Crash of a Canadair CL-215-1A10 near Volos: 2 killed

Date & Time: Jul 15, 2000
Type of aircraft:
Operator:
Registration:
1048
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Volos - Volos
MSN:
1048
YOM:
1974
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew departed Volos-Nea Anchialos Airport on a fire fighting mission over Mt Pelion, about 10 km northeast of Volos. While flying at low height, the crew was preparing to drop water when the right wing struck the ground. The aircraft crashed and exploded, killing both pilots.

Crash of a BAe 3201 Jetstream 32EP near Chulum Juárez: 19 killed

Date & Time: Jul 8, 2000 at 1950 LT
Type of aircraft:
Operator:
Registration:
N912FJ
Flight Phase:
Survivors:
No
Site:
Schedule:
Tuxtla Gutiérrez – Villahermosa – Veracruz – Mérida
MSN:
912
YOM:
1990
Flight number:
QA7831
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
5300
Captain / Total hours on type:
1100.00
Copilot / Total flying hours:
667
Copilot / Total hours on type:
40
Aircraft flight hours:
12041
Circumstances:
The aircraft departed Tuxtla Gutiérrez Airport on a regular schedule flight to Mérida with intermediate stops in Villahermosa and Veracruz, carrying 17 passengers and two pilots. En route to Villahermosa-Carlos Rovirosa Pérez Airport, at an altitude of 16,000 feet and about 50 miles from the destination, the crew encountered poor weather conditions and deviated from the V3 Airway to the right for about 24 km. After he initiated the descent, the crew was instructed by ATC to report 25 DME. Shortly later, while descending in clouds, the twin engine aircraft struck the slope of a mountain located near Chulum Juárez, about 80 km southeast of Villahermosa Airport. The wreckage was found at an altitude of 1,890 metres. The aircraft disintegrated on impact and all 19 occupants were killed.
Probable cause:
Controlled flight into terrain. Combining instrument flight (IFR), with visual flight (VFR), the crew lost situational awareness, deviating 29.8 miles to the right of the Victor 3 airway due to bad weather, when the weather conditions imposed the application of the instrument flight rules (IFR), causing collision of the aircraft with the mountain at 6200 feet of elevation without loss of control (CFIT).
The following contributing factors were identified:
- Severe weather conditions en route,
- Persistence of the pilot in command, to continue the instrument flight (IFR) on visual flight (VFR),
- Inconsistency in cockpit resource management (CRM),
- Loss of situational awareness of the flight crew and the controllers, due to numerous deviations from the route, due to severe weather conditions and poor communication between the parties.
- inadequate preparation of the flight plan, since in view of the very probable need to circumnavigate severe meteorological conditions, the flight altitudes that would continue outside of the controlled airspace (outside the v-3 airway) were not verified.
Final Report:

Crash of a Cessna 402A in Kamina: 1 killed

Date & Time: Jun 29, 2000
Type of aircraft:
Operator:
Registration:
P2-SAV
Flight Type:
Survivors:
No
Site:
Schedule:
Kerema - Kamina
MSN:
402A-0069
YOM:
1969
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While descending to Kamina Airport, the twin engine aircraft struck a mountain and crashed. The pilot, sole on board, was killed.

Crash of a Cessna 414 Chancellor near Monarch: 3 killed

Date & Time: May 31, 2000 at 1728 LT
Type of aircraft:
Operator:
Registration:
N5113G
Flight Phase:
Survivors:
No
Site:
Schedule:
Great Falls - Billings
MSN:
414-0952
YOM:
1977
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
8000
Aircraft flight hours:
7406
Circumstances:
During climbout, the airplane encountered an area of freezing rain resulting in rapid airframe ice accretion and loss of climb capability. The pilot informed ATC that he was unable to maintain altitude and requested and received clearance back to Great Falls, the departure airport. ATC radar showed that the airplane then began a right turn over mountainous terrain extending up to 8,309 feet prior to loss of radar contact (lower and relatively flat terrain, down to less than 5,000 feet, was located to the left of the aircraft's track.) During the last minute of radar contact, the aircraft was in a right turn at a descent rate of about 400 feet per minute; the aircraft passed less than 1/2 mile from the 8,309-foot mountain summit just prior to loss of radar contact, at an altitude of 8,400 to 8,500 feet. The aircraft crashed on the southwest flank of the 8,309-foot mountain about 1/2 mile south of the last recorded radar position. Wreckage and impact signatures at the crash site were indicative of an inverted, steep-angle, relatively low-speed, downhill impact with the terrain. The investigation revealed no evidence of any aircraft mechanical problems.
Probable cause:
The failure of the pilot-in-command to ensure adequate airspeed for flight during a forced descent due to airframe icing, resulting in a stall. Factors included: freezing rain conditions, airframe icing, an improper decision by the pilot-in-command to turn toward mountainous terrain (where a turn toward lower and level terrain was a viable option), mountainous terrain, and insufficient altitude available for stall recovery.
Final Report:

Crash of a Britten-Norman BN-2A-9 Islander in Kurupung: 1 killed

Date & Time: May 3, 2000
Type of aircraft:
Operator:
Registration:
8R-GAC
Flight Type:
Survivors:
No
Site:
MSN:
694
YOM:
1973
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The twin engine aircraft was descending to Kurupung Airstrip in marginal weather conditions when it collided with trees and crashed in a wooded area located in hilly terrain. The pilot, sole on board, was killed. The aircraft was on its way to Kurupung to deliver fuel drums.

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Estes Park: 2 killed

Date & Time: Apr 30, 2000 at 1211 LT
Registration:
N7421S
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Page - Fort Collins
MSN:
61-0006
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4400
Circumstances:
While on a cross-country flight, according to radar data and weather information, the pilot descended below terrain clearance altitude and entered IMC conditions. The aircraft impacted a mountain peak approximately 100 feet below the summit. No flight plan had been filed and the pilot was not instrument rated.
Probable cause:
A descent below the surrounding terrain, by the pilot, in IMC conditions. Factors were high mountainous terrain, clouds, inaccurate weather evaluation by the pilot, and the pilot's flight into IMC conditions.
Final Report:

Crash of a Casa 212-DE Aviocar 100 near Cubillejo: 7 killed

Date & Time: Mar 22, 2000 at 1745 LT
Type of aircraft:
Operator:
Registration:
TM.12D-73
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Seville - Zaragoza
MSN:
314
YOM:
1983
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
While cruising in poor weather conditions, the twin engine aircraft struck the slope of a mountain located near Cubillejo. All seven occupants were killed.

Crash of a De Havilland DHC-6 Twin Otter 300 in Carreto: 10 killed

Date & Time: Mar 17, 2000 at 0930 LT
Operator:
Registration:
HP-1267APP
Flight Phase:
Survivors:
No
Site:
Schedule:
Panama City - Puerto Obaldía
MSN:
624
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
While descending at an altitude of 7,500 feet in relative good weather conditions, the crew informed ATC about their position when contact was lost. The wreckage was found five days later at the altitude of 762 metres on the slope of a mountain (850 metres high) located near Carreto, about 22 km northwest pf Puerto Obaldía Airport. All 10 occupants were killed. The crew was descending under VFR mode when the accident occurred for unknown reasons.

Crash of a Cessna 402B near Mojotoro: 4 killed

Date & Time: Feb 23, 2000 at 0925 LT
Type of aircraft:
Operator:
Registration:
LV-MEW
Survivors:
No
Site:
Schedule:
Orán – Salta
MSN:
402B-1310
YOM:
1977
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
890
Captain / Total hours on type:
83.00
Copilot / Total flying hours:
680
Copilot / Total hours on type:
70
Circumstances:
The twin engine aircraft departed Orán Airport at 0845LT on an executive flight to Salta, carrying two passengers and two pilots. At 0910LT, while flying under VFR mode, the crew reported his position over Moxat at an altitude of 8,000 feet. At 0923LT, he informed ATC about his position 15NM northeast of Salta Airport and was instructed to contact Salta Tower. Shortly later, the aircraft struck the slope of a mountain (Finca el Desmonde) located near Mojotoro. The aircraft disintegrated on impact and all four occupants were killed.
Probable cause:
Controlled flight into terrain after the crew decided to continue the descent under VFR mode in IMC conditions. It was reported that both pilots have the qualifications for IFR flight but were never trained to fly in such conditions.
Final Report:

Crash of a De Havilland DHC-2 Beaver near Lake Adonis: 3 killed

Date & Time: Jan 13, 2000 at 1030 LT
Type of aircraft:
Operator:
Registration:
C-FIVA
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Saint-Michel-des-Saints - La Pourvoirie des 100 Lacs - Lac Adonis
MSN:
515
YOM:
1953
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3147
Captain / Total hours on type:
3000.00
Aircraft flight hours:
26400
Circumstances:
The DHC-2 Mk. 1 skiplane, registration C-FIVA, serial number 515, with the pilot and five passengers on board, took off from the frozen surface of Lake Adonis, Quebec, on a pleasure flight under visual flight rules (VFR). The route had not been determined, but the flight was to last about 20 minutes. When the aircraft did not return, the search and rescue (SAR) service was advised. The aircraft was found crashed on a mountainside in a wooded area a little less than five km from its point of departure. The pilot and two passengers suffered fatal injuries. The other three passengers suffered serious injuries and hypothermia. The aircraft was destroyed by the force of the impact but did not catch fire. The five passenger, all from the same family, were originating from Marseille, France.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft probably stalled with insufficient altitude for the pilot to execute a recovery.
2. The prevailing conditions were conducive to optical illusions associated with low-altitude flight over rising terrain.
3. The aircraft was not equipped with a stall warning system, nor was it required by regulation.
4. The pilot's decision to fly at low altitude and probably use cutback power for the climb did not allow for safe obstacle clearance.
5. The pre-flight safety briefing did not inform passengers where to find the survival equipment on board the aircraft. Consequently, they could not use the sleeping bags to protect themselves from exposure and thereby delay hypothermia.
6. Rescue was late because the mostly white aircraft blended into the snowy ground, making it difficult to locate, and the ELT antenna was broken, reducing the range of the signal. Consequently, the survivors' exposure time was increased.
Other Findings:
1. The pilot was certified and qualified for the flight.
2. The autopsy and toxicological test results revealed no indication that physiological factors affected the pilot's performance.
3. Records indicate that the aircraft was certified, equipped, and maintained in accordance with existing regulations and approved procedures.
4. The aircraft's weight and centre of gravity were within the limits specified in the aircraft fight manual.
5. There is no indication that there was an emergency situation or that the aircraft experienced problems prior to impact.
6. The ready-to-use weight and balance calculation form is not consistent with the standard. Transport Canada reported this irregularity in 1992, but no change was made in the form, which is still part of the company operations manual approved by Transport Canada on 23 October 1999.
7. The weather conditions were suitable for visual flight.
Final Report: