Crash of a Piper PA-31-310 in Guatemala City

Date & Time: Nov 21, 2015 at 1240 LT
Type of aircraft:
Registration:
C6-TAK
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Guatemala City - Guatemala City
MSN:
31-228
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
191
Copilot / Total flying hours:
4735
Aircraft flight hours:
7600
Circumstances:
The crew departed Guatemala City-La Aurora Airport on a local training flight. Shortly after takeoff from runway 02, while in initial climb, the aircraft entered a right turn then lost height and crashed near an industrial building located about 900 metres from the runway 20 threshold. The aircraft was destroyed by impact forces and a post crash fire. Both pilots escaped uninjured.
Probable cause:
The aircraft stalled at low height after takeoff due to a poor crew coordination about flight controls.
Final Report:

Crash of a Piper PA-31-325 Navajo C/R in Bogotá: 2 killed

Date & Time: Oct 3, 2015 at 1212 LT
Type of aircraft:
Registration:
HK-3909G
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bogotá – Medellín
MSN:
31-7612070
YOM:
1976
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10377
Captain / Total hours on type:
121.00
Aircraft flight hours:
5209
Circumstances:
Shortly after takeoff from Bogotá-Guaymaral Airport, while climbing, the pilot declared an emergency after the failure of the right engine. He attempted an emergency landing in an open field when the aircraft crashed in a prairie located near the Los Andes hippodrome, some 5 km northeast of Guaymaral Airport, bursting into flames. A passenger was seriously injured while both other occupants were killed.
Probable cause:
Failure of the right engine during initial climb due to the failure of internal components. The high density altitude was considered as a contributing factor as its affected the aircraft performances.
Final Report:

Crash of a Piper PA-31-310 Navajo in Los Camastros: 1 killed

Date & Time: Oct 2, 2015 at 1203 LT
Type of aircraft:
Operator:
Registration:
C-GCMD
Flight Phase:
Survivors:
No
MSN:
31-7912101
YOM:
1979
Location:
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 Managua-Augusto C. Sandino Airport at 0934LT on a flight for the Australian Company CSA Global, taking part to a geological mission dedicated to the construction of a canal. In unknown circumstances, the twin engine aircraft went out of control and crashed in a field located in Los Camastros, about one km north of Veracruz. The pilot was killed and maybe tried to use a parachute before the crash as one was found in the wreckage.

Crash of a Piper PA-31-425 Pressurized Navajo in Conrado Castillo: 6 killed

Date & Time: Nov 14, 2014 at 1730 LT
Type of aircraft:
Operator:
Registration:
XB-ZAX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
San Luis Potosí – Ciudad Victoria – Torreón
MSN:
31-46
YOM:
1967
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine aircraft departed San Luis Potosí on a flight to Torreón with an intermediate stop in Ciudad Victoria, carrying five passengers and one pilot. At the end of the afternoon, while descending to Ciudad Victoria Airport, the pilot encountered poor weather conditions. Too low, the aircraft impacted trees and crashed in a hilly terrain located near Conrado Castillo. The wreckage was found the following morning about 60 km northwest of Ciudad Victoria Airport. The aircraft disintegrated on impact and all six occupants were killed.
Pilot:
Juan José Castro Maldonado
Passengers:
Maribel Lumbreras,
Paulina García Lumbreras,
Lucero Salazar Méndez,
Juana Lumbreras Ruiz,
Guadalupe Lumbreras Ruiz.

Crash of a Piper PA-31-325 Navajo in Grand Manan Island: 2 killed

Date & Time: Aug 16, 2014 at 0512 LT
Type of aircraft:
Operator:
Registration:
C-GKWE
Flight Type:
Survivors:
Yes
Schedule:
Saint John - Grand Manan Island
MSN:
31-7812037
YOM:
1978
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
17400
Copilot / Total flying hours:
304
Copilot / Total hours on type:
67
Circumstances:
The Atlantic Charters Piper PA-31aircraft had carried out a MEDEVAC flight from Grand Manan, New Brunswick, to Saint John, New Brunswick. At 0436 Atlantic Daylight Time, the aircraft departed Saint John for the return flight to Grand Manan with 2 pilots and 2 passengers. Following an attempt to land on Runway 24 at Grand Manan Airport, the captain carried out a go-around. During the second approach, with the landing gear extended, the aircraft contacted a road perpendicular to the runway, approximately 1500 feet before the threshold. The aircraft continued straight through 100 feet of brush before briefly becoming airborne. At about 0512, the aircraft struck the ground left of the runway centreline, approximately 1000 feet before the threshold. The captain and 1 passenger sustained fatal injuries. The other pilot and the second passenger sustained serious injuries. The aircraft was destroyed; an emergency locator transmitter signal was received. The accident occurred during the hours of darkness.
Probable cause:
Findings as to causes and contributing factors:
1. The captain commenced the flight with only a single headset on board, thereby preventing a shared situational awareness among the crew.
2. It is likely that the weather at the time of both approaches was such that the captain could not see the required visual references to ensure a safe landing.
3. The first officer was focused on locating the runway and was unaware of the captain’s actions during the descent.
4. For undetermined reasons, the captain initiated a steep descent 0.56 nautical mile from the threshold, which went uncorrected until a point from which it was too late to recover.
5. The aircraft contacted a road 0.25 nautical mile short of the runway and struck terrain.
6. The paramedic was not wearing a seatbelt and was not restrained during the impact sequence.
Findings as to risk:
1. If cockpit data recordings are not available to an investigation, then the identification and communication of safety deficiencies to advance transportation safety may be precluded.
2. If crew members are unable to communicate effectively, then they are less likely to anticipate and coordinate their actions, which could jeopardize the safety of flight.
3. If crew resource management training is not provided, used and continuously fostered, then there is a risk that pilots will be unprepared to avoid or mitigate crew errors encountered during flight.
4. If an actual weight and balance cannot be determined, then the aircraft may be operating outside of its approved limits, which could affect the aircraft’s performance characteristics.
5. If pre-computed weight and balance forms do not include standard items, then it increases the likelihood of omissions in weight and balance calculations, which increases the risk of inadvertently overloading or incorrectly loading the aircraft.
6. If organizations carry out a maintenance task that they consider to be elementary work and the task is not approved as an elementary work task, then there is a risk that the aircraft will not conform to its type design, which could jeopardize the safety of flight.
7. If individuals are performing maintenance tasks for which they have not received approved training, then there is a risk that the task will not be performed in accordance with the manufacturer’s instructions.
8. If components are not installed in accordance with the manufacturer’s instructions, then occupants are at a greater risk of injury or death during an incident or accident if these components are not properly secured.
9. If organizations do not record when maintenance is carried out, then the proper completion of tasks cannot be confirmed, and there is a risk that the aircraft will not conform to its type design, which could jeopardize the safety of flight.
10. If an aircraft is modified without regulatory approval and without supporting documentation, then the aircraft is not in compliance with all applicable standards of airworthiness, which could jeopardize the safety of flight.
11. If an operator undertakes unapproved changes to a supplemental type certificate, then there is a risk that the aircraft will not be airworthy, which could jeopardize the safety of flight.
12. If organizations do not use modern safety management practices, then there is an increased risk that hazards will not be identified and risks mitigated.
13. If Transport Canada does not adopt a balanced approach that combines thorough inspections for compliance with audits of safety management processes, unsafe operating practices may not be identified, thereby increasing the risk of accidents.
14. If organizations contract aviation companies to provide a service with which the organizations are not familiar, then there is an increased risk that safety deficiencies will go unnoticed, which could jeopardize the safety of the organizations’ employees.
15. If passengers are not provided with a regular safety briefing, then there is an increased risk that they will not use the available safety equipment or be able to perform necessary emergency functions in a timely manner to avoid injury or death.
16. If passengers are not properly restrained, then there is an increased risk of injuries and death to those passengers and the other occupants in the event of an accident.
17. If carry-on baggage, equipment or cargo is not restrained, then occupants are at a greater risk of injury or death if these items become projectiles in a crash.
18. If carry-on baggage, equipment or cargo is not restrained, then there is an increased risk that the occupants’ access to normal and emergency exits, and to safety equipment, will be completely or partially blocked.
19. If pilots continue an approach below published minimum descent altitudes without seeing the required visual references, then there is a risk of collision with terrain and/or obstacles.
20. If current charts and databases are not used, then navigational accuracy and obstacle avoidance cannot be assured.
21. If GPS (global positioning system) approaches are conducted without the approved Operations Specification, then there is a risk that the pilot’s training and knowledge will be inadequate to safely conduct the approach.
22. If medical symptoms/conditions are not reported to Transport Canada, then it negates some of the safety benefit of examinations and increases the risk that pilots will continue to fly with a medical condition that poses a risk to safety.
Other findings:
1. The pilot who installed the air ambulance system did not have approved training, nor was the pilot approved to carry out elementary work.
2. Atlantic Charters was not approved to install the air ambulance system as an elementary work task.
3. Atlantic Charters’ pre-computed weight and balance form did not include a line item to indicate nacelle fuel.
4. The semi-annual safety training offered to paramedics in lieu of safety briefings prior to flights did not meet regulatory requirements.
Final Report:

Crash of a Piper PA-31P Pressurized Navajo in Częstochowa: 11 killed

Date & Time: Jul 5, 2014 at 1611 LT
Type of aircraft:
Registration:
N11WB
Flight Phase:
Survivors:
Yes
Schedule:
Częstochowa - Częstochowa
MSN:
31P-7630005
YOM:
1976
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
996
Captain / Total hours on type:
40.00
Circumstances:
The twin engine aircraft was engaged in a series of skydiving flights at Częstochowa-Rudniki Airport, Silesia. It took off from runway 26C with 11 skydivers and one pilot on board. During initial climb, at an altitude of 100 metres, the pilot encountered technical problems with the engines and elected to make an emergency landing. He informed the passengers about the emergency situation and reduced his altitude when the aircraft rolled to the left to an angle of 70° then stalled and crashed in a wooded area, bursting into flames. The wreckage was found 4,200 metres past the runway end. Three skydivers were seriously injured while 9 other occupants were killed. Few minutes later, two of the survivors died from their injuries.
Probable cause:
The following findings were identified:
- The aircraft was operated without a valid CofA,
- Failure of the left engine during initial climb after the crankshaft failed, causing the malfunction of the propeller that could not be feathered, resulting in an asymmetry that caused the aircraft to enter a stall condition. Damages to the pin clutch connecting the crankshaft to the drive shaft of the right engine transmission could be due to the following causes: an earlier impact of a propeller's blade with an obstacle, in circumstances and time which could not be determined and/or a long-term fatigue process caused by uneven engine operation (one of the cylinders was replaced on the right engine),
- Improper maintenance of the aircraft,
- The left engine was producing low power due to improper operation,
- The fuel in the tanks did not meet the engine manufacturer's requirements,
- The aircraft was modified in violation of its Type Certificate,
- A high ambiant temperature.
Final Report:

Crash of a Piper PA-31-310 Navajo near Coromoro: 2 killed

Date & Time: May 3, 2014 at 1023 LT
Type of aircraft:
Operator:
Registration:
C-GSVM
Flight Phase:
Survivors:
No
Site:
Schedule:
Bucaramanga - Bucaramanga
MSN:
31-109
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4000
Captain / Total hours on type:
1400.00
Aircraft flight hours:
11000
Circumstances:
The twin engine aircraft departed Bucaramanga-Palonegro Airport at 0804LT on a geophysical mission over the Coromoro Region, Santander. At 1000LT, the last radio contact was recorded with the pilot. While flying in marginal weather conditions (low clouds), the aircraft impacted the slope of a mountain located near Coromoro. The wreckage was found two days later at an altitude of 4,500 metres, some 98 km south of Bucaramanga. The aircraft disintegrated on impact and both occupants were killed, among them Peter Moore, co-founder of Oracle Geoscience International and Neville Ribeiro, the pilot.
Probable cause:
Controlled flight into terrain after the pilot was flying under VFR mode in IMC conditions. It was determined that the accident occurred after the pilot suffered a loss of situational awareness while flying under VFR mode in low clouds conditions.
Final Report:

Crash of a Piper PA-31-310 Navajo in Deán Funes

Date & Time: Apr 27, 2014 at 1915 LT
Type of aircraft:
Operator:
Registration:
LV-JGN
Flight Type:
Survivors:
Yes
Schedule:
Termas de Río Hondo – Río Cuarto
MSN:
31-213
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
462
Captain / Total hours on type:
8.00
Aircraft flight hours:
5245
Circumstances:
The twin engine aircraft departed Termas de Río Hondo Airport on a flight to Río Cuarto, carrying six passengers and one pilot who took part to a motorcycle GP in Termas de Río Hondo. About 45 minutes into the flight, while cruising at an altitude of 6,500 feet, the left engine failed. The pilot contacted ATC and was cleared to divert to Deán Funes Airfield. On approach, he realized he could not make it and attempted an emergency landing on the National Road 60 at km 835. After touchdown, the aircraft veered off the street, lost its nose gear and came to rest in bushes. One passenger and the pilot were injured while five other occupants escaped unhurt. The aircraft was damaged beyond repair.
Probable cause:
The following findings were identified:
- Failure of the left engine in cruising flight due to the failure of the fuel injection system connected to the cylinder n°3,
- Inadequate maintenance of the aircraft and engine and non application of the bulletins related to the maintenance of the injection system,
- Impossibility for the pilot to increase engine power due to the high temperature of the cylinder,
- The aircraft's performances were degraded,
- Late decision of the pilot to attempt an emergency landing at dusk,
- Insufficient information regarding the procedure to feather the propeller.
Final Report: