Crash of a Douglas DC-9-51 in Abidjan

Date & Time: Apr 12, 1997 at 1350 LT
Type of aircraft:
Operator:
Registration:
9G-ACM
Survivors:
Yes
Schedule:
Accra - Abidjan
MSN:
47755
YOM:
1978
Flight number:
GH560
Location:
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
97
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Accra-Kotoka Airport, the crew started the descent to Abidjan-Félix Houphouët-Boigny Airport in poor weather conditions. Due to heavy rain falls, the horizontal visibility did not exceed 2 km and on final, the captain decided to initiate a go-around procedure. Few minutes later, the crew started a second approach to runway 21, established on the ILS but continued the approach above the glide. This caused the aircraft to land 900 metres past the runway threshold. On a wet runway surface, the aircraft skidded and veered off runway to the left. While contacting soft ground, the aircraft lost its undercarriage and came to rest 1,800 metres past the runway threshold. All 104 occupants were evacuated, among them three passengers were slightly injured. At the time of the accident, weather conditions were poor with heavy rain falls and wind from 110 gusting at 25 knots.

Crash of a Cessna 208B Grand Caravan in Wainwright: 5 killed

Date & Time: Apr 10, 1997 at 2030 LT
Type of aircraft:
Operator:
Registration:
N408GV
Survivors:
No
Schedule:
Barrow - Wainwright
MSN:
208B-0455
YOM:
1995
Flight number:
HAG502
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
3660
Captain / Total hours on type:
60.00
Aircraft flight hours:
1700
Circumstances:
The pilot had contacted the FSS 11 times on the day of the accident to obtain weather briefings. The conditions were below VFR minimums, which were required to conduct the passenger carrying commercial flight in a single-engine airplane. The conditions later improved and the pilot departed under a special VFR clearance. The pilot performed two approaches at the destination airport in IMC that were consistent with the two GPS approaches that were available there. Weather data and witnesses indicate that daylight conditions, low clouds and poor visibility prevailed, with cloud tops at 1,000 feet. After the second approach, the pilot radioed that he was heading back to the departure airport because he could not see the airport. No distress calls or unusual engine noises were heard. The airplane subsequently flew north of the airport and away from the departure airport at an altitude beneath the minimum radar coverage of 2,200 feet. It impacted the frozen Arctic Ocean in a right bank and at a 60-degree nose-down attitude about three miles away from the location of the pilot's last radio transmission. An examination of the airplane (before it sank through cracking ice) revealed no pre-impact mechanical malfunctions. An examination of the propeller revealed that it was under a power setting consistent with a maneuvering airspeed at the time of impact. An examination of the autopilot annunciator filament revealed that the autopilot was not engaged at impact. The airplane was nearly full of fuel and over its published maximum gross weight at impact. Small pieces of clear ice, about 1/4-inch thick, were found on portions of the tail surfaces. Interviews with operator employees and the pilot's wife revealed that the pilot may have felt pressure from himself and passengers to complete the flight.
Probable cause:
The pilot's intentional VFR flight into instrument meteorological conditions and his failure to maintain altitude/clearance from terrain. Factors contributing to the accident were the weather conditions.
Final Report:

Crash of a Convair CV-580 in Tshikapa

Date & Time: Apr 1, 1997
Type of aircraft:
Operator:
Registration:
9Q-CRU
Flight Phase:
Survivors:
Yes
Schedule:
Kinshasa – Tshikapa – Mbuji-Mayi
MSN:
41
YOM:
1967
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the captain heard a noise and suspected a technical problem so he decided to abandon the takeoff procedure. Unable to stop within the remaining distance, the aircraft overran and struck an embankment. All 14 occupants escaped uninjured while the aircraft was damaged beyond repair. It was reported that the crew initiated the takeoff in an up-slope configuration while the takeoffs at Tshikapa Airport are normally completed in a down-slope configuration. The runway is 1,000 metres long.

Crash of an Antonov AN-24RV in Cherkessk: 50 killed

Date & Time: Mar 18, 1997 at 1003 LT
Type of aircraft:
Registration:
RA-46516
Flight Phase:
Survivors:
No
Schedule:
Stavropol - Trabzon
MSN:
3 73 085 02
YOM:
1973
Flight number:
SVL1023
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
44
Pax fatalities:
Other fatalities:
Total fatalities:
50
Captain / Total flying hours:
12641
Captain / Total hours on type:
11600.00
Copilot / Total flying hours:
4563
Copilot / Total hours on type:
2657
Aircraft flight hours:
41181
Aircraft flight cycles:
27628
Circumstances:
While cruising at an altitude of 6,000 metres, the aircraft suffered a structural failure when the tail separated. The aircraft entered an uncontrolled descent and crashed in a wooded area located about one km from Cherkessk. The aircraft was totally destroyed upon impact and all 50 occupants were killed. The tail was found about 1,600 metres from the main wreckage. It was reported during investigations that the tail separated due to corrosion after the aircraft was operated in humid environment in Zimbabwe and DRC from 15 August 1994 till 28 December 1995.
Probable cause:
The accident was caused by the combination of the following factors:
1.Surface, without the use of instrumental control methods, by the commission's assessment of the technical condition of the An-24 RA 46516 aircraft and the subsequent unjustified issuance of a conclusion and a decision on the possibility of extending its MTO and service life;
2. Violation of the requirements of the current documents when extending the overhaul life for the An-24 RA 46516 aircraft and extending the established overhaul life without taking into account its long-term operation in a humid and hot climate;
3. Inconsistency of the regulatory documents governing the organization of work to establish and extend the resources and service life of civil aircraft (Regulation 1994) with the requirements of flight safety in modern conditions;
4. Violation of the requirements of the technology for repairing aircraft and household equipment during repairs in ARZ conditions;
5. Imperfection of technological documentation for periodic maintenance in terms of determining the corrosion and corrosion-fatigue state of the aircraft structure in hard-to-reach areas;
6. Insufficient control in the operation of hard-to-reach areas of the underground part of the fuselage in terms of determining the state of structural elements and the presence of corrosion lesions;
7. Failure to comply with the prescribed anti-corrosion measures for the structure of the aircraft during repairs at the ARP and in operation.
Final Report:

Crash of an Airbus A320-212 in Abu Dhabi

Date & Time: Mar 10, 1997 at 1056 LT
Type of aircraft:
Operator:
Registration:
A4O-EM
Flight Phase:
Survivors:
Yes
Schedule:
Muscat – Abu Dhabi – Bahrain – Cairo
MSN:
536
YOM:
1995
Flight number:
GF071
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
107
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 31 at Abu Dhabi Airport, just before V1, the aircraft started to vibrate and longitudinal control was lost. The captain decided to abandon the takeoff procedure and initiate an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, lost its nose gear and came to a halt few dozen metres further. On impact, the cockpit and both engines were almost destroyed and the left wing broke in two.
Probable cause:
It was determined that the vibration during the takeoff roll was the consequence of a tyre burst.

Crash of a Britten-Norman BN-2A-26 Islander near Guapiles

Date & Time: Mar 7, 1997 at 0900 LT
Type of aircraft:
Operator:
Registration:
N851JA
Flight Phase:
Survivors:
Yes
Schedule:
Tortuguero – San José
MSN:
913
YOM:
1981
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route from Tortuguero to San José, the pilot lost control of the airplane that crashed in a triple canopy jungle near Guapiles. All seven occupants were rescued and the aircraft was destroyed.
Probable cause:
Engine failure in flight for unknown reasons.

Crash of a Let L-410UVP-E in La Ceiba

Date & Time: Mar 3, 1997 at 0700 LT
Type of aircraft:
Operator:
Registration:
HR-IAS
Flight Phase:
Survivors:
Yes
Schedule:
La Ceiba - Puerto Lempira
MSN:
86 16 08
YOM:
1986
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Just after liftoff from runway 06, while in initial climb, the crew raised the landing gear and reduced the engine power. The aircraft stalled and sank back on the runway, slid for about 450 metres and came to rest. All 21 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Failure of the crew to reduce power shortly after rotation as it is specified in the flight manual on this model that the engine power cannot be reduced below the minimum altitude of 1,500 feet.

Crash of an Embraer EMB-120RT Brasília in Vilhena

Date & Time: Mar 3, 1997 at 0044 LT
Type of aircraft:
Operator:
Registration:
PT-MFC
Survivors:
Yes
Schedule:
Campo Grande - Vilhena
MSN:
120-206
YOM:
1990
Flight number:
PTN126
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9280
Captain / Total hours on type:
2501.00
Copilot / Total flying hours:
4153
Copilot / Total hours on type:
1988
Circumstances:
En route from Campo Grande to Vilhena, while in cruising altitude, the crew received the last weather bulletin about Vilhena with conditions below minimums. The copilot (under line check on this flight) suggested to divert to the alternate airport but the captain/instructor preferred to attempt an approach via Echo 1 and the NDB for runway 03. If visual contact would not be established at decision height, the crew would divert to the alternate airport. Then the copilot set the decision height at 2,500 feet which was wrong as the correct decision height was fixed at 2,560 feet. Nor the copilot nor the captain realized this mistake prior to start the descent to Vilhena Airport. On approach, the copilot was told by captain to monitor the horizon. He focused his attention on the horizon and failed to monitor the altimer. On his side, the captain elected to establish a visual contact with the ground and the runway light but is was later confirmed that the city of Vilhena suffered a general blackout. On final, the aircraft descended below MDA then struck trees and crashed less than one km from the runway threshold, bursting into flames. All 16 occupants evacuated safely while the aircraft was destroyed by fire.
Probable cause:
The following findings were identified:
- Poor crew coordination,
- Wrong approach configuration,
- The crew's attention was focused on their respective tasks without monitoring the approach configuration, causing the aircraft to descent below the glide,
- The captain/instructor failed to supervise properly the copilot's manoeuvres,
- No approach briefing,
- Lack of visibility due to a general blackout.

Final Report:

Crash of a Yakovlev Yak-40 in Semipalatinsk

Date & Time: Feb 19, 1997
Type of aircraft:
Operator:
Registration:
UN-87233
Survivors:
Yes
MSN:
9 53 18 42
YOM:
1975
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For unknown reasons, the aircraft landed at an excessive speed and was unable to stop within the remaining distance. It overran and came to rest few dozen metres further. All 18 occupants escaped uninjured while the aircraft was written off.

Crash of a Boeing 737-2C3 in Carajás: 1 killed

Date & Time: Feb 14, 1997 at 1234 LT
Type of aircraft:
Operator:
Registration:
PP-CJO
Survivors:
Yes
Schedule:
Belém – Marabá – Carajás – Brasília
MSN:
21013
YOM:
1974
Flight number:
RG265
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
48
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6138
Captain / Total hours on type:
2478.00
Copilot / Total flying hours:
1720
Copilot / Total hours on type:
1464
Circumstances:
The aircraft departed Belém-Val de Cans Airport on a flight to Brasília with intermediate stops in Marabá and Carajás, carrying 48 passengers and a crew of six. The approach to Carajás-Parauapebas Airport was completed in poor weather conditions with rain falls, clouds down to 120 metres and a limited visibility due to rain and fog. On final the aircraft was unstable and landed hard on runway 10. On touchdown, the right main gear was torn off and the aircraft went out of control. It veered off runway to the right, collided with trees and eventually came to rest in a wooded area. The copilot was killed as the right side of the cockpit was destroyed upon impact. Ten other people were injured and 43 escaped unhurt. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- Lack of crew coordination,
- The captain was overconfident,
- The copilot showed a lack of self confidence,
- The environment developed in the cockpit on approach allowed the pilots to deviate from the operational tasks primarily related to mutual controls,
- Poor approach and landing planning which required a higher sink rate than normal,
- The crew failed to make an approach briefing,
- Insufficient application of controls,
- The crew completed an unstable approach,
- Weather conditions were below minimums,
- The runway was not equipped with a lighting system but only with PAPIs,
- The crew failed to initiate a go-around procedure as the landing was obviously missed.
Final Report: