Crash of a De Havilland DHC-8-202 near Acandí: 4 killed

Date & Time: Oct 5, 2013 at 0100 LT
Registration:
N356PH
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Panama City - Panama City
MSN:
502
YOM:
1997
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft departed Panama City-Marcos A. Gelabert Airport in the evening on an anti-narcotic survey flight over Colombia, carrying four passengers and two pilots, five US citizens and one Panamanian. En route, while cruising along the border between Panama and Colombia, the aircraft collided with trees and crashed on the slope of a wooded mountain, bursting into flames. All four passengers were killed and both pilots were seriously injured.

Crash of a Cessna 340A in Paulden: 4 killed

Date & Time: Oct 4, 2013 at 1300 LT
Type of aircraft:
Registration:
N312GC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bullhead City – Prescott
MSN:
340A-0023
YOM:
1975
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4006
Circumstances:
Witnesses located at a gun club reported observing the airplane make a high-speed, low pass from north to south over the club's buildings and then maneuver around for another low pass from east to west. During the second low pass, the airplane collided with a radio tower that was about 50 ft tall, and the right wing sheared off about 10 ft of the tower's top. The tower's base was triangular shaped, and each of its sides was about 2 ft long. One witness reported that the airplane remained in a straight-and-level attitude until impact with the tower. The airplane then rolled right to an almost inverted position and subsequently impacted trees and terrain about 700 ft southwest of the initial impact point. One witness reported that, about 3 to 4 years before the accident, the pilot, who was a client of the gun club, had "buzzed" over the club and had been told to never do so again. A postaccident examination of the engines and the airframe revealed no evidence of a mechanical malfunction or failure that would have precluded normal operation.
Probable cause:
The pilot's failure to maintain sufficient altitude to clear a radio tower while maneuvering at low altitude and his decision to make a high-speed, low pass over the gun club.
Final Report:

Crash of a Cessna 208B Grand Caravan in the Hudson Bay: 1 killed

Date & Time: Sep 25, 2013 at 1400 LT
Type of aircraft:
Operator:
Registration:
C-FEXV
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sault Sainte Marie - Sault Sainte Marie
MSN:
208B-0482
YOM:
1995
Flight number:
MAL8988
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On behalf of Morningstar Air Express, the pilot departed Sault Sainte Marie Airport, south Ontario, in the morning, for a local training flight. For unknown reasons, the pilot did not maintain any radio contact with his base or ATC and continued to the north for about 1,200 km when the aircraft crashed in unknown circumstances in the Hudson Bay, some 500 km east of Churchill, Manitoba. The aircraft was destroyed and the pilot was killed.
Probable cause:
The exact cause of the accident remains unknown.

Crash of a PZL-Mielec AN-2R near Nyagan

Date & Time: Sep 18, 2013 at 1337 LT
Type of aircraft:
Operator:
Registration:
RA-33017
Flight Phase:
Survivors:
Yes
Schedule:
Surgut – Saranpaul – Arbyn – Surgut
MSN:
1G218-04
YOM:
1986
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
5277
Aircraft flight cycles:
24822
Circumstances:
The aircraft departed Surgut on September 12 on a special flight to Saranpaul and Arbyn, carrying two pilots and five employees of the Sosvapromgeologya Company. On September 18, the crew was supposed to fly back to Surgut but due to poor weather conditions, decided to fly to Nefteyugansk. About an hour and 10 minutes into the flight, while cruising at an altitude of 700 metres, the engine temperature increased to 305° C. and the oil temperature to 90° C. In the same time, the engine lost power. The crew decided to reduce his altitude and to attempt an emergency landing when the aircraft crash landed in a field located 48 km west of Nyagan. There was no fire. All seven occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Most probably the accident with An-2 RA-33017 aircraft was caused by usage of uncoordinated automative fuel not specified by valid aircraft maintenance engineering documentation with low octane grade, mechanical admixture (rusting) that resulted in cylinder-heads temperature increase beyond operating limits, engine power loss, unintentional flight altitude decrease and the need of an emergency landing on saturated terrain.
The contributing factors could be:
- Unsatisfactory management of storage, refiling procedures and fuel quality inspection at Arbyn Airfield,
- Incorrect PIC's decision to perform a flight after detection of deviation from standards in fuel quick drain (color, consistency, mechanical mixtures).

Crash of a De Havilland DHC-3 Otter near Ivanhoe Lake: 1 killed

Date & Time: Aug 22, 2013 at 1908 LT
Type of aircraft:
Operator:
Registration:
C-FSGD
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Scott Lake Lodge - Ivanhoe Lake
MSN:
316
YOM:
1959
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1600
Captain / Total hours on type:
248.00
Circumstances:
The float-equipped Transwest Air Limited Partnership DHC-3 turbine Otter (registration C-FSGD, serial number 316) departed Scott Lake, Northwest Territories, at approximately 1850 Central Standard Time on a 33-nautical mile, day, visual flight rules flight to Ivanhoe Lake, Northwest Territories. The aircraft did not arrive at its destination, and was reported overdue at approximately 2100. The Joint Rescue Coordination Centre Trenton was notified by the company. There was no emergency locator transmitter signal. A search and rescue C-130 Hercules aircraft was dispatched; the aircraft wreckage was located on 23 August 2013, in an unnamed lake, 10 nautical miles north of the last reported position. The pilot, who was the sole occupant of the aircraft, sustained fatal injuries.
Probable cause:
Findings as to causes and contributing factors:
1. During approach to landing on the previous flight, the right-wing leading-edge and wing tip were damaged by impact with several trees.
2. The damage to the aircraft was not evaluated or inspected by qualified personnel prior to take-off.
3. Cumulative unmanaged stressors disrupted the pilot’s processing of safety-critical information, and likely contributed to an unsafe decision to depart with a damaged, uninspected aircraft.
4. The aircraft was operated in a damaged condition and departed controlled flight likely due to interference between parts of the failing wing tip, acting under air loads, and the right aileron.
Findings as to risk:
Not applicable.
Other findings:
1. The emergency locator transmitter did not activate, due to crash damage and submersion in water.
2. The aircraft was not fitted with FM radio equipment that is usually carried by aircraft servicing the lodge. Lodge personnel did not have a means to contact the pilot once the aircraft moved away from the dock.
Final Report:

Crash of a Britten Norman BN-2B-27 Islander in Purisima del Maguey

Date & Time: Aug 22, 2013 at 1530 LT
Type of aircraft:
Operator:
Registration:
XC-FEE
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Chihuahua – Zacatecas
MSN:
2022
YOM:
1980
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
4000
Circumstances:
The twin engine aircraft departed Chihuahua-General Fierro Villalobos Airport at 1352LT on a flight to Zacatecas, carrying four passengers and one pilot. It continued to the south at an altitude of 11,500 feet and a speed of 120 knots. The flight was uneventful until the pilot started the descent to Zacatecas-General Leobardo C. Ruiz. when the left engine lost power then failed shortly later. The pilot reduced his altitude and attempted an emergency landing when the aircraft crash landed in an open field located near Purisima del Maguey, some 25 km northwest of Zacatecas Airport. All five occupants evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
Failure of the left engine due to fuel exhaustion.
The following contributing factors were identified:
- Failure to apply the standard procedures relating to the quantity of fuel required as set out in the applicable regulations which were not provided to the crew by the operator.
- Poor flight preparation.
- Non-adherence to VFR rules.
- Lack of familiarity in the equipment on the part of the pilot when not receiving adequate training from the operator.
Final Report:

Crash of a Beechcraft 200C Super King Air in Lake Manyara

Date & Time: Aug 22, 2013
Operator:
Registration:
5H-TZW
Flight Phase:
Survivors:
Yes
Schedule:
Bukoba - Zanzibar - Dar es-Salaam
MSN:
BL-17
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route to Zanzibar, while cruising at an altitude of 21,000 feet, the right engine failed. The pilot decided to divert to Arusha Airport when few minutes later, while passing 16,000 feet on descent, the left engine failed as well. The pilot attempted to ditch the aircraft into Lake Manyara. The aircraft belly landed and came to rest in shallow water, bent in two. All seven occupants were rescued by fishermen and the aircraft was damaged beyond repair.

Crash of a PZL-Mielec AN-2TP near Vilyuisk

Date & Time: Aug 16, 2013 at 1345 LT
Type of aircraft:
Operator:
Registration:
RA-01419
Flight Phase:
Survivors:
Yes
Schedule:
Vilyuisk - Kyubeinde-Ugulet
MSN:
1G230-59
YOM:
1988
Flight number:
PI9977
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3973
Captain / Total hours on type:
480.00
Copilot / Total flying hours:
374
Copilot / Total hours on type:
52
Aircraft flight hours:
7587
Aircraft flight cycles:
10148
Circumstances:
Few minutes after takeoff from Vilyuisk Airport, on a schedule service (flight n° PI9977) to Kyubeinde-Ugulet, while cruising at an altitude of about 400 metres, the engine overheated and lost power while the oil pressure dropped. The crew decided to return to Vilyuisk when the engine failed shortly later. The captain attempted an emergency landing in a swampy area located 26 km northwest of Vilyuisk (at N63°54.584" E121°18.048"). The main wheels got stuck in soft ground, the engine was ripped off, and the aircraft came to rest, bursting into flames. Both pilots and all 9 passengers escaped uninjured and the aircraft was totally destroyed by fire.
Probable cause:
The accident with An-2Т RA-01419 aircraft was caused by emergency landing at the landing place in marsh area selected from air that resulted in main landing gear dipping in soft ground, dynamic pitch-down moment followed by engine ground impact and fuselage separation along engine mounting fitting, airframe structure and gear damage. Gasoline pipeline destruction during engine separation from aircraft frame and gasoline ingestion on the hot parts of power unit caused fire which almost completely destroyed the aircraft. Wrong PIC's actions who didn't turn off ignition and shut off fuel before aircraft landing could contribute to the fire. The emergency landing at the landing place selected from air was caused by oil temperature increase and pressure drop below specified by the aircraft FOM values in flight. It wasn't possible to determine the cause of temperature increase and oil pressure drop due to engine component substantial damage during fire.
Final Report:

Crash of a De Havilland DH.60G Moth in Canons Ashby

Date & Time: Aug 12, 2013 at 1130 LT
Type of aircraft:
Operator:
Registration:
G-AAZG
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Turweston - Turweston
MSN:
1253
YOM:
1930
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
512
Captain / Total hours on type:
15.00
Circumstances:
The pilot was carrying out a local flight with a friend. The weather was good (CAVOK), with a westerly wind of about 12 to 15 kt. The passenger occupied the front cockpit and the pilot the rear. The engine started normally and the aircraft departed, climbing to an altitude of 1,200 ft. The pilot carried out two medium banked turns and a gentle wingover manoeuvre before entering another steep turn to the left. When established in the turn, the engine stopped and the aircraft entered a spin to the left. The pilot recovered from the spin but, due to the limited height available, could only pull out of the dive and carry out a forced landing in an isolated grass area, amongst trees and other obstacles. In doing so, the aircraft struck a ridge and furrow, which destroyed the landing gear and much of the forward fuselage. A member of the public witnessed the accident and called the emergency services, who recovered both occupants from the wreckage. The pilot and his passenger had suffered serious injuries and were transferred to hospital. There was no fire.The aircraft had recently been re-weighed. During that process, the fuel tank had been drained and the same fuel was then used to refill the tank. After that, the aircraft had flown some five hours, during which it had been refuelled twice at a licensed aerodrome. The second refuel had taken place prior to positioning the aircraft back to the private site from which the accident flight departed. It was reported that the engine had been consistently reliable. No reason for the engine failure was identified. The pilot considered that he had avoided a serious head injury because he was wearing a protective helmet. Also, he commented that he had since had discussions with others in the historic aircraft community regarding energy absorbing foam in seat pans and its potential for reducing the level of back injuries in the event of an accident.
Probable cause:
Engine failure for undetermined reason.
Final Report:

Crash of a Shijiazhuang Yunsunji Y-5B in Danfeng: 1 killed

Date & Time: Aug 6, 2013
Type of aircraft:
Registration:
B-8473
Flight Phase:
Survivors:
Yes
Schedule:
Danfeng - Danfeng
MSN:
0101
YOM:
1989
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing a crop spraying mission in the region of Danfeng. While cruising at low altitude, the aircraft impacted tree tops, stalled and crashed in a wooded area. While the captain was seriously injured, the copilot was killed.