engine lost all power and the pilot performed a forced landing to a field. About 8 months prior to the accident, all six cylinders were replaced. Examination of the engine revealed the engine was seized and would not rotate. The reason for the loss of power was not determined. The engine was not made available for an NTSB postaccident examination. Probable Cause: A total loss of engine power for underdetermined reasons. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | 5443 hours | ERA21LA174 | NTSB | Final report | dad9c97408df80d7ae86fa6fdacd236d | Investigation completed | 2 years 1 month | |
2021 | Sunday 30 May 2021 | 08:37 | Cessna A188A | Agrícola de Servicios Aéreos del Meta - ASAM | HK-1477 | 18800696 | Fatalities: 1 / Occupants: 1 | 0 | Destroyed | Accident | near El Dólar airfield, Paz de Ariporo - Colombia | Manoeuvring (airshow, firefighting, ag.ops.) | Agricultural | Accident investigation report completed and information captured | During the execution of aerial spraying activities to rice fields in the La Reforma field, located in the Municipality of Paz de Ariporo - Casanare, the Cessna A188A aircraft, registration HK-1477, lost altitude during the execution of a turn, colliding with the ground. As a result of the impact, the aircraft suffered substantial damage and its sole occupant sustained fatal injuries. The investigation determined that the accident was caused by the loss of control in flight due to the execution of a turn maneuver, which probably exceeded the aerodynamic limits of the aircraft, generating a loss of lift at low altitude and the subsequent collision with the terrain. To this cause, a contributing factor related to the existence in the area of low level wind shear (LLWS) and clear air turbulence (CAT) in the atmospheric surface layer during low altitude flights was assigned. Probable Cause(s). - Loss of control in flight originating from the execution of a turn maneuver, which probably exceeded the aerodynamic limits of the aircraft, generating a loss of lift at low altitude and the followed collision with the terrain. Contributing factors: - Existence in the area of low-level wind shear (LLWS) and clear air turbulence (CAT) in the atmospheric surface layer during low-altitude flight execution. | You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | COL-21-20-DIACC | Aerocivil | Final report | c708373bdd02cd6f0df247287d10620b | Investigation completed | 10 months | ||||||
2021 | Tuesday 27 April 2021 | 23:00 | Learjet 60 | Emergencias | LV-HXK | 60-316 | Fatalities: 0 / Occupants: | 0 | Minor | San Fernando Airport, BA (FDO/SADF) - Argentina | Pushback / towing | Executive | San Fernando Airport, BA (FDO/SADF) | Information is only available from news, social media or unofficial sources | The plane was being towed along taxiway "C" to a remote location at the San Fernando International Airport (FDO/SADF), when it was hit by a van belonging to the airport operator. No injuries were reported. Material damage to the wing tip and windshield of the truck. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description | ||||||||||||
2021 | Saturday 29 May 2021 | ultralight | Fatalities: 0 / Occupants: 1 | 0 | Minor | Dahlemer Binz Airfield (EDKV) - Germany | Landing | Training | Dahlemer Binz Airfield (EDKV) | Information is only available from news, social media or unofficial sources | The ultralight was caught by a gust of wind. A wing hit the ground and the aircraft swerved into a meadow. | This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information. Corrections or additions? ... Edit this accident description |
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