Crash of a Britten-Norman BN-2B-27 Islander in Yerbabuena

Date & Time: Aug 12, 2024 at 1502 LT
Type of aircraft:
Operator:
Registration:
HK-2822
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bogotá - La Macarena
MSN:
2109
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Few minutes after takeoff from Bogotá-Guaymaral Airport, the crew encountered an unexpected situation and declared an emergency. He attempted an emergency landing when the airplane nosed down and crashed on hilly and wooded terrain located in Yerbabuena, about 10 km northeast of Guaymaral Airport. All four occupants were injured and the airplane was destroyed. It was en route to La Macarena on an ambulance flight, carrying two pilots and a medical team.

Crash of a Beechcraft C90 King Air near Yarumal: 4 killed

Date & Time: Mar 21, 2024 at 0720 LT
Type of aircraft:
Operator:
Registration:
HK-4684
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Montería - Medellín
MSN:
LJ-934
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The twin engine airplane departed Montería-Los Garzones Airport on an ambulance flight to Medellín, carrying two pilots, a doctor and a nurse. About 30 minutes into the flight, while cruising at an altitude of 19,000 feet, the airplane initiated a descent and the speed started to decrease until it stalled and crashed in a prairie, bursting into flames. All four occupants were killed.

Crash of a Cessna 421C Golden Eagle III in Valledupar: 1 killed

Date & Time: Jan 7, 2024 at 1140 LT
Operator:
Registration:
HK-4983
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Valledupar – Bogotá
MSN:
421C-0346
YOM:
1977
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The airplane was operated on an ambulance flight from Valledupar to Bogotá-Guaymaral Airport, carrying six people, a mother and son, a doctor, a nurse and two pilots. After takeoff from runway 02/20, the airplane reached the altitude of 50 metres then stalled and crashed near trees, bursting into flames. Five occupants were injured and the doctor was killed. The airplane was destroyed by a post crash fire.

Crash of a Piper PA-31-350 Navajo Chieftain in Medellín: 8 killed

Date & Time: Nov 21, 2022 at 1015 LT
Operator:
Registration:
HK-5121
Flight Phase:
Survivors:
No
Site:
Schedule:
Medellín – Pizarro
MSN:
31-7652004
YOM:
1976
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The twin engine airplane was chartered by the Grupo San Germán Express to carry a team of six people from Medellín to Pizarro, Chocó. Shortly after takeoff from runway 02 at Medellín-Enrique Olaya Herrera Airport, while in initial climb, the crew encountered engine problems. The airplane went out of control and crashed onto a house located in the district of Belén Rosales, less than 500 metres from the runway end, bursting into flames. The house and the aircraft were destroyed and all 8 occupants were killed.
Crew:
Julián Aladino, pilot,
Sergio Guevara Delgado, copilot.
Passengers:
Jorge Cantillo Martínez,
Dubán Ovalle Quintero,
Anthony Mosquera Blanquiceth,
Pedro Pablo Serna,
Melissa Pérez Cuadros,
Nicolás Jiménez.

Crash of a Basler BT-67 in Villavicencio

Date & Time: Apr 13, 2022 at 1303 LT
Type of aircraft:
Operator:
Registration:
PNC-0257
Flight Type:
Survivors:
Yes
Schedule:
Florencia – Villavicencio
MSN:
9670
YOM:
1943
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing on runway 23 at Villavicencio-La Vanguardia Airport, the airplane veered off runway to the left and entered a grassy area. It rolled for few hundred metres then the pilot attempted to takeoff when the left wing dropped. The aircraft stalled, impacted trees and crashed about 200 metres to the right of the runway 05 threshold. All 14 occupants were rescued, among them few were injured.

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:

Crash of a Cessna T303 Crusader in Bojacá: 1 killed

Date & Time: Jan 8, 2021 at 1320 LT
Type of aircraft:
Operator:
Registration:
HK-3856-G
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Girardot – Bogotá
MSN:
303-00010
YOM:
1981
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot, sole on board, departed Flandes-Santiago Vila Airport runway 02 at 1257LT on a flight to Guaymaral in Bogotá. En route, weather conditions worsened and the visibility was poor. While cruising at an altitude of 9,260 feet, the twin engine airplane impacted trees and crashed in a wooded and hilly terrain located near Bojacá. The aircraft was destroyed by impact forces and the pilot was killed.
Probable cause:
The accident was the consequence of a controlled flight into terrain after the decision of the pilot to continue the flight under VFR mode in IMC conditions.
The following contributing factors were identified:
- The pilot took the decision to continue the flight to destination instead of returning to Flandes (Girardot) or to divert to the alternate airport,
- A low situational awareness on part of the pilot who failed to take into account the geographical environment and to maintain a safe separation from the terrain.
Final Report:

Crash of a Cessna 208B Grand Caravan in Guaymaral

Date & Time: Sep 22, 2020 at 0655 LT
Type of aircraft:
Registration:
HK-4669G
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Guaymaral – Flandes
MSN:
208B-0968
YOM:
2002
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13220
Captain / Total hours on type:
1506.00
Aircraft flight hours:
2830
Circumstances:
After takeoff from Guaymaral-Flaminio Suárez Camacho Airport runway 29, while climbing to a height of 200 feet, the engine suffered and explosion and lost power. The airplane started to descend, impacted a brick wall and lost its undercarriage. It then crash landed in a prairie and slid for few dozen metres before coming to rest. All five occupants escaped uninjured. The accident occurred three minutes after takeoff.
Probable cause:
The investigation determined that the accident was caused by the following probable causes:
- Emergency landing of the aircraft on an unprepared field, as a result of a decrease in power, generated by engine failure.
- An engine failure caused by the fracture of three (3) blades of the rotor disk of the high pressure compressor, which caused severe backwards damage to the hot and power section.
Contributing Factors:
- Non-compliance in the engine maintenance process, of what was ordered in AD. No. 2014-17-08R1 FAA (year 2014), which establishes the replacement of the engine blades high pressure compressor in anticipation of material failures in these components.
- Deficient maintenance processes by the provider of this service to the aircraft HK4669G, by not detecting the condition of the high-pressure rotor blades in the boroscopic inspections of the high pressure during routine boroscopic inspections.
- Deficient verification of the Operator's contracted maintenance processes, by not verifying the quality and compliance the quality and full compliance of these processes by the maintenance service provider.
Final Report:

Crash of a Piper PA-31-310 Navajo in Bogotá: 4 killed

Date & Time: Feb 12, 2020 at 1544 LT
Type of aircraft:
Operator:
Registration:
HK-4686
Flight Phase:
Survivors:
No
Schedule:
Bogotá – Villagarzón
MSN:
31-344
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1890
Captain / Total hours on type:
250.00
Copilot / Total flying hours:
646
Aircraft flight hours:
10251
Circumstances:
Shortly after takeoff from Bogotá-Guaymaral Airport, while in initial climb, the crew informed ATC about the failure of the right engine. He was cleared to return for an emergency and completed a circuit to land on ruwnay 11. On final, the airplane lost height and crashed in a wooded area located about 800 metres short of runway, bursting into flames. The aircraft was destroyed by a post crash fire and all four occupants were killed.
Probable cause:
The investigation determined that the accident was caused by the following probable cause(s):
- Loss of in-flight control as a result of slowing below Minimum Control Speed and drag, generated by the failure of the right engine (No. 2).
- Failure of engine No. 2, due to lack of lubrication, possibly caused by oil leakage through an 11.5 mm fracture, found in one of the sides of cylinder No. 2 at the height of the intake valves.
- Inappropriate application by the crew of the emergency procedure for landing with an inoperative engine, by not declaring the emergency, not feathering the propeller of the inoperative engine and configuring the aircraft early for landing (with landing gear and flaps) without having a safe runway, making it difficult to control the aircraft and placing it in a condition of loss of lift and control.

Contributing Factors:
- Failure of the operator to emphasize in the crew training program the techniques and procedures to be followed in the event of engine failure, among others, the declaration of emergency to ATC, the flagging of the propeller of the inoperative engine, the care in the application of power to the good engine so as not to increase yaw and not to configure the aircraft until landing has been assured.
- Lack of emergency calls by the crew, which denotes deficiencies in the Operator's Safety Management System, and which prevented the early warning of the aerodrome support services and deprived the crew of possible assistance from other aircraft or from the same operator.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Popayán: 7 killed

Date & Time: Sep 15, 2019 at 1406 LT
Operator:
Registration:
HK-5229
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Popayán - López de Micay
MSN:
31-7405212
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
3291
Captain / Total hours on type:
991.00
Copilot / Total flying hours:
300
Copilot / Total hours on type:
55
Aircraft flight hours:
12304
Circumstances:
The twin engine airplane departed Popayán-Guillermo León Valencia Airport runway 26 at 14:06:06. The aircraft encountered difficulties to gain sufficient height. About 20 seconds after liftoff, at a speed of 82 knots, the aircraft rolled to the right then entered an uncontrolled descent and crashed onto two houses located 530 metres past the runway end. Two passengers were seriously injured and seven other occupants were killed.
Probable cause:
A loss of in-flight control of the aircraft due to possible excess weight. The aircraft probably managed to take off due to "ground effect", but, once in the air and out of ground effect, it was not able to obtain the speed that would allow it to safely accomplish the climb.
Contributing Factors:
- Absence of Dispatch procedures of the operator to perform a correct Weight and Balance of the aircraft, and the effective control of the boarded cargo.
- Incorrect calculation of the weight and balance of the aircraft by the crew, by not considering all the cargo that was loaded, causing the aircraft to take off with a possible excess weight.
- Weak operational safety management processes of the operator by not considering the operating characteristics of airfields such as Popayán (high altitude, high ambient temperature) that significantly limit the operation.
Final Report: