Crash of a Cessna 208B Grand Caravan near Pickle Lake: 1 killed

Date & Time: Dec 11, 2015 at 0909 LT
Type of aircraft:
Operator:
Registration:
C-FKDL
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pickle Lake – Angling Lake
MSN:
208B-0240
YOM:
1990
Flight number:
WSG127
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2990
Captain / Total hours on type:
245.00
Aircraft flight hours:
36073
Aircraft flight cycles:
58324
Circumstances:
On 11 December 2015, the pilot of Wasaya Airways Limited Partnership (Wasaya) flight 127 (WSG127) reported for duty at the Wasaya hangar at Pickle Lake Airport (CYPL), Ontario, at about 0815. The air taxi flight was to be the first of 3 cargo trips in the Cessna 208B Caravan (registration C-FKDL, serial number 208B0240) planned from CYPL to Angling Lake / Wapekeka Airport (CKB6), Ontario. The first flight was planned to depart at 0900. The pilot went to the Wasaya apron and conducted a pre-flight inspection of C-FKDL while a ground crew was loading cargo. A Wasaya aircraft fuel-handling technician confirmed with the pilot that the planned fuel load was 600 pounds per wing of Jet A fuel. After completing the fueling, the technician used the cockpit fuel-quantity indicators to verify that the distribution was 600 pounds per wing. The pilot returned to the hangar and received a briefing from the station manager regarding the planned flights. The pilot was advised that the first officer assigned to the flight had been reassigned to other duties in order to increase the aircraft’s available payload and load a snowmobile on board. The pilot completed and signed a Wasaya flight dispatch clearance (FDC) form for WSG127, and filed a copy of it, along with the flight cargo manifests, in the designated location in the company operations room. The FDC for WSG127 showed that the flight was planned to be conducted under visual flight rules (VFR), under company flight-following, at an altitude of 5500 feet above sea level (ASL). Time en route was calculated to be 66 minutes, with fuel consumption of 413 pounds. The pilot returned to the aircraft on the apron. Loading and fueling were complete, and the pilot conducted a final walk-around inspection of C-FKDL. Before entering the cockpit, the pilot conducted an inspection of the upper wing surface. At 0854, the pilot started the engine of C-FKDL and conducted ground checks for several minutes. At 0858, the pilot advised on the mandatory frequency (MF), 122.2 megahertz (MHz), that WSG127 was taxiing for departure from Runway 09 at CYPL. WSG127 departed from Runway 09 at 0900, and, at 0901, the pilot reported on the MF that the flight was airborne. The flight climbed eastward for several miles and then turned left toward the track to CKB6. At about 3000 feet ASL, WSG127 briefly descended about 100 feet over 10 seconds, and then resumed climbing. At 0905, the pilot reported on the MF that WSG127 was clear of the MF zone. WSG127 intercepted the track to CKB6 and climbed northward until the flight reached a peak altitude of about 4600 feet ASL at 0908:41, and then began descending at 0908:46. At 0909:16, the flight made a sharp right turn of about 120° as it descended through about 4000 feet ASL. At 0909:39, the descent ended at about 2800 feet and the aircraft climbed to about 3000 feet ASL before again beginning to descend. At approximately 0910, WSG127 collided with trees and terrain at an elevation of 1460 feet ASL during daylight hours.
Probable cause:
Findings as to causes and contributing factors:
1. Although the aircraft was prohibited from flying in known or forecast icing conditions, Wasaya Airways Limited Partnership (Wasaya) flight 127 (WSG127) was dispatched into forecast icing conditions.
2. The high take-off weight of WSG127 increased the severity of degraded performance when the flight encountered icing conditions.
3. The pilot of WSG127 continued the flight in icing conditions for about 6 minutes, resulting in progressively degraded performance.
4. WSG127 experienced substantially degraded aircraft performance as a result of ice accumulation, resulting in aerodynamic stall, loss of control, and collision with terrain.
5. The Type C pilot self-dispatch procedures and practices in use at Wasaya at the time of the occurrence did not ensure that operational risk was managed to an acceptable level.
6. Wasaya had not implemented all of the mitigation strategies from its January 2015 risk assessment of Cessna 208B operations in known or forecast icing conditions, and the company remained exposed to some unmitigated hazards that had been identified in the risk assessment.
7. There was a company norm of dispatching Cessna 208B flights into forecast icing conditions, although 4 of Wasaya’s 5 Cessna 208B aircraft were prohibited from operating in these conditions.

Findings as to risk:
1. Without effective risk-management processes, aircraft may continue to be dispatched into forecast or known icing conditions that exceed the operating capabilities of the aircraft, increasing the risk of degraded aircraft performance or loss of control.
2. If pilots operating under self-dispatch do not have adequate tools to complete an operational risk assessment before releasing a flight, there is an increased likelihood that hazards will not be identified or adequately mitigated.
3. If aircraft that are not certified for flight in known or forecast icing conditions are dispatched into, and encounter, such conditions, there is an increased risk of degraded performance or loss of control.
4. If aircraft that are certified for flight in known or forecast icing conditions are dispatched into, and encounter, such conditions, at weights exceeding limitations, there is an increased risk of loss of control.
5. If flights are continued in known icing conditions in aircraft that are not certified to do so, there is an increased risk of degraded aircraft performance and loss of control.
6. If operators exceed aircraft manufacturers’ recommended ICEX II servicing intervals, there is an increased risk of degraded aircraft performance or loss of control resulting from greater accretion of ice on the leading-edge de-icing and propeller blade anti-icing boots.
7. If pilots do not receive the minimum required training, there is an increased risk that they will lack the necessary technical knowledge to operate aircraft safely.
8. If pilots are not provided with the information they need to calculate the aircraft’s centre of gravity accurately, they risk departing with their aircraft’s centre of gravity outside the limits, which can lead to loss of control.
9. If emergency locator transmitter antennas and cable connections are not robust enough to survive impact forces, potentially life-saving search-and-rescue operations may be impaired by the absence of a usable signal.

Other findings:
1. Wasaya’s use of a satellite aircraft flight-following system provided early warning of WSG127’s abnormal status and an accurate last known position for search-and-rescue operations.
2. The investigation could not determine whether the autopilot had been used by the pilot of WSG127 at any time during the flight.
Final Report:

Crash of a Cessna 208B Grand Caravan near Yumbo: 3 killed

Date & Time: Oct 14, 2015 at 1146 LT
Type of aircraft:
Operator:
Registration:
PR-MIC
Flight Phase:
Survivors:
No
Site:
Schedule:
Cali - Cali
MSN:
208B-0841
YOM:
2000
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9388
Captain / Total hours on type:
4155.00
Copilot / Total flying hours:
6343
Copilot / Total hours on type:
1029
Aircraft flight hours:
10519
Circumstances:
The single engine airplane departed Cali-Alfonso Bonilla Aragón Airport on an geophysical exploration mission of the south part of Chocó, carrying three crew members, two pilots and one operator in charge of the LIDAR equipment. At 1144LT, the crew reported his altitude at 5,600 feet. Two minutes later, while cruising in poor visibility, the aircraft struck trees and crashed in wooded and hilly terrain near Yambo. The wreckage was found few hours later and all three occupants were killed.
Probable cause:
The following factors were identified:
- Controlled flight into terrain,
- Execution of a VFR flight in reduced visibility weather conditions,
- Poor decision making by the crew in continuing VFR operation as they were in an environment of significantly reduced visibility,
- Inadequate operational risk assessment due to the lack of familiarity of the foreign crew with the topography and meteorological evolution of the sector.
Final Report:

Crash of a Cessna 208B Grand Caravan near Bamyan: 2 killed

Date & Time: Oct 12, 2015 at 1400 LT
Type of aircraft:
Operator:
Registration:
YA22382
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
208B-2382
YOM:
2012
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Few minutes after takeoff from Bamyan Airport, the single engine crashed on the top of a rocky mountain. Both pilots were killed while five passengers were injured. The aircraft was destroyed. The aircraft was repatriating the body of a deceased soldier when the accident occurred.

Crash of a Cessna 208B Super Cargomaster off Saba Island

Date & Time: Aug 12, 2015 at 1205 LT
Type of aircraft:
Operator:
Registration:
N924FE
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
San Juan – Basseterre
MSN:
208B-0024
YOM:
1987
Flight number:
FDX8124
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot departed San Juan-Luis Muñoz Marín Airport at 1049LT on a cargo flight to Basseterre-Robert L. Bradshaw International Airport, Saint Kitts & Nevis. The flight was performed by Mountain Air Cargo on behalf of FedEx. The pilot continued the flight at FL110 until 1139LT, reduced his altitude down to FL100 and maintained this level until 1153LT. At this moment, the aircraft was descending between 600 and 800 feet per minute and the pilot decided to divert to the Juancho E. Yrausquin Airport located on Saba Island, Dutch Antilles. While approaching to island from the south, the pilot realized he would not make it, so he attempted to ditch the aircraft some 900 metres off shore. The pilot evacuated the cabin and was quickly rescued while the aircraft sank by a depth of about 1,500 feet. According to the pilot, he decided to divert to the nearest airport due to a loss of engine power.

Crash of a Cessna 208B Grand Caravan in Dubai

Date & Time: Jul 7, 2015 at 0800 LT
Type of aircraft:
Operator:
Registration:
DU-SD1
Flight Phase:
Survivors:
Yes
Schedule:
Dubai - Dubai
MSN:
208B-1141
YOM:
2005
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Dubai-Skydive Campus Airfield, while climbing to a height of 2,500 feet, the pilot encountered engine problems. He elected to return to the airport but eventually attempted an emergency landing in a desert area close to the airport. The aircraft crash landed and came to rest, bursting into flames. All 15 occupants escaped uninjured and the aircraft was destroyed by a post crash fire.

Crash of a Cessna 208B Caravan I in Mandeng

Date & Time: May 19, 2015
Type of aircraft:
Operator:
Registration:
5Y-NKV
Survivors:
Yes
Schedule:
Juba - Mandeng
MSN:
208B-0387
YOM:
1994
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine airplane suffered an accident upon landing at Mandeng Airfield. The undercarriage were torn off and the aircraft was severely damaged. There were no casualties.

Crash of a Cessna 208B Grand Caravan in Verdigris

Date & Time: Mar 24, 2015 at 1507 LT
Type of aircraft:
Operator:
Registration:
N106BZ
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Tulsa - Tulsa
MSN:
208B-0106
YOM:
1988
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6500
Captain / Total hours on type:
970.00
Aircraft flight hours:
11443
Circumstances:
The pilot reported that, during the postmaintenance test flight, the turboprop engine lost power. The airplane was unable to maintain altitude, and the pilot conducted a forced landing, during which the airplane was substantially damaged. The engine had about 9 total flight hours at the time of the accident. A teardown of the fuel pump revealed that the high-pressure drive gear teeth exhibited wear and that material was missing from them, whereas the driven gear exhibited little to no visible wear. A metallurgical examination of the gears revealed that the damaged drive gear was made of a material similar to 300-series stainless steel instead of the harder specified M50 steel, whereas the driven gear was made of a material similar to the specified M50 steel. Subsequent to these findings, the airplane manufacturer determined that the gear manufacturer allowed three set-up gears made from 300-series stainless steel to become part of the production inventory during the manufacturing process. One of those gears was installed in the fuel pump on the accident airplane, and the location of the two other gears could not be determined. Based on the evidence, it is likely that the nonconforming gear installed in the fuel pump failed because it was manufactured from a softer material than specified, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power. The manufacturer subsequently inspected its stock of gears and issued notices to customers that had engines with fuel pumps installed with the same part number gear set as the one installed on the accident airplane. The manufacturer also issued a service information letter and service bulletins regarding the fuel pump gear set for engines used in civilian and military applications. As of the date of this report, the two remaining gears have not been located.
Probable cause:
The fuel pump gear manufacturer’s allowance of set-up gears made from a nonconforming material to be put in the production inventory system, the installation of a nonconforming gear in the accident airplane’s production fuel pump, and the gear’s failure, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power.
Final Report: