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

Date & Time: Aug 29, 2003 at 1427 LT
Type of aircraft:
Registration:
C-GHAF
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Nanaimo - Penticton - Calgary
MSN:
1408
YOM:
1959
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
915
Captain / Total hours on type:
615.00
Aircraft flight hours:
9029
Circumstances:
The aircraft left Nanaimo, British Columbia, and landed at Penticton Airport at 1232 Pacific daylight time (PDT). The aircraft was fueled with 184 litres of fuel, filling all three belly tanks. At this time, the rear portion of the aircraft cabin was observed to be loaded with luggage and cargo. The pilot/aircraft owner was planning his flight to Calgary (Springbank), Alberta, and spent at least an hour flight planning and talking with the Kamloops Flight Information Centre by telephone. He had some difficulty determining a route to fly to Springbank, because of airspace restrictions due to forest fires, but decided on a routing of Penticton, Kelowna, Vernon, Revelstoke, and Springbank. The aircraft took off from Penticton Airport at 1420 PDT, with the pilot and two passengers on board and crashed approximately seven minutes later in a ravine of Penticton Creek, 11 nautical miles northeast of Penticton Airport. A post-impact fire broke out and consumed most of the fuselage area. The fire caused a small forest fire, seen by a firefighting aircraft crew. There were no radio calls from the occurrence aircraft, and the three occupants were fatally injured.
Probable cause:
Findings as to Causes and Contributing Factors:
1. As the aircraft approached high terrain in a climb, the pilot, for undetermined reasons, did not turn away from the terrain; the aircraft struck tree tops and crashed.
2. The aircraft’s climb performance was adversely affected by density altitude and the relatively high aircraft weight, so that the aircraft was unable to clear the high terrain ahead.
Findings as to Risk:
1. The licensed passenger had not informed the TC medical examiner who conducted her last medical that she had been diagnosed with coronary artery disease, posing the risk that she could pilot an aircraft while not medically fit to do so.
2. The aircraft was being operated at a higher weight than was justified by the STC, under which it was converted to an amphibian. Some of the structural modifications called for by the STC for the higher weight had not been carried out.
Other Findings:
1. It could not be determined who was piloting the aircraft on the occurrence flight.
Final Report:

Crash of a Canadair CL-415-6B11 in Esine

Date & Time: Aug 16, 2003 at 1548 LT
Type of aircraft:
Operator:
Registration:
I-DPCN
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Verona - Verona
MSN:
2008
YOM:
1995
Flight number:
Tanker 9
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15700
Captain / Total hours on type:
3500.00
Copilot / Total flying hours:
2200
Copilot / Total hours on type:
400
Aircraft flight hours:
1186
Circumstances:
The aircraft was dispatched over the region of Esine to fight a forest fire under call sign Tanker 9. The area under fire was located on the southern slope of the Val Camonica, about 8 NM northeast from Lake Iseo. While approaching the zone to be treated, the aircraft struck trees and crashed on the mountain slope. Both pilots were injured, one seriously, and the aircraft was destroyed.
Probable cause:
The cause of the accident is attributable to the human factor and can be identified in the impact of the aircraft against certain trees following the setting of an inadequate escape manoeuvre.
The following causal factors may have contributed to the dynamics of the accident:
- The crew's failure to strictly comply with the Operator's Manual of Operations, which provided that the route of attack and escape should not be made uphill, unless there were very limited differences in level that could be overcome without power fluctuations,
- The failure to carry out, as a precautionary measure, since the trajectory of the attack route has changed (from descending to ascending), a new reconnaissance with subsequent briefing by the crew, in order to properly assess the different perspective of all the elements of interest (orography, escape route, etc..), even if the Operating Manual provided for a new reconnaissance by the crew with a subsequent briefing only in the case of a different target, even within the same fire, not even if the target had remained unchanged, but had changed the trajectory of the attack,
- The attack to the fire in unstabilized conditions, therefore not in line with what is previewed from the operating manual, even if the Operating Manual provided for a new reconnaissance by the crew with a subsequent briefing only in the case of a different target, even within the same fire, not even if the target had remained unchanged, but had changed the trajectory of the attack,
- The attack to the fire in not stabilized conditions, therefore not in line with what is previewed from the operating manual;
- The existence of communication problems within the cockpit, deriving from the fact that there was no information flow between the co-pilot (depositary of the information necessary for the assumption of the most appropriate operational decisions) and the commander, responsible for the final decisions; in this regard, it should be noted that radio communications with the DOCFS were made by the co-pilot in Italian, as the latter was not known by the commander, of Canadian nationality,
- The significant difference in experience and age between the two crew members, with possible negative effects in terms of crew coordination,
- The presence of critical points in the operating manuals, partly eliminated after the accident,
- The presence of locally significant turbulence.
Final Report:

Crash of a Swearingen SA226TC Metro II on Point Lenana: 14 killed

Date & Time: Jul 19, 2003 at 1800 LT
Type of aircraft:
Registration:
ZS-OYI
Flight Phase:
Survivors:
No
Site:
Schedule:
Nairobi – Samburu
MSN:
TC-349
YOM:
1980
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The twin engine aircraft departed Nairobi-Wilson Airport at 1558LT on a charter flight to Samburu, carrying 12 passengers (all US citizens) and two pilots. En route, the crew decided to make a tour over the Mt Kenya before continuing to Samburu. While cruising at an altitude of 16,500 feet in clouds, the aircraft struck the eastern slope of Mt Point Lenana (third highest peak of Mt Kenya). The wreckage was found 450 feet below the summit and all 14 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew failed to maintain horizontal and vertical situational awareness of the aircraft’s proximity to the surrounding terrain.
The following contributing factors were identified:
- Unfamiliarity with the airspace and the route in particular and the existence of high ground on the planned flight route,
- Inadequate flight planning by the pilots and distraction of their attention when they were instructed to contact Nanyuki,
- Poor pilot briefing by the Wilson ATC briefing office,
- Poor communication between the air traffic control units,
- Failure of the radar controller to advise the pilot of termination of radar service,
- Lack of a radar system minimum safe altitude warning to the radar controller,
- Poor civil military coordination during transit through the military airspace.

Crash of a Lockheed L-188A Electra in Cranbrook: 2 killed

Date & Time: Jul 16, 2003 at 1221 LT
Type of aircraft:
Operator:
Registration:
C-GFQA
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Cranbrook - Cranbrook
MSN:
1040
YOM:
1959
Flight number:
Tanker 86
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
38775
Circumstances:
The aircraft took off from Runway 16 at the Cranbrook Airport, British Columbia. Two pilots were on board to conduct a fire-management mission on a small ground fire (designated N10156) two nautical miles southwest of the township of Cranbrook. Seven minutes earlier, the partner “bird dog” aircraft, a Turbo Commander, also departed Cranbrook to assess the appropriate aircraft flight path profiles and to establish the most suitable fire-retardant delivery program for the ground fire. Following the flight path demonstrations by the bird dog aircraft, Tanker 86 proceeded to carry out the retardant drop on the fire. After delivering the specified retardant load, Tanker 86 was seen to turn right initially then entered a turn to the left. At 1221 MST, the Electra struck the terrain on the side of a steep ridge at about 3900 feet above sea level. The aircraft exploded on impact and the two pilots were fatally injured. An intense post-crash fire consumed much of the wreckage and started a forest fire at the crash site and the surrounding area. The on-board emergency locator transmitter was damaged by the impact forces and did not activate.
Probable cause:
Findings as to Causes and Contributing Factors:
1. For undetermined reasons, the Electra did not climb sufficiently to avoid striking the rising terrain.
2. Given the flight path and the rate of climb chosen, a collision with the terrain was unavoidable.
3. The characteristics of the terrain were deceptive, making it difficult for the pilots to perceive their proximity and rate of closure to the rising ground in sufficient time to avoid it.
Other Findings:
1. Performance calculations show that the Electra—in the absence of limiting mechanical malfunction—could have climbed at a rate that would have allowed the aircraft to avoid the terrain.
2. Although a functional cockpit voice recorder was installed in the aircraft, it was not required by regulation and it was not used; as a result, vital clues that could have shed light on the circumstances of this accident were not available.
3. The emergency locator transmitter could not transmit a signal as a result of severe impact forces that exceeded the design criteria.
Final Report:

Crash of a Let L-410UVP-E in San Cristóbal: 4 killed

Date & Time: Jul 13, 2003 at 1415 LT
Type of aircraft:
Registration:
YV-1060CP
Survivors:
Yes
Site:
Schedule:
La Carlota - San Cristóbal
MSN:
90 25 05
YOM:
1990
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
While descending to San Cristóbal Airport, the crew encountered marginal weather conditions and limited visibility due to low clouds. On approach, the twin engine aircraft struck the slope of Mt La Gama located in the Chorro del Indio National Park. Six people were seriously injured while four passengers were killed. The aircraft was destroyed by impact forces.
Probable cause:
Controlled flight into terrain after the crew initiated the descent prematurely in poor visibility.

Crash of a Cessna 421C Golden Eagle III in Sitka: 5 killed

Date & Time: Jul 3, 2003 at 1600 LT
Operator:
Registration:
N777DX
Flight Type:
Survivors:
No
Site:
Schedule:
Prince Rupert – Anchorage
MSN:
421C-0048
YOM:
1976
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
9200
Aircraft flight hours:
7981
Circumstances:
The pilot of the twin-engine accident airplane was on an IFR flight plan in instrument meteorological conditions when the right side nose baggage door opened. The pilot expressed concerns to air traffic control about baggage exiting the compartment and striking the right propeller. He requested a diversion to the nearest airport with an instrument approach. The flight was diverted as requested, and was cleared for a non precision instrument approach to a coastal airport adjacent to mountainous terrain. The flight was authorized to a lower altitude when established on the approach. A review of the radar track information disclosed that the pilot did not fly the published approach, but abbreviated the approach and turned the wrong direction, toward higher terrain, north of the approach course. The airplane was discovered in mountainous terrain, about 1,100 msl, and 1.5 miles north of the approach course. The crash path was initially at a shallow angle in the treetops, until the airplane struck larger trees. Post accident inspection of the airplane disclosed no evidence of any preimpact mechanical problems, other than the baggage door, which was still attached to the airplane.
Probable cause:
The pilot's failure to follow IFR procedures by not following the published approach procedures, which resulted in an in-flight collision with terrain. Factors contributing to the accident were a low ceiling, and the pressure induced by conditions/events (the open baggage door).
Final Report:

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.

Crash of a Yakovlev Yak-42D near Trabzon: 75 killed

Date & Time: May 26, 2003 at 0445 LT
Type of aircraft:
Operator:
Registration:
UR-42352
Survivors:
No
Site:
Schedule:
Bishkek - Trabzon - Zaragoza
MSN:
18 11 395
YOM:
1988
Flight number:
UKM4230
Country:
Region:
Crew on board:
13
Crew fatalities:
Pax on board:
62
Pax fatalities:
Other fatalities:
Total fatalities:
75
Aircraft flight hours:
18739
Aircraft flight cycles:
9700
Circumstances:
Chartered by the Spanish Government, the aircraft was completing a charter flight from Bishkek to Zaragoza with an intermediate stop in Trabzon, carrying 62 Spanish peacekeepers and 13 crew members. The 62 passengers were respectively 41 members of the Land Forces and 21 members of the Air Force who were returning to Spain following a peacekeeping mission in Afghanistan. While descending to Trabzon Airport by night, the crew encountered poor visibility due to foggy conditions. Unable to establish a visual contact with the approach lights and the runway 29, the crew initiated a go-around procedure. Few minutes later, while completing a second approach, the crew failed to realize he was not following the correct pattern for an approach to runway 29 when the aircraft impacted a mountain at an altitude of 4,600 feet. The aircraft disintegrated on impact and all 75 occupants were killed. The wreckage was found 3,5 km east of the village of Maçka, about 23 km southwest of the airport.
Probable cause:
The accident was the consequence of a controlled flight into terrain due to the combination of the following factors:
- Loss of situational awareness on part of the flying crew,
- The crew failed to comply with the Standard Operational Procedures published by the operator,
- The crew failed to follow the published approach charts,
- Implementation of a non-precision approach,
- Incorrect use of the automated flight systems,
- Inadequate training (LOFT),
- The crew descended below the MDA in limited visibility.

Crash of a Cessna 414 Chancellor in Canton: 1 killed

Date & Time: Apr 10, 2003 at 1700 LT
Type of aircraft:
Operator:
Registration:
N822DB
Flight Type:
Survivors:
No
Site:
Schedule:
Rome – Canton
MSN:
414-0813
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4500
Captain / Total hours on type:
245.00
Aircraft flight hours:
5078
Circumstances:
The VFR repositioning flight departed Rome, Georgia en route to Canton, Georgia but never arrived. Late on the evening of April 10, 2003, the pilot's spouse contacted the local authorities when her husband did not arrive at home or call. The spouse stated that her husband flew out of Rome early Thursday morning headed to Augusta, Georgia to pick up an unknown number of passengers and fly them back to Rome, Georgia. The authorities confirmed that the passengers had arrived at their destination. The Civil Air patrol began a search and located the airplane on the side of "Bear Mountain" in Canton, Georgia, on April 11, 2003. The wreckage site was located 11.3 nautical miles west of Cherokee County Airport, Canton, Georgia, and 26 nautical miles east of Rome, Georgia on the west side of Bear Mountain. The mountains ridgeline runs northeast and southwest, near the town of Waleska, Georgia. The field elevation at the crash site was 1,750 feet above mean sea level (msl) and the peak of Bear Mountain was 2,268 feet msl. The upslope of the terrain at the site was estimated at 30-40 degrees. Examination of the airframe, flight controls, engine assembly and accessories revealed no anomalies.
Probable cause:
The pilot's failure to maintain clearance from terrain.
Final Report:

Crash of a Cessna 207 Skywagon in Grants Pass: 2 killed

Date & Time: Apr 9, 2003 at 0850 LT
Registration:
N9785M
Survivors:
No
Site:
Schedule:
North Bend – Grants Pass
MSN:
207-0729
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
34976
Aircraft flight hours:
4516
Circumstances:
During a visual flight rules (VFR) cross-country flight from North Bend, Oregon, to Grants Pass, Oregon, the airplane collided with mountainous terrain approximately seven miles northwest of the pilot's planned destination. Weather data and witness reports outlined areas of low ceilings and low visibility throughout the area during the approximate time of the accident. Post-accident inspection of the aircraft and engine revealed no evidence of a mechanical malfunction or failure.
Probable cause:
The pilot's failure to maintain clearance from mountainous terrain while in cruise flight. Factors include low ceilings and mountainous terrain.
Final Report: