Crash of a Cessna 208B Grand Caravan in Felipe Carrillo Puerto: 9 killed

Date & Time: Jun 14, 2010 at 1730 LT
Type of aircraft:
Registration:
XA-TWK
Flight Phase:
Survivors:
No
Schedule:
Felipe Carrillo Puerto-Chetumal
MSN:
208B-0992
YOM:
2002
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
Shortly after takeoff from Felipe Carrillo Puerto Airport, while in initial climb, the single engine airplane entered an uncontrolled descent and crashed nose first in a wooded area located past the runway end. The aircraft was destroyed and all 9 occupants were killed, among them 7 members of the campaign team of the candidate for Governor of Quintana Roo, Roberto Borge.

Crash of a Swearingen SA226TC Metro II in Lanseria

Date & Time: Jun 13, 2010 at 1100 LT
Type of aircraft:
Operator:
Registration:
ZS-ZOC
Survivors:
Yes
Schedule:
Lanseria – Polokwane
MSN:
TC-293
YOM:
1979
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6900
Captain / Total hours on type:
400.00
Copilot / Total flying hours:
1630
Copilot / Total hours on type:
35
Aircraft flight hours:
27532
Aircraft flight cycles:
27353
Circumstances:
Two flight crew members accompanied by thirteen passengers departed from FALA to FAPP. The flight was uneventful until during the approach to land on Runway 05 at FAPP. The flight crew selected landing gear down and observed a red light which indicate undercarriage unsafe. The flight crew reported the situation to FAPP Air Traffic Control (ATC). FAPP ATC gave instruction to do a missed approach at low level fly-past. The intention was to conduct a visual inspection of the undercarriage to determine its condition. The ATC observed that the left main gear had not extended. FAPP ATC gave an instruction to the flight crew, to hold over the beacon (BHV), where they could attempt to extend the gear by means of normal and emergency procedure. The flight crew was not successful and undercarriage remained retracted. The flight crew returned to FALA with the intention to carry out an emergency landing. FALA ATC give instructions to the flight crew to hold over the beacon (LIV), to again attempt the normal and emergency undercarriage extension procedures. But jet again; the flight crew was unsuccessful to lower the left main gear. ATC then instructed that the aircraft should execute the emergency landing on Runway 24R. During short finals overhead the threshold, prior to touchdown, the flight crew shut down both engines, feathered the propellers and switched off all the electronics. The aircraft landed and came to a gradual stop on its lower fuselage on the centreline of the runway.
Probable cause:
The pilot executed a belly “wheels up” emergency landing after the left main landing gear failed to extend.
Contributory Factors:
The new tyres installed on the main landing gear wheels were not in compliance with the instructions of the Fairchild Service Letter 226-SN-131.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain near Cartwright: 2 killed

Date & Time: May 26, 2010 at 0930 LT
Operator:
Registration:
C-FZSD
Flight Phase:
Survivors:
No
Site:
Schedule:
Goose Bay - Cartwright - Black Tickle - Goose Bay
MSN:
31-7405233
YOM:
1974
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9000
Circumstances:
Aircraft departed on a round trip flight from Goose Bay to Cartwright and Black Tickle before returning to Goose Bay, Newfoundland and Labrador. The pilot was to deliver freight to Cartwright as well as a passenger and some freight to Black Tickle. At approximately 0905, the pilot made a radio broadcast advising that the aircraft was 60 nautical miles west of Cartwright. No further radio broadcasts were received. The aircraft did not arrive at destination and, at 1010, was reported as missing. The search for the aircraft was hampered by poor weather. On 28 May 2010, at about 2200, the aircraft wreckage was located on a plateau in the Mealy Mountains. Both occupants of the aircraft were fatally injured. The aircraft was destroyed by impact forces and a post-crash fire. There was no emergency locator transmitter on board and, as such, no signal was received.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The pilot conducted a visual flight rules (VFR) flight into deteriorating weather in a mountainous region.
2. The pilot lost visual reference with the ground and the aircraft struck the rising terrain in level, controlled flight.
Findings as to Risk:
1. When an aircraft is not equipped with a functioning emergency locator transmitter (ELT), the ability to locate the aircraft in a timely manner is hindered.
2. Not applying current altimeter settings along a flight route, particularly from an area of high to low pressure, may result in reduced obstacle clearance.
3. Without a requirement for terrain awareness warning systems, there will be a continued risk of accidents of this type.
Final Report:

Crash of a Beechcraft 200 Super King Air in Angola: 3 killed

Date & Time: May 21, 2010 at 0020 LT
Operator:
Registration:
D2-FFT
Flight Phase:
Survivors:
No
Schedule:
Pointe Noire - Luanda
MSN:
BB-607
YOM:
1980
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was performing a charter flight from Pointe Noire to Luanda with one passenger on board, the Mauritanian businessman Rashid Mustapha who was candidate to the Presidential elections in Mauritania in 2007. The pax called his bodyguard just before takeoff, asking them to be ready upon arrival at Luanda-4 de Fevereiro Airport. The twin engine aircraft departed Pointe Noire Airport at 2321LT for a 75-90 minutes flight to Luanda. Just before it started the descent, while cruising over the area of Caxito, some 50 km northeast of Luanda, the aircraft disappeared from radar screens at 0020LT. SAR operations were abandoned after few days as no trace of the aircraft nor the three occupants was found. It is possible that the aircraft crashed by night in the ocean off the Angolan coast but this was not confirmed as the wreckage was never found. Three years later, in March 2013, unconfirmed reports and rumors in Africa said that the aircraft never crashed anywhere and that Rashid Mustapha was in fact hostage by a terrorist group somewhere in Africa, but this was not confirmed by Officials in Mauritania or Angola. Without any trace of the aircraft, all hypothesis remains open.

Crash of a Beechcraft 200 Super King Air in Arlit

Date & Time: Apr 27, 2010 at 1830 LT
Operator:
Registration:
F-GLIF
Survivors:
Yes
Schedule:
Niamey - Arlit
MSN:
BB-192
YOM:
1977
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Arlit Airport, the crew lost visual contact with the runway due to a sand storm. The aircraft was too low and hit the ground short of runway. Upon impact, the undercarriage were torn off and the aircraft slid over few dozen metres before coming to rest. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The crew continued the approach in a reduced visibility due to blowing sand and descended too low without visual contact with the ground.

Crash of a Learjet 25D in Bahías de Huatulco

Date & Time: Apr 1, 2010 at 1300 LT
Type of aircraft:
Operator:
Registration:
XA-UNC
Survivors:
Yes
Schedule:
Oaxaca – Bahías de Huatulco
MSN:
222
YOM:
1977
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Bahías de Huatulco Airport, the crew was unable to lower the landing gear. It was decided to perform a wheels up landing. The aircraft landed on its belly then slid for few dozen metres, veered off runway and came to rest, bursting into flames. All six occupants escaped uninjured but the aircraft was destroyed by fire. Among the passenger was Ulises Ruiz Ortiz, Governor of the State of Oaxaca.

Crash of a Dassault Falcon 20C in Vail

Date & Time: Jan 8, 2010 at 1225 LT
Type of aircraft:
Registration:
XA-PCC
Flight Phase:
Survivors:
Yes
Schedule:
Vail - Chihuahua
MSN:
159
YOM:
1968
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11000
Captain / Total hours on type:
5000.00
Circumstances:
During taxi the airplane was observed to run over a tire chock with the left main gear tire. During a turn out of the ramp, the left main gear was observed to run over the nose gear chock that had been removed from the nose gear by the pilot during pre-flight. During the departure roll, the left main gear tire failed and the pilot elected to abort the takeoff attempt. The airplane did not stop on the remaining runway surface and departed the runway overrun area, coming to rest in snow-covered terrain. An examination of the airplane's systems revealed no anomalies.
Probable cause:
The flight crew’s improper preflight inspection and failure to remove the main landing gear wheel chock, resulting in damage and subsequent failure of the main landing gear tire during the takeoff roll.
Final Report:

Crash of a Swearingen SA227AC Metro III in Cap Haïtien

Date & Time: Dec 20, 2009 at 1200 LT
Type of aircraft:
Operator:
Registration:
C6-JER
Survivors:
Yes
Schedule:
Nassau – Cap Haïtien
MSN:
AC-588B
YOM:
1984
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7400
Circumstances:
On Sunday December 20, 2009 at approximately 1700 UTC a fixed wing, multi engine, Fairchild SA-227AC Metro-liner III aircraft landed at Cap Haïtien Int’l Airport, Haiti, with its landing gear retracted. The pilot reported on two occasions whilst the aircraft was configured with flaps and gear extended, upon reduction in power preparing to land, the aircraft had a very high nose up attitude. The pilot further stated that after two go around, the decision was made to land the aircraft with its landing gear retracted. The aircraft landed on Runway 05. According to the pilot, the crew and all 19 passengers onboard suffered no injuries.
Final Report:

Crash of an Avro 748-398-2B in Tonj: 1 killed

Date & Time: Dec 20, 2009
Type of aircraft:
Operator:
Registration:
5Y-YKM
Survivors:
Yes
Schedule:
Juba - Tonj
MSN:
1779
YOM:
1981
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
15620
Circumstances:
After landing at Tonj Airfield, the aircraft that was unable to stop within the remaining distance. It overran and came to rest against houses. All 41 occupants escaped uninjured while a woman was killed on the ground. The aircraft departed Juba on a charter flight to Tonj, carrying security personnel from the Presidency who should prepare the next visit of the President of South Sudan in Tonj.

Crash of a Beechcraft A100 King Air in Chicoutimi: 2 killed

Date & Time: Dec 9, 2009 at 2250 LT
Type of aircraft:
Operator:
Registration:
C-GPBA
Survivors:
Yes
Schedule:
Val d'Or - Chicoutimi
MSN:
B-215
YOM:
1975
Flight number:
ET822
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3500
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
1000
Copilot / Total hours on type:
150
Circumstances:
The Beechcraft was on an instrument flight rules flight between Val-d’Or and Chicoutimi/Saint-Honoré, Quebec, with 2 pilots and 2 passengers on board. At 2240 Eastern Standard Time, the aircraft was cleared for an RNAV (GNSS) Runway 12 approach and switched to the aerodrome traffic frequency. At 2250, the International satellite system for search and rescue detected the aircraft’s emergency locator transmitter signal. The aircraft was located at 0224 in a wooded area approximately 3 nautical miles from the threshold of Runway 12, on the approach centreline. Rescuers arrived on the scene at 0415. The 2 pilots were fatally injured, and the 2 passengers were seriously injured. The aircraft was destroyed on impact; there was no post-crash fire.
Probable cause:
Findings as to Causes and Contributing Factors:
For undetermined reasons, the crew continued its descent prematurely below the published approach minima, leading to a controlled flight into terrain (CFIT).
Findings as to Risk:
1. The use of the step-down descent technique rather than the stabilized constant descent angle (SCDA) technique for non-precision instrument approaches increases the risk of an approach and landing accident (ALA).
2. The depiction of the RNAV (GNSS) Runway 12 approach published in the Canada Air Pilot (CAP) does not incorporate recognized visual elements for reducing ALAs, as recommended in Annex 4 to the Convention, thereby reducing awareness of the terrain.
3. The installation of a terrain awareness warning system (TAWS) is not yet a requirement under the Canadian Aviation Regulations (CARs) for air taxi operators. Until the changes to regulations are put into effect, an important defense against ALAs is not available.
4. Most air taxi operators are unaware of and have not implemented the FSF ALAR task force recommendations, which increases the risk of a CFIT accident.
5. Approach design based primarily on obstacle clearance instead of the 3° optimum angle increases the risk of ALAs.
6. The lack of information on the SCDA technique in Transport Canada reference manuals means that crews are unfamiliar with this technique, thereby increasing the risk of ALAs.
7. Use of the step-down descent technique prolongs the time spent at minimum altitude, thereby increasing the risk of ALAs.
8. Pilots are not sufficiently educated on instrument approach procedure design criteria. Consequently, they tend to use the CAP published altitudes as targets, and place the aircraft at low altitude prematurely, thereby increasing the risk of an ALA.
9. Where pilots do not have up-to-date information on runway conditions needed to check runway contamination and landing distance performance, there is an increased risk of landing accidents.
10. Non-compliance with instrument flight rules (IFR) reporting procedures at uncontrolled airports increases the risk of collision with other aircraft or vehicles.
11. If altimeter corrections for low temperature and remote altimeter settings are not accurately applied, obstacle clearance will be reduced, thereby increasing the CFIT risk.
12. When cockpit recordings are not available to an investigation, this may preclude the identification and communication of safety deficiencies to advance transportation safety.
13. Task-induced fatigue has a negative effect on visual and cognitive performance which can diminish the ability to concentrate, operational memory, perception and visual acuity.
14. Where an emergency locator transmitter (ELT) is not registered with the Canadian Beacon Registry, the time needed to contact the owner or operator is increased which could affect occupant rescue and survival.
15. If the tracking of a call to 911 emergency services from a cell phone is not accurate, search and rescue efforts may be misdirected or delayed which could affect occupant rescue and survival.
Other Findings:
1. Weather conditions at the alternate airport did not meet CARs requirements, thereby reducing the probability of a successful approach and landing at the alternate airport if a diversion became necessary.
2. Following the accident, none of the aircraft exits were usable.
Final Report: