Crash of a Cessna 340A in Selma: 1 killed

Date & Time: Nov 6, 2000 at 0400 LT
Type of aircraft:
Operator:
Registration:
N12273
Flight Type:
Survivors:
Yes
Schedule:
Paso Robles – Selma
MSN:
340A-1536
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
19000
Captain / Total hours on type:
2000.00
Aircraft flight hours:
4915
Circumstances:
The airline transport rated pilot was returning an organ transplant nurse passenger to an uncontrolled, no facilities airport, with ground fog present about 0400 in the morning. The pilot had obtained two abbreviated preflight weather briefings while waiting for his passenger, and prior to departing at 0235. According to witnesses he attempted to land twice on runway 28, then he made an approach and attempted a landing on runway 10. Witnesses reported that the airport was engulfed in ground fog at the time of the approaches. They said that you could see straight up but not horizontally. The airplane collided with grape vineyard poles and canal/wash berms, about 250 feet short of the runway 10 displaced threshold. Approach charts for two airports with instrument approaches within 20 miles were found lying on the instrument panel glare shield. The passenger's car was parked at the uncontrolled airport.
Probable cause:
The pilot's improper decision to attempt a visual approach and landing in instrument meteorological conditions and his failure to follow instrument flight rules procedures.
Final Report:

Crash of a Boeing 747-2H7B in Paris

Date & Time: Nov 5, 2000 at 2157 LT
Type of aircraft:
Operator:
Registration:
TJ-CAB
Survivors:
Yes
Schedule:
Douala - Paris
MSN:
22378
YOM:
1981
Flight number:
UY070
Country:
Region:
Crew on board:
16
Crew fatalities:
Pax on board:
187
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
20250
Captain / Total hours on type:
12000.00
Copilot / Total flying hours:
14188
Copilot / Total hours on type:
9767
Aircraft flight hours:
48770
Aircraft flight cycles:
12872
Circumstances:
Following an uneventful flight from Douala, the crew started the descent to Paris-Roissy-CDG Airport by night and poor weather conditions. After touchdown on the wet runway 09R, the crew started the braking procedure when the aircraft went out of control, veered to the right off runway, crossed a grassy area, lost its nose gear and came to rest between both taxiways Z6 and Z7. All 203 occupants evacuated safely while the aircraft christened 'Mount Cameroon' was damaged beyond repair due to severe damages in the electronic bay because the nose landing gear penetrated the fuselage.
Probable cause:
The initial cause of the accident was the incomplete reduction of thrust on the left outer engine at the beginning of deceleration. This caused the de-activation of the automatic braking system and the non-extension of the n°1 thrust reverser. The inadvertent selection of full thrust on this engine after the landing created a high thrust asymmetry leading to the runway excursion. The lack of coordination and of joint control by the crew members, perhaps aggravated by the presence of third parties in the cockpit, contributed to the development of this situation.
Final Report:

Crash of a Rockwell Grand Commander 690B in São Tomé

Date & Time: Nov 1, 2000 at 1745 LT
Operator:
Registration:
N6900K
Flight Type:
Survivors:
Yes
Schedule:
Luanda - São Tomé
MSN:
690-11441
YOM:
1978
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, was completing a delivery flight from South Africa to the US via Luanda and São Tomé. Upon landing at São Tomé Airport, the left main gear collapsed. The aircraft slid on its belly for few dozen metres and came to rest. The pilot was uninjured.
Probable cause:
It was reported that the aircraft was unstable on final approach and not properly aligned with the runway centerline. This caused the aircraft to land hard in 'crab' configuration, causing the left main gear to collapse upon touchdown.

Crash of a Piper PA-60 Aerostar (Ted Smith 602P) in Coburg

Date & Time: Oct 30, 2000 at 1456 LT
Operator:
Registration:
D-IUAK
Flight Type:
Survivors:
Yes
MSN:
62-0920-8165044
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing on runway 12/30 which is 632 metres long, the twin engine aircraft was unable to stop within the remaining distance. It overran, lost its left wing and came to rest, bursting into flames. The pilot, sole on board, was slightly injured.

Crash of a Dornier DO.128 Skyservant near Warri: 6 killed

Date & Time: Oct 26, 2000
Type of aircraft:
Operator:
Registration:
NAF018
Flight Type:
Survivors:
No
Schedule:
Benin City – Warri
MSN:
6018
YOM:
1985
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
While approaching Warri Airport runway 06 following an uneventful flight from Benin City, the twin engine aircraft entered an uncontrolled descent and crashed near a refinery located near Jeddo, about 11 km west of the airport. All six occupants were killed, among them five Nigerian Army Officers.

Crash of an Ilyushin II-18D near Batumi: 84 killed

Date & Time: Oct 25, 2000 at 1722 LT
Type of aircraft:
Operator:
Registration:
RA-74295
Flight Type:
Survivors:
No
Site:
Schedule:
Moscow – Batumi
MSN:
187 0106 02
YOM:
1967
Location:
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
73
Pax fatalities:
Other fatalities:
Total fatalities:
84
Captain / Total flying hours:
1579
Captain / Total hours on type:
212.00
Copilot / Total flying hours:
1242
Aircraft flight hours:
15256
Aircraft flight cycles:
7694
Circumstances:
This flight between Moscow and Batumi was operated by the Russian Air Force twice a month. On board were Russian soldiers and family members returning to their base in Batumi following a leave period. Due to poor weather conditions west of Batumi, the crew was cleared to initiate the approach to Batumi-Chorokh Airport from the northeast to runway 31 while the usual approach is from the sea to runway 13. While descending in poor visibility at an altitude of 940 metres and a speed of 340 km/h, the aircraft struck the slope of Mt Mtirala (,1336 metres high) located about 17 km northeast of Batumi Airport. The aircraft disintegrated on impact and all 84 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew continued the approach in poor weather conditions below the minimum prescribed altitude and while deviated from the approach path. The following contributing factors were identified:
- Navigational error on part of the crew during the final stage of the approach,
- ATC based at Batumi Airport failed to determine the exact position of the aircraft and failed to warn the crew accordingly,
- The crew 's decision to continue the approach in such conditions rather than to divert to a suitable alternate airport,
- Erroneous data transmitted by ground navigational aids in the Batumi area.

Crash of a Beechcraft 300 Super King Air near Donaueschingen: 4 killed

Date & Time: Oct 24, 2000 at 1716 LT
Registration:
D-CFMC
Flight Type:
Survivors:
No
Site:
Schedule:
Donaueschingen - Donaueschingen
MSN:
FA-104
YOM:
1986
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The twin engine aircraft departed Donaueschingen-Villingen Airport in the afternoon on a local calibration mission. After several circuits over the area at an altitude of 7,000 feet, both NDB and DME systems have been calibrated and the crew was returning to the airport at the end of the afternoon. While approaching runway 36 in marginal weather conditions, the crew failed to realize his altitude was insufficient when the aircraft struck trees and crashed in a wooded area located about 15 km from the airport. The aircraft was destroyed and all four occupants were killed. According to published procedures, the crew was supposed to continue the approach at a minimum altitude of 4,500 feet until 11 km from the runway threshold then descending to 2,650 feet. For unknown reasons, the crew started the descent prematurely, causing the aircraft to impact terrain.
Probable cause:
Controlled flight into terrain after the crew descended too low under VFR mode in IMC conditions. The following contributing factors were identified:
- The crew canceled the IFR flight plan for an approach under VFR mode despite weather conditions were marginal and the visibility was insufficient,
- The crew failed to follow the approach checklist,
- The crew failed to complete an approach briefing,
- The crew did not proceed to any callouts on approach,
- The second pilot was procedurally not involved in cockpit work processes and decision-making,
- On approach, the crew referred to the Flight Management System (FMS type III series) which was initially dedicated to flight inspection purposes only,
- Measurement was performed by the flight engineer.

Crash of a Cessna 303 TCrusader near Dossenheim: 1 killed

Date & Time: Oct 20, 2000 at 0900 LT
Type of aircraft:
Operator:
Registration:
N9645C
Flight Type:
Survivors:
No
Site:
Schedule:
Regensburg - Mannheim
MSN:
303-00197
YOM:
1982
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
875
Circumstances:
The twin engine aircraft departed Regensburg-Oberhub Airport in the morning on a flight to Mannheim City. About 15 minutes prior to arrival, the pilot cancelled his IFR flight plan and started the descent under VFR mode. On approach, at an altitude of 1,700 feet and at a speed of 110 knots, the aircraft struck tree tops and crashed in a wooded and hilly terrain located east of Dossenheim, about 15 km southeast of Mannheim Airport, bursting into flames. The aircraft was destroyed by impact forces and a post crash fire and the pilot, sole on board, was seriously injured. He died from his injuries two weeks later.
Probable cause:
The decision of the pilot to continue the approach under VFR mode in IMC conditions. The limited visibility caused by low clouds was considered as a contributing factor. At the time of the accident, the hilly terrain was shrouded in clouds. For unknown reasons, the approach speed was relatively low (110 knots).
Final Report:

Crash of a Harbin Yunsunji Y-12 II in Sam Neua: 8 killed

Date & Time: Oct 19, 2000 at 1212 LT
Type of aircraft:
Operator:
Registration:
RDPL-34130
Survivors:
Yes
Site:
Schedule:
Vientiane – Sam Neua
MSN:
0086
YOM:
1994
Flight number:
QV703
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
While descending to Sam Neua Airport, the crew encountered poor weather conditions with limited visibility. Approaching in clouds, the aircraft struck the slope of a mountain located 12 km from the airport. Eight passengers were killed while nine other occupants were injured.
Probable cause:
Controlled flight into terrain after the crew descended too low in poor visibility. At the time of the accident, the aircraft deviated from the approach path from 4 to 6 km.

Crash of a Short SC.7 Skyvan 3 Variant 100 in Port Radium: 3 killed

Date & Time: Oct 8, 2000 at 1520 LT
Type of aircraft:
Operator:
Registration:
C-FSDZ
Flight Type:
Survivors:
No
Schedule:
Yellowknife – Kugluktuk – Port Radium – Yellowknife
MSN:
1953
YOM:
1977
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
22000
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
280
Copilot / Total hours on type:
100
Circumstances:
At 1108 mountain daylight time on 08 October 2000, the Summit Air Charter's Short Brothers SC-7 Skyvan, serial number SH1953, departed on a visual flight rules six-hour flight from Yellowknife, Northwest Territories, to Kugluktuk, Nunavut, to Port Radium, Northwest Territories, and back to Yellowknife. The flight plan indicated a one-hour stop in Kugluktuk, with an estimated time of arrival at Yellowknife of 1710. The pilot-in-command was the chief pilot of Summit Air Charters Ltd. A cargo handler, who was also a pilot, was in the co-pilot's seat, and there was one passenger. When the aircraft failed to arrive at Yellowknife, Search and Rescue (SAR) were alerted and a search was begun. At 2202 SAR personnel confirmed that the SAR satellite was picking up an emergency locator transmitter signal in the vicinity of Port Radium. SAR aircraft were directed to the signal location and found the signal source but were not able to see the wreckage because of fog and freezing rain. The wreckage was found at 1309 the following day. The aircraft had struck the top of steeply rising hills along the east shore of Great Bear Lake, approximately 2.9 nautical miles northeast of the Port Radium airstrip. The crash site is approximately 440 feet above the lake surface and 250 feet above the airstrip elevation (see Appendix A). The aircraft was destroyed, and the three persons on board were fatally injured.
Probable cause:
Findings as to Causes and Contributing Factors:
1. Although the pilot and the aircraft were certified for instrument flight, the pilot apparently continued to fly in accordance with visual flight rules after encountering marginal weather conditions and reduced visibility.
2. For undetermined reasons, the pilot descended below the elevation of the terrain surrounding the airstrip, resulting in a controlled-flight-into-terrain accident.
Finding as to Risk:
1. Given the pilot's flying time during the 30 days before the accident, the pilot=s performance might have been affected by fatigue.
Final Report: