Crash of a Beechcraft B100 King Air in Lake Simcoe

Date & Time: Aug 13, 2024 at 1225 LT
Type of aircraft:
Operator:
Registration:
C-FTFT
Flight Type:
Survivors:
Yes
Schedule:
Toronto - Lake Simcoe
MSN:
BE-49
YOM:
1978
Flight number:
TOR804
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew departed Toronto-Lester Bowles Pearson Airport in the morning to perform training at Lake Simcoe Regional Airport under flight number TOR804. After performing several approaches and touch-and-go, the crew was completing an approach to runway 28 when the airplane belly landed. It slid for few dozen metres before coming to a halt, bursting into flames. All three crew members evacuated safely but the airplane was totally destroyed by fire.

Crash of a Transall C-160T in Kayseri

Date & Time: Jan 25, 2024
Type of aircraft:
Operator:
Registration:
69-036
Flight Type:
Survivors:
Yes
Schedule:
Kayseri - Kayseri
MSN:
D036
YOM:
1969
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Kayseri-Erkilet Airport on behalf of the 12 Wing. While flying in the vicinity of the airport, he encountered technical problems and elected to return for an emergency landing. The crew performed a very low approach over the surrounding districts before landing on runway 25. After touchdown, the airplane apparently encountered issues with the left main gear, slid for few hundred metres then veered off runway to the left and came to rest in a grassy area. All crew members escaped uninjured.

Crash of a Beechcraft C99 Airliner in Litchfield: 2 killed

Date & Time: Aug 22, 2023 at 1741 LT
Type of aircraft:
Operator:
Registration:
N55RP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Auburn - Auburn
MSN:
U-198
YOM:
1982
Flight number:
WIG634
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew departed Auburn-Lewiston Municipal Airport on a local training mission under callsign WIG634. After making a circuit over Sebago Lake located southwest of the airport, the crew continued to the northeast when control was lost. The airplane entered a descent with a rate of 7,300 feet per minute until it crashed in a wooded area located near Mt Oak Hill, about 25 km northeast of Auburn-Lewiston Municipal Airport. The airplane was destroyed and both occupants were killed.

Crash of a Cessna 208B Grand Caravan in Chrcynno: 6 killed

Date & Time: Jul 17, 2023 at 1730 LT
Type of aircraft:
Operator:
Registration:
SP-WAW
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Chrcynno - Chrcynno
MSN:
208B-0854
YOM:
2000
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The crew was completing a local training flight at Chrcynno Aerodrome. After takeoff from a grassy runway, the single engine airplane went out of control and crashed onto a hangar located nearby the control tower. Two pilots were injured while a third was killed as well as five people in the hangar. Weather conditions were considered as marginal at the time of the accident with a thunderstorm passing over the area.

Crash of a Learjet 35A at Hohn AFB: 2 killed

Date & Time: May 15, 2023 at 1247 LT
Type of aircraft:
Operator:
Registration:
D-CGFQ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Hohn - Hohn
MSN:
35-676
YOM:
1993
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
11955
Captain / Total hours on type:
8083.00
Copilot / Total flying hours:
10349
Copilot / Total hours on type:
6265
Aircraft flight hours:
9846
Aircraft flight cycles:
6739
Circumstances:
On the day of the occurrence, six Learjet flight crews of the operator involved planned to take off almost at the same time from Hohn Military Airport to different missions. The airplane involved was the third to take off. Two pilots were on board of the Learjet 35A. The Pilot Flying (PF) sat in the left-hand seat and the Pilot Monitoring (PM) in the right. It was planned to fly from Hohn to Wunstorf Military Airport and conduct several instrument approaches for training purposes of the local air traffic control personnel. At the same time, the flight was to be used as proficiency check for the pilot in the left-hand seat for his type and instrument rating for Learjet 20/30. According to the Cockpit Voice Recorder (CVR) recording, the pilots completed the Before Starting Engine checklist prior to starting the engines. A Yaw Damper check and a so-called Full Travel check of the flight controls were performed, among other things. At 1224 hrs, the right engine was started; at 1226 hrs, the left. At 1237 hrs, while still on taxiway C3, the take-off emergency briefing was performed with the words: „[…] when airborn keine [no] Items ausser [except] gear below 500 ft, continue climb, in real life accelerate to V2 plus 30, Klappen [flaps] rein, slight climb weiter auf [to] […]“. At 1238 hrs, another Learjet received take-off clearance with simulated engine failure from the Tower. That flight crew asked over the radio if the single engine take-off was approved and the Tower once again acknowledged it. After the take-off of that Learjet, the flight crew taxied with the airplane involved on the runway to Ramp 1, turned and waited for the clearance to line up on runway 26. At 1244 hrs, the flight crew received the instruction to roll on to runway 26 and wait. They completed the Line-up check and the Before Take-off check. They planned to take-off with flaps 8° and engine full thrust with N1 of 96.6%. After they had received take-off clearance at about 1247 hrs, the airplane accelerated and took off at 1247:34 hrs, according to witnesses in the area of taxiway C3, and entered climb. According to the CVR recording, after take-off the PF instructed the PM to retract the landing gear and engage the Yaw Damper. At 1247:39 hrs, the PM responded with: “Vorab verlierst du simuliert das rechte Triebwerk (in advance, you will lose the right engine)“, the PF acknowledged it by saying: “Copy, gear up“. Then the thrust of the right engine reduced, the left engine maintained the set take-off thrust. At that time, indicated speed was about 160 kt, according to the FDR. At 1247:44 hrs, the PF instructed: “Damper on”. At 1247:45 hrs, the PM answered “Jawohl (yes)”, almost at the same time the PF said quietly: “Oh shit“. At 1247:44 hrs, the PF called out loud several times: “Fuck” and at 1247:54 hrs the PM several times “Shit”. At 1247:55 hrs, the last recording was the landing gear warning generated by the airplane: “Too low“. From the PM’s announcement about the simulated engine failure at 1247:39 hrs until the impact, Hohn Tower transmitted traffic information regarding two Tornado aircraft in the vicinity and instructed the frequency change to Hohn Radar. Witnesses observed that the airplane performed a sort of snap roll and then crashed to the ground at the end of the runway. On impact, an explosive fireball occurred. The pilots suffered fatal injuries and the airplane was destroyed.
Probable cause:
The accident, loss of control of the airplane, was the result of an untimely or significantly too low rudder deflection to correct the asymmetric thrust after initiation of a simulated engine failure. The large yaw angle resulted in a stall of the vertical tail and on the wing and an uncontrolled roll of the airplane. It was not possible to determine without doubt the reason for the untimely or significantly too low rudder deflection.
Final Report:

Crash of a Cessna 208B Grand Caravan in Puerto Ayacucho: 5 killed

Date & Time: Nov 6, 2022 at 0656 LT
Type of aircraft:
Operator:
Registration:
AMB-0956
Flight Type:
Survivors:
No
Schedule:
Puerto Ayacucho - Puerto Ayacucho
MSN:
208B-0977
YOM:
2002
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The single engine airplane was engaged in a local training flight at Puerto Ayacucho Airport, carrying five pilots. While completing a turn on approach to runway 04, the airplane went out of control and crashed in a wooded area located about 3 km south of the airport, bursting into flames. The airplane was totally destroyed by impact forces and a post crash fire and all five occupants were killed. Puerto Ayacucho Airport is named Cacique Aramare but the military side is named José Antonio Páez.
Crew:
Cpt José Castillo Tovar,
Cpt Jefferson Aular,
1st Lt Roberto Aponte,
Lt Santiago Collado,
Lt Joé Rivas.

Crash of a Piper PA-60 Aerostar (Ted Smith 600) in South Haven: 2 killed

Date & Time: Aug 2, 2022 at 1030 LT
Registration:
N9784Q
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
South Haven - South Haven
MSN:
60-0416-143
YOM:
1977
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3250
Copilot / Total flying hours:
28500
Copilot / Total hours on type:
0
Aircraft flight hours:
11197
Circumstances:
A friend of the copilot reported this was the multiengine airplane’s first flight since the (single engine-rated) copilot purchased it five years before the accident. He stated that the purpose of the flight was to conduct touch-and-go landings. Another (multiengine-rated) pilot was flying in the left seat, with the copilot flying in the right seat. On the day of the accident, when the friend arrived at the airport, he noticed that the airplane was not in the traffic pattern. After a few hours, he became concerned and reported the airplane missing to local authorities, and it was found the next morning in a heavily wooded area about one mile away from the airport. There were no witnesses to the accident. Post accident examination of the wreckage revealed that the airplane’s left propeller displayed signatures indicative of low rotational speed at impact, suggesting that the airplane’s left engine may have lost at least partial power. The right propeller showed signatures consistent with high rotational speed/power settings at the time of impact. Examination of the left engine’s fuel servo revealed that it was heavily contaminated with sediment and that the fuel pump had weak suction and compression. Either or both of these conditions could have reduced the left engine’s performance during the flight. Additionally, the airplane was found with its wing flaps extended, the landing gear not retracted, and the left engine’s propeller was not feathered. A representative from the airplane’s type certificate holder stated that, depending on the airplane’s takeoff weight, it generally could not maintain level flight during an engine-out condition unless the flaps and landing gear were up and the failed engine’s propeller was feathered. While there were no witnesses to the accident or other recorded data to suggest what flight regime the airplane was in when the loss of engine power occurred, given the stated purpose of the flight and the findings of the post accident examination of the wreckage, it is likely that, while maneuvering the airplane in the airport traffic pattern, the airplane’s left engine lost power and the airplane subsequently impacted trees and terrain. Given the configuration of the wing flaps and landing gear and the unfeathered position of the left propeller, it is likely that the airplane’s single-engine performance was degraded.
Probable cause:
A loss of power to the left engine due to contamination of the fuel system. Contributing to the accident was the pilots’ failure to properly configure the airplane for flight with one engine inoperative.
Final Report:

Crash of a Cessna 340 in Covington: 2 killed

Date & Time: Apr 21, 2022 at 1844 LT
Type of aircraft:
Operator:
Registration:
N84GR
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Covington - Covington
MSN:
340-0178
YOM:
1973
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
0
Captain / Total hours on type:
0.00
Copilot / Total flying hours:
3148
Copilot / Total hours on type:
0
Aircraft flight hours:
7581
Circumstances:
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.
Probable cause:
The private pilot’s loss of control in flight, which resulted in a collision with terrain. Contributing to the accident was the student pilot’s decision to obtain flight instruction from the private pilot and the private pilot's insufficient qualifications to fly or to provide flight instruction in a multi-engine airplane.
Final Report:

Crash of a Britten-Norman BN-2A-9 Islander in Culebra

Date & Time: Feb 15, 2022 at 0955 LT
Type of aircraft:
Operator:
Registration:
N821RR
Flight Type:
Survivors:
Yes
Schedule:
San Juan - Culebra
MSN:
338
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
16550
Captain / Total hours on type:
0.00
Copilot / Total flying hours:
6000
Copilot / Total hours on type:
5000
Aircraft flight hours:
2864
Circumstances:
The pilot was receiving flight training as a new hire, and the accident occurred during his first flight in the airplane and the first landing. The pilot stated the approach was flown at the upper end of the allowable approach speed, and about 100 ft above the normal glidepath. During the landing, all three of the airplane’s landing gear touched down at the same time, the airplane immediately veered right, and continued off the right side of the runway. The airplane sustained substantial damage to the right-wing structure. The flight instructor chose an airport with a challenging approach that required a special training program prior to the first landing. The approach procedure requires a left 40° turn then rolling wings level just before touchdown. It is likely that the airplane’s descent rate during landing exceeded the airplane’s capability, which resulted in a hard landing and failure of the right-wing structure.
Probable cause:
The flight crew’s failure to arrest the descent rate during the non-standard approach, which resulted in a hard landing and failure of the right-wing structure. Contributing was the flight instructor’s selection of a challenging approach for initial training.
Final Report:

Crash of a Douglas DC-3C near Restrepo: 3 killed

Date & Time: Jul 8, 2021 at 0709 LT
Type of aircraft:
Operator:
Registration:
HK-2820
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Villavicencio - Villavicencio
MSN:
20171
YOM:
1944
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
16923
Captain / Total hours on type:
16680.00
Copilot / Total flying hours:
9387
Copilot / Total hours on type:
8170
Aircraft flight hours:
18472
Circumstances:
The twin engine airplane departed Villavicencio-La Vanguardia Airport Runway 05 at 0659LT on a training flight consisting with a proficiency check of the captain. On board were one instructor, one captain and one mechanic. About 10 minutes into the flight, while cruising at an altitude of 6,000 feet over mountainous terrain in Instrument Meteorological Conditions, the airplane impacted trees and crashed on the slope of a hilly terrain located in the region of Restrepo. The wreckage was found three days later. All three crew members were killed.
Probable cause:
Probable causes:
- Controlled flight into terrain during the execution of the IFR departure procedure VVC2A, during which the crew mistakenly turned left, contrary to the procedure, heading towards the mountainous area at the foothills of the eastern range, where the impact occurred.
- Loss of situational awareness by the crew, which, for reasons that could not be determined, apparently made a controlled left turn, contrary to the indications of the VVC2A departure procedure, even though it was an experienced crew familiar with the operating area.

The following contributing factors were identified:
- Lack of operator standards, as there was no detailed, organized, and sequential instructional plan and syllabus for the crew to follow during each maneuver, such as the VVC2A instrument departure.
- Lack of operator standards, as there was no specific syllabus for the planning and execution of the Recurrent Check, taking into account, among other aspects, the composition of the aircraft crew, consisting of two instructor pilots, one of whom was conducting the check on the other.
- Inadequate planning and supervision of the training flight by the operator, as they did not conduct a specific risk analysis of the flight, did not monitor its preparation and execution, did not provide details in a flight order or other document, considering especially the composition of the aircraft crew, consisting of two instructor pilots, one of whom was conducting the check on the other.
- Deficient planning and preparation of the flight by the crew, as they informally changed the VFR Flight Plan to IFR, apparently did not conduct a complete and adequate briefing, were unaware of or did not consider the VVC2A SID for the start of the IFR flight, and omitted several IFR flight procedures.
- Crew's neglect of the following IFR flight procedures:
- Not specifying a route and an IFR departure procedure in the IFR Flight Plan.
- Not requesting complete authorization from ATC to initiate an IFR flight. At no time did they mention the VVC2A departure, which was key to the verbally proposed plan before takeoff.
- Not defining or requesting from ATS which standard departure procedure or other they would use to initiate the IFR flight, in which they would encounter IMC shortly after takeoff.
- Not requiring ATC to assign a transponder code before takeoff or at any other phase of the flight, or selecting code 2000 as they did not receive instructions from ATS to activate the transponder.
- Likely not activating the transponder before takeoff and/or not verifying its correct operation before takeoff or immediately once the aircraft was in the air.
- Inaccurate use of phraseology with non-standard terminology in their transmissions with ATC.
- Insufficient experience and training in IFR flights by the crew, despite their extensive experience with the equipment. Much of this experience had been gained in the eastern region of the country, where the majority of DC3 flights are conducted in VMC and under VFR, with no opportunity for the practical execution of IFR procedures.
- Overconfidence of the crew, influenced by factors such as the high flight experience and DC3 equipment experience of the two pilots in the crew, their status as instructor pilots, the relatively low operational demand of the flight mission, and the knowledge, familiarity, and confidence of both crew members with the aerodrome's characteristics, the surrounding area, and especially the peculiarities and risks of the terrain to the west of the takeoff path.
- Non-observance by air traffic control of the following IFR flight procedures initiated by HK2820:
- Failure to issue complete authorization to the aircraft for the IFR flight before initiating the flight or at any other time.
- Failure to issue a standardized instrument departure, SID, or any other safe departure procedure to the aircraft. At no time did ATC mention the VVC2A departure, which was crucial for carrying out the plan verbally proposed by the crew.
- Failure to provide the aircraft with a transponder code before takeoff or at another appropriate time, or to verify its response. This process started only 03:11 minutes after the aircraft took off, so positive radar contact verification was only achieved 04:58 minutes after takeoff, delaying radar presentation and limiting positive flight control.
- Late transfer of aircraft control from the Control Tower to Approach Control (03:35 minutes after takeoff), not immediately after the aircraft was airborne as it should have been, considering prevailing IMC flight conditions in the vicinity of the aerodrome.
- Operating with an incomplete radar display configuration in Approach Control, with insufficient symbology, depriving control of references and judgment elements for an accurate location of the aircraft and its left turn from the path.
- Failure to observe radar surveillance techniques and procedures.
- Inaccurate use of phraseology with non-standard terminology in their transmissions with the aircraft.
- Lack of situational awareness by both the crew and ATC during a flight that, perhaps because it seemed routine, led both parties to omit elementary IFR flight procedures, disregarding the inherent risks of an operation in IMC conditions, with strict IFR procedures that needed to be followed, considering, among other things, the aerodrome's proximity to a mountainous area.
Final Report: