Crash of a Cessna 208B Grand Caravan on Mt Awakapa Tepuy: 7 killed

Date & Time: May 4, 2004 at 1145 LT
Type of aircraft:
Operator:
Registration:
YV-O-CBL-7
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ciudad Bolívar – Uonquén
MSN:
208B-0926
YOM:
2001
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The single engine aircraft departed Ciudad Bolívar at 1016LT on a flight to Uonquén, State of Bolívar. En route, around 1100LT, the pilot reported flying at 11,500 feet in poor weather conditions. About 45 minutes later, while cruising at an altitude of 7,000 feet, the aircraft struck the slope of Mt Awakapa Tepuy located in the Chimanta Mountain Range. All seven occupants were killed, among them two church women.
Probable cause:
Controlled flight into terrain.

Crash of a Cessna 208B Grand Caravan off Punta Gorda

Date & Time: Mar 20, 2004 at 1159 LT
Type of aircraft:
Operator:
Registration:
V3-HGB
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Punta Gorda – Placencia
MSN:
208B-0871
YOM:
2000
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Five minutes after takeoff from Punta Gorda, while cruising at an altitude of 1,500 feet, the pilot informed ATC about engine problem. He elected to return to the airport but as he was unable to maintain the altitude, he attempted to ditch the aircraft 3 km offshore. The pilot was rescued while the aircraft sank and was lost.

Crash of a Cessna 208B Grand Caravan in Lake Manyara

Date & Time: Mar 17, 2004 at 0615 LT
Type of aircraft:
Operator:
Registration:
5H-MUA
Flight Phase:
Survivors:
Yes
Schedule:
Arusha – Lake Manyara – Klein’s Camp – Grumet – Seronera – Lake Manyara – Arusha
MSN:
208B-0487
YOM:
1995
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14000
Circumstances:
The aircraft was operating a scheduled flight starting from its base at Arusha. It was to call at Lake Manyara, Klein’s Camp, Grumet and Seronera before returning to Arusha via Lake Manyara. 5H-MUA took off from Arusha at 0530 hours. It was carrying one pilot and 3 passengers. The VFR flight to Lake Manyara was uneventful and the aircraft landed at Lake Manyara at 0555 hours. Five more passengers joined the flight here and 5H-MUA subsequently took off for Klein’s Camp at 0615 hours. During initial climb, the engine failed. The pilot feathered the propeller and attempted an emergency landing on a road. But he was forced to make an evasive manoeuvre because of a truck. The aircraft lost speed and height, collided with a stone wall beside the road and came tor rest. All nine occupants were rescued, among them five were seriously injured.
Probable cause:
Engine failure for undetermined reasons.
Final Report:

Crash of a Cessna 208B Grand Caravan off Pelée Island: 10 killed

Date & Time: Jan 17, 2004 at 1638 LT
Type of aircraft:
Operator:
Registration:
C-FAGA
Flight Phase:
Survivors:
No
Schedule:
Pelée Island – Windsor
MSN:
208B-0658
YOM:
1998
Flight number:
GGN125
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
3465
Captain / Total hours on type:
957.00
Aircraft flight hours:
7809
Circumstances:
On 17 January 2004, the occurrence pilot started his workday in Toronto, Ontario, reporting for duty at 0445 eastern standard time. In the morning, he completed flights in the Cessna 208B Caravan from Toronto to Windsor, Ontario, Windsor to Pelee Island, Ontario, and then Pelee Island to Windsor where the aircraft landed at 0916. At approximately 1500, the pilot received local weather and passenger information by telephone from the Pelee Island office personnel. The 1430 weather was reported as follows: ceiling 500 feet obscured, visibility two miles. There were eight male passengers for pick up at Pelee Island. One additional passenger was travelling with the pilot. There was no discussion concerning the amount of cargo to be carried or the passenger weights. At 1508, the pilot received a faxed weather package that he had requested from the Flight Information Centre (FIC) in London, Ontario. At 1523, the aircraft was refuelled in preparation for the scheduled 1600 departure to Pelee Island. The passengers were loaded earlier than usual to allow time for aircraft de-icing, as wet snow had accumulated on the fuselage and wings since the previous flight. At 1555, the aircraft was de-iced with Type 1 de-icing fluid, and it departed for Pelee Island at 1605 on an instrument flight rules (IFR) flight plan as Flight GGN125. At 1615, the pilot advised the Cleveland Control Centre, Ohio, United States, that he had Pelee Island in sight, was cancelling IFR, and was descending out of 5000 feet. The pilot also advised Cleveland that he would be departing IFR out of Pelee Island in about 20 minutes as GGN126 and asked if a transponder code could be issued. The Cleveland controller issued a transponder code and requested a call when GGN126 became airborne. The pilot advised that the flight would depart on Runway 27 then turn north. These were the last recorded transmissions from the aircraft. The aircraft landed at 1620. While on the ramp, two individuals voiced concern to the pilot that there was ice on the wing. Freezing precipitation was falling. The pilot was observed to visually check the leading edge of the wing; however, he did not voice any concern and proceeded with loading the passengers and cargo. At approximately 1638, GGN126 departed Pelee Island for Windsor. After using most of the runway length for take-off, the aircraft climbed out at a very shallow angle. No one on the ground observed the aircraft once it turned toward the north; however, witnesses who were not at the airport reported that they heard the sound of a crash, then no engine noise. A normal flight from Pelee Island to Windsor in the Cessna Caravan takes 15 to 20 minutes. Shortly after the aircraft departed, the ticket agent in Windsor received a call from Pelee Island reporting that a crash had been heard. At 1705, when the aircraft had not arrived, the ticket agent called Windsor tower. The pilot had not made contact with any air traffic services (ATS) facility immediately before or after departure, so there was nothing in the ATS system to indicate that the aircraft had taken off. It was, therefore, unaccounted for. There was no signal heard from the emergency locator transmitter (ELT). At 1710, the Windsor tower controller contacted the Rescue Coordination Centre in Trenton, Ontario, and a search was initiated. At 1908, the aircraft empennage and debris were spotted by a United States Coast Guard (USCG) helicopter on the frozen surface of the lake, about 1.6 nautical miles (nm) from the departure end of the runway. There were no survivors. The empennage sank beneath the surface some four hours later. The wreckage recovery was not fully completed until 13 days later.
Probable cause:
Findings as to Causes and Contributing Factors:
1. At take-off, the weight of the aircraft exceeded the maximum allowable gross take-off weight by at least 15 per cent, and the aircraft was contaminated with ice. Therefore, the aircraft was being flown significantly outside the limitations under which it was certified for safe flight.
2. The aircraft stalled, most likely when the flaps were retracted, at an altitude or under flight conditions that precluded recovery before it struck the ice surface of the lake.
3. On this flight, the pilotís lack of appreciation for the known hazards associated with the overweight condition of the aircraft, ice contamination, and the weather conditions was inconsistent with his previous practices. His decision to take off was likely adversely affected by some combination of stress and fatigue.
Findings as to Risk:
1. Despite the abbreviated nature of the September 2001 audit, the next audit of Georgian Express Ltd. was not scheduled until September 2004, at the end of the 36-month window.
2. The internal communications at Transport Canada did not ensure that the principal operations inspector responsible for the air operator was aware of the Pelee Island operation.
3. The standard passenger weights available in the Aeronautical Information Publication at the time of the accident did not reflect the increased average weight of passengers and carry-on baggage resulting from changes in societal-wide lifestyles and in travelling trends.
4. The use of standard passenger weights presents greater risks for aircraft under 12 500 pounds than for larger aircraft due to the smaller sample size (nine passengers or less) and the greater percentage of overall aircraft weight represented by the passengers. The use of standard passenger weights could result in an overweight condition that adversely affects the safety of flight.
5. The Cessna Caravan de-icing boot covers up to a maximum of 5% of the wing chord. Research on this wing has shown that ice accumulation beyond 5% of the chord can result in degradation of aircraft performance.
6. At the Pelee Island Airport, the air operator did not provide the equipment that would allow an adequate inspection of the aircraft for ice during the pre-flight inspection and did not provide adequate equipment for aircraft de-icing.
7. Repetitive charter operators are not considered to be scheduled air operators under current Transport Canada regulations, and, therefore, even though the charter air operator may provide a service with many of the same features as a scheduled service, Transport Canada does not provide the same degree of oversight as it does for a scheduled air operator.
8. A review of the Canadian Aviation Regulations regarding simulator training requirements indicates that there is no requirement to conduct recurrent simulator training if currency and/or pilot proficiency checks do not lapse.
9. Commercial Air Service Standard 723.91(2) does not clearly indicate whether there is a requirement for simulator training following expiration of a pilot proficiency check.
10. Incorrect information on the passenger door placards, an incomplete safety features card, and the fact that the operating mechanisms and operating instructions for the emergency exits were not visible in darkness could have compromised passenger egress in the event of a survivable accident.
11. The dogs being carried on the aircraft were not restrained, creating a hazard for the flight and its occupants.
Final Report:

Crash of a Cessna 208B Super Cargomaster in Cody: 1 killed

Date & Time: Oct 29, 2003 at 0854 LT
Type of aircraft:
Operator:
Registration:
N791FE
Flight Type:
Survivors:
No
Schedule:
Casper – Cody
MSN:
208B-0289
YOM:
1991
Flight number:
FDX8773
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
11094
Captain / Total hours on type:
5821.00
Aircraft flight hours:
6885
Aircraft flight cycles:
6599
Circumstances:
ARTCC asked the pilot of Airspur 8773 if he would be able to execute the VOR instrument approach. The pilot said he could, but he wanted to "hold for a while to see if [the weather] gets a little better" [according to the METAR, visibility was 1.75 statute miles and there was a 200-foot overcast ceiling]. He was cleared to hold north of the VOR at 12,000 feet msl. While holding, the pilot filed the following PIREP indicating light rime icing. Shortly thereafter, he was cleared for the approach. Three witnesses saw the airplane on the downwind leg, just past midfield, at an estimated altitude of 500 feet. Shortly thereafter, one of them heard the engine "spool up to high power...[like reversing] the pitch of the propeller to slow down," and he thought the airplane had landed. Five witnesses said the airplane emerged from the overcast and banked "sharply to the left, then back to the right, then back to the left, then took a hard bank to the right," rolled inverted and struck the highway just south of the airport perimeter. The airplane slid down the embankment and out into a lake, becoming partially submerged. Witnesses said it was "snowing hard" and the highway was covered with 1 to 2 inches of slush. Wreckage examination revealed the flaps were down 30 degrees, the wing deice boots were "ribbed," and the inertial separator was open. According to the toxicological report, chlorpheniramine, desmethylsertraline, sertraline, and pseudoephedrine were detected in blood. In addition, chlorpheniramine, sertraline, phenylpropanolamine, and pseudoephedrine were detected in the urine. The urine also contained acetaminophen. Sertraline (trade name Zoloft) is a prescription antidepressant medication. According to the Guide for Aviation Medical Examiners, "The use of a psychotropic medication is considered disqualifying. This includes all... antidepressant drugs..." Chlorpheniramine is an over-the-counter sedating antihistamine used primarily for the treatment of allergies. Pseudophedrine (trade name Sudafed) is a decongestant. Acetaminophen (trade name Tylenol) is an over-the-counter pain reliever and fever-reducer. According to Dr. Stanley R. Mohler's "Medication and Flying: A Pilot's Guide," the adverse side effects of chlorpheniramine include drowsiness, dizziness, and lessened coordination. The side effects of pseudophedrine are usually mild and infrequent, but may include sleepiness, dizziness, restlessness, headache, and perhaps some loss of coordination and alertness or confusion.
Probable cause:
The pilot's failure to maintain aircraft control. Contributing factors include the pilot's failure to divert to an alternate airport, an inadvertent stall, and the snow and icing conditions.
Final Report:

Crash of a Cessna 208B Grand Caravan near Summer Beaver: 8 killed

Date & Time: Sep 11, 2003 at 2130 LT
Type of aircraft:
Operator:
Registration:
C-FKAB
Survivors:
No
Schedule:
Pickle Lake - Summer Beaver
MSN:
208B-0305
YOM:
1992
Flight number:
WSG125
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
2351
Captain / Total hours on type:
946.00
Aircraft flight hours:
16770
Circumstances:
The aircraft departed Pickle Lake to Summer Beaver, Ontario, on a charter flight with seven passengers and one crew member. The flight proceeded on a direct routing to destination at 3500 feet above sea level under night visual flight conditions. On approaching Summer Beaver, the aircraft joined the circuit on a downwind leg for a landing on Runway 17. When the aircraft did not land, personnel at Summer Beaver contacted the Pickle Lake flight dispatch to inquire about the flight. The aircraft was declared missing following an unsuccessful radio search by the Pickle Lake flight dispatch staff. Search and rescue personnel found the wreckage in a wooded area three nautical miles northwest of Summer Beaver. The aircraft had been nearly consumed by a post-crash fire. All eight people on board had been fatally injured.
Probable cause:
Findings as to Causes and Contributing Factors:
The aircraft departed controlled flight and struck terrain for undetermined reasons.
Findings as to Risk:
The company's flight-following procedures for flights operating in remote areas were impractical and were not consistently applied; this could compromise timely search and rescue operations following an accident.
Other Findings:
The aircraft did not carry flight recorders. Lack of information about the cause of this accident affects TSB's ability to identify related safety deficiencies and to issue safety communications intended to prevent accidents that could occur under similar circumstances.
Final Report:

Crash of a Cessna 208B Grand Caravan in Old Fangak

Date & Time: Aug 19, 2003
Type of aircraft:
Operator:
Registration:
5Y-TWI
Flight Phase:
Survivors:
Yes
MSN:
208B-0606
YOM:
1997
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taking off from Old Fangak Airstrip, the single engine aircraft hit trees located past the runway end, nosed down and crashed in a marsh. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Cessna 208B Grand Caravan in Tocomita: 1 killed

Date & Time: Aug 8, 2003 at 0932 LT
Type of aircraft:
Operator:
Registration:
YV-1069C
Survivors:
Yes
Schedule:
Porlamar - Canaima
MSN:
208B-0713
YOM:
1998
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route from Porlamar to Canaima, the crew informed ATC about engine problems and was cleared to divert to Tocomita for an emergency landing. On final approach, the aircraft stalled and crashed into trees 100 meters short of runway. A passenger was killed while 15 other occupants were injured. The aircraft was destroyed.

Crash of a Cessna 208B Grand Caravan near Rooisand: 4 killed

Date & Time: Jun 26, 2003 at 1930 LT
Type of aircraft:
Operator:
Registration:
V5-CAS
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Rooisand - Windhoek
MSN:
208B-0549
YOM:
1996
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Chartered by International SOS, the single engine aircraft was dispatched to the Rooisand Desert Ranch Aerodrome with a medical team to pick up a patient who suffered a car accident. The aircraft landed at Rooisand Airstrip about 15 minutes before sunset. Due to the night and because the airfield was not equipped with any light systems, the pilot asked people to park their cars along the runway with their lights on. After take off, the aircraft continued westbound with a 12 knots tailwind and was supposed to circle the runway two or three times to gain sufficient height to avoid the hills surrounding the area. Then the aircraft turned right towards a hill that was 258 metres higher than the end of the runway. The aircraft had flown about 4,8 km far towards that hill when it banked steeply to the left and headed back to the southeast. The aircraft then descended to a height of 191 metres until it struck the slope of a hill. The wreckage was found 17 metres below the hill's top and all four occupants were killed.
Probable cause:
Controlled flight into terrain caused by the combination of the following factors:
- The decision of the pilot to take off from an airfield that was not suitable for night operations,
- The absence of a copilot considerably increased the workload of the captain, assuming that the copilot could have assisted him in the reconnaissance of the terrain, the preparation of the flight, the assistance to the patient and the medical team,
- Lack of visibility due to the night and lack of visual reference points on the ground, especially since the pilot had to wear corrective glasses,
- The pilot could not clearly distinguish the various parameters displayed on his instrument's panel because he forgot his glasses.