Crash of a De Havilland DHC-6 Twin Otter 100 near Timika: 17 killed

Date & Time: Apr 12, 2005 at 1058 LT
Operator:
Registration:
PK-LTZ
Flight Phase:
Survivors:
No
Site:
Schedule:
Timika – Enarotali
MSN:
23
YOM:
1966
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
The twin engine aircraft departed Timika-Moses Kilangin Airport at 1050LT on a 27-minutes flight to Enarotali, carrying 14 passengers and a crew of three. Some eight minutes into the flight, while cruising in poor weather conditions, the aircraft impacted hilly terrain. The wreckage was found two days later. The aircraft disintegrated on impact and all 17 occupants were killed. At the time of the accident, weather conditions were poor with low ceiling and rain falls.
Probable cause:
Controlled flight into terrain.

Crash of a Fokker F28 Fellowship 4000 in Coca

Date & Time: Apr 7, 2005 at 0955 LT
Type of aircraft:
Operator:
Registration:
HC-CDA
Survivors:
Yes
Schedule:
Quito – Coca
MSN:
11230
YOM:
1986
Flight number:
ICD504
Location:
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
60
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
36087
Aircraft flight cycles:
46662
Circumstances:
Following an uneventful flight from Quito, the crew started the approach to Coca Airport runway 15. Too low on final, the aircraft landed 4,5 metres short of runway. Upon impact, the left main gear was torn off. The aircraft rolled for 112 metres then veered off runway to the left, rolled another 263 metres then came to rest against a concrete wall. All 65 occupants were rescued, among them seven passengers were injured. The aircraft was damaged beyond repair.
Probable cause:
It was determined that the crew thought the Coca runway was short. To be able to stop the plane on the runway without excessive use of the brakes, the crew decided to land as early as possible. Doing so, the aircraft landed 4,5 metres short of runway. The published procedure request a minimum altitude of 50 feet over the threshold and the AFM showed a landing distance of 930 metres needed at maximum landing weight considering 42° of flaps, speed brakes out, lift dumpers armed, antiskid operative. Wrong approach procedure on part of the crew.

Crash of an Ilyushin II-18D-40 in Caracas

Date & Time: Mar 28, 2005 at 1615 LT
Type of aircraft:
Operator:
Registration:
CU-T1539
Flight Phase:
Survivors:
Yes
Schedule:
Caracas – Havana
MSN:
296 4017 102
YOM:
1983
Flight number:
CRN4311
Country:
Crew on board:
10
Crew fatalities:
Pax on board:
87
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 09, the captain decided to reject takeoff for unknown reasons. Unable to stop within the remaining distance, the four engine aircraft overran, lost its undercarriage and came to rest on the top of a hill with the n°1 engine torn off. All 97 occupants were rescued, among them 16 were injured, some seriously.

Crash of a Let L-410UVP-E in El Embrujo: 9 killed

Date & Time: Mar 26, 2005 at 0951 LT
Type of aircraft:
Operator:
Registration:
HK-4146
Flight Phase:
Survivors:
Yes
Schedule:
El Embrujo – San Andrés
MSN:
90 24 26
YOM:
1990
Flight number:
YH9955
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
6038
Captain / Total hours on type:
145.00
Copilot / Total flying hours:
868
Copilot / Total hours on type:
653
Aircraft flight hours:
6901
Circumstances:
The crew already completed four round trips the same morning on the same routing. During the takeoff roll from runway 35 at El Embrujo Airport, around V1 speed, the left engine speed. The crew continued the takeoff procedure while the speed dropped. Shortly after rotation, the aircraft rolled to the right to an angle of 135° then entered an uncontrolled descent and crashed in a wooded area located 117 metres past the runway end. Both pilots and seven passengers were killed while five others passengers were injured.
Probable cause:
The non-observance of the procedures described for an engine failure after V1, especially those relating to the maintenance of safe takeoff speed of 84 knots, the retraction of the flaps, automatic operation of the landing gear lever and the use of contingency power. The erroneous operation of the fuel-flow-control lever (FCL) of engine number one, the move from the open to the closed position during the chain of events, which left the plane and the inappropriate use of the fuel-flow-control lever (FCL) of engine number two, to bring it to the MAX NG position in an attempt to obtain performance of the engine. Maintaining an attitude of the plane on take-off after nr. 2 engine failure with the consequent reduction of speed and then maintaining the aircraft in a climbing attitude, after an engine shutdown, which came at stall speed and the subsequent lack of control of the aircraft. The failure of the engine for undetermined reasons during the takeoff roll, after V1, which forced the crew to perform a series of emergency procedures to deal with the fault and continue with the initial climb. The absence or failure of resource management among flight crew members during the sequence of events. The unmeasurable reduction in the situational awareness of the crew as a result of the financial situation of the company and the divorce in which the Captain of the aircraft was involved.
Final Report:

Crash of a Cessna 208B Grand Caravan off Belize City

Date & Time: Mar 9, 2005 at 1720 LT
Type of aircraft:
Operator:
Registration:
V3-HFW
Flight Phase:
Survivors:
Yes
Schedule:
Belize City – San Pedro
MSN:
208B-0791
YOM:
1999
Flight number:
9N2110
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Belize City-Sir Barry Bowen Municipal Airport, while in initial climb, the single engine aircraft went out of control and crashed in the sea, coming to rest upside down in shallow water. All 14 occupants were rescued while the aircraft was damaged beyond repair.
Probable cause:
Loss of control during initial climb due to windshear after weather conditions suddenly changed as a thunderstorm was approaching the airport.

Crash of a Boeing 737-242 near Kabul: 104 killed

Date & Time: Feb 3, 2005 at 1515 LT
Type of aircraft:
Operator:
Registration:
EX-037
Flight Phase:
Survivors:
No
Site:
Schedule:
Herat - Kabul
MSN:
22075
YOM:
1980
Flight number:
KMF904
Location:
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
97
Pax fatalities:
Other fatalities:
Total fatalities:
105
Circumstances:
On February 3, 2005, a Boeing 737-242 aircraft (the "Aircraft") with Kyrgyz Republic registration EX-037, operated by Phoenix Aviation, was conducting Kam Air Flight 904 from Herat to Kabul. There were a total of 105 occupants on board the Aircraft, including eight crew members and ninety-seven passengers. The Aircraft was cruising at flight level 270 when it contacted Bagram Radar Approach Control ("Bagram") for descent and landing. The flight was normal until it failed to level at flight level 130 during the VOR/DME approach. At 1043:24 UTC, Bagram cleared the flight to descend at its discretion and to expect the VOR approach to runway 29. The prevailing weather was also passed on to the Aircraft. Visibility was reported 2 kilometers with snow, ceiling 2,200 feet broken. wind calm and altimeter setting QNH 1016. AT 1043:58 UTC, when the Aircraft was 35 miles west of the Kabul VOR. radar contact was established with Ba9ram. The Aircraft was advised by Bagram to cross the VOR at or above flight level 130 and cleared it for the VOR/DME approach to runway 29. At 1048:41 UTC the Aircraft reported flight level 130. Bagram again cleared the Aircraft for the VOR approach to runway 29 and advised the Aircraft to report procedure turn inbound. The crew replied that they would report proceeding inbound for the VOR approach to runway 29. This was the last transmission from the Aircraft. At about 1050:11 UTC, Bagram stated that radar contact had been lost with the Aircraft. Bagram and Kabul Air Traffic Control Tower attempted to locate the Aircraft through radar and radio communication, but were not successful. Search for the Aircraft was delayed and hampered due to a severe snowstorm in the region. The Aircraft was located approximately three days later by an International Security Assistance Force (ISAF) helicopter approximately 30 kilometers southeast of Kabul International Airport at N 36 27.900 E 69 30.185. The Aircraft was destroyed by force of impact from colliding with the mountain. All 105 occupants on board the Aircraft had received fatal injuries. Subsequently, all bodies were recovered and identified. The wreckage was found at the altitude of 9,960 feet (3,035 metres) on the summit of Mt Shapiri Ghar located about 30 km southeast of Kabul Airport.
Probable cause:
The accident occurred probably due to the premature descent by the aircraft below its minimum assigned altitude of 13,000 feet during approach in weather conditions below VFR requirements. The reason for descending below the minimum altitude could not be determined due to inadequate evidence. The investigation was severely affected due to non-availability of FDR and CVR data readouts. The investigation was finalized to the extent possible based on the limited evidence available. The investigation revealed that the aircraft did not proceed to the VOR as instructed by the air traffic controller and descended below the minimum assigned altitude prior to being established on any segment of the approach. As a result, the aircraft collided with a mountain. The cause of descending below the assigned altitude could not be determined due to inadequate data and evidence.
Final Report:

Crash of a Cessna 208B Grand Caravan near Colquiri

Date & Time: Jan 21, 2005 at 1000 LT
Type of aircraft:
Operator:
Registration:
CP-2412
Flight Phase:
Survivors:
Yes
Site:
Schedule:
La Paz - Sucre
MSN:
208B-0897
YOM:
2001
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft departed La Paz-El Alto Airport at 0915LT on a schedule service to Sucre with 10 passengers and two pilots on board. About 45 minutes into the flight, the crew reported icing conditions. The aircraft lost height and crashed on the slope of Mt Huaricollo. All 12 occupants were rescued and the aircraft was destroyed.
Probable cause:
Loss of control following an excessive accumulation of ice/frost while flying in freezing fog conditions.

Crash of a McDonnell Douglas MD-83 in Cali

Date & Time: Jan 8, 2005 at 1548 LT
Type of aircraft:
Operator:
Registration:
VP-BGI
Survivors:
Yes
Schedule:
Cartagena – Cali
MSN:
49940
YOM:
1990
Flight number:
RPB7463
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
164
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
41329
Aircraft flight cycles:
18037
Circumstances:
After landing at Cali-Alfonso Bonilla Aragón Airport, the aircraft encountered difficulties to decelerate properly. It overrun the runway 19 (which is 9,842 feet long), lost its undercarriage, collided with the perimeter fence and came to rest on its belly. Six passengers were slightly injured while all other occupants escaped unhurt. The aircraft was damaged beyond repair.
Probable cause:
The accident was caused by a chain of errors and mistakes which began by accepting and carrying out a hasty descent that led to the omission of key points in the checklist such as the arming of the spoilers, excessive descent rate and speed and a configuration that led to faulty placement of the aircraft on the runway in abnormal conditions and 862 meters from the normal touchdown point. These conditions caused a vibration of the right main landing gear that could not be controlled by the Shimmy Damper, allowing higher loads to the strength of the undercarriage, which broke.

Crash of a Partenavia P.68 off Puerto Villamil: 2 killed

Date & Time: Dec 21, 2004 at 1219 LT
Type of aircraft:
Operator:
Survivors:
No
Schedule:
Baltra Island - Puerto Villamil
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The twin engine aircraft departed Galapagos International Airport (Baltra Island) at 1200LT on a flight to Puerto Villamil Airport, Isabela Island, carrying one passenger and one pilot. At 1219LT, the pilot was cleared to descend to Puerto Villamil Airport when he lost control of the airplane that crashed in the sea. The wreckage was found few hundred metres offshore at 1655LT. Both occupants were killed. The accident occurred three minutes prior to landing.

Crash of a McDonnell Douglas MD-82 in Surakarta: 25 killed

Date & Time: Nov 30, 2004 at 1815 LT
Type of aircraft:
Operator:
Registration:
PK-LMN
Survivors:
Yes
Schedule:
Jakarta – Surakarta
MSN:
49189
YOM:
1984
Flight number:
JT583
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
156
Pax fatalities:
Other fatalities:
Total fatalities:
25
Aircraft flight hours:
56674
Aircraft flight cycles:
43940
Circumstances:
While descending to Surakarta-Adisumarmo Airport, the crew was informed about stormy conditions at destination with cumulonimbus and heavy rain falls over the airport with a ceiling at 1,500 feet. The approach was continued and after touchdown on runway 26, the crew started the braking procedure and activated the thrust reverser systems. ON a wet runway, the aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and slid for few dozen metres, collided with equipments of the localizer antenna, a fence and came to rest in a cemetery. Both pilots and 23 passengers were killed while 70 other occupants were injured. 68 occupants escaped unhurt. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- About 3 mm of water was stagnating on the runway surface, reducing the braking action,
- The crew completed the landing procedure with a 13 knots tailwind component,
- Airbrakes deployed after touchdown but retracted few seconds later due to wrong position of the power levers,
- Power levers were not in idle position after touchdown but slightly forward, so the flight computer increased power,
- Heavy rain falls,
- The crew failed to initiate a go-around procedure.