Crash of a Cessna 207 Skywagon in San Juan de Manapiare: 4 killed

Date & Time: Sep 16, 2005 at 1600 LT
Registration:
YV-412C
Flight Phase:
Survivors:
No
Site:
Schedule:
San Juan de Manapiare – Puerto Ayacucho
MSN:
207-0508
YOM:
1979
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Few minutes after takeoff from San Juan de Manapiare, while flying in marginal weather conditions, the single engine aircraft impacted a rocky face of Mt Morrocoy located about 8 km west of San Juan de Manapiare. The aircraft was totally destroyed by impact forces and all four occupants were killed.
Probable cause:
Controlled flight into terrain.

Crash of a Cessna 525 CJ1 in Alto da Boa Vista: 2 killed

Date & Time: Sep 16, 2005 at 1405 LT
Type of aircraft:
Operator:
Registration:
PT-WLX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Rio de Janeiro - Jacarepaguá
MSN:
525-0176
YOM:
1997
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total hours on type:
917.00
Copilot / Total hours on type:
2231
Aircraft flight hours:
2231
Circumstances:
The twin engine airplane departed Rio de Janeiro-Santos Dumont at 1402LT on a positioning flight to Jacarepaguá Airport located 23 km southwest from Santos Dumont Airport. After takeoff, the copilot informed ATC he maintained the altitude of 1,500 feet via route Bravo until the coast. Shortly later, while cruising in clouds at an altitude of 1,380 feet, the aircraft struck the slope of Mt Morro da Taquara located in the Tijuca National Park. The wreckage was found near Alto da Boa Vista and both pilots were killed. At the time of the accident, weather conditions were considered as marginal with low ceiling above the mountainous area.
Probable cause:
The accident was the consequence of a controlled flight into terrain after the crew decided to conduct this short flight under VFR mode in IMC conditions. The following contributing factors were identified:
- The visibility was reduced by the presence of a low ceiling over the mountains,
- Poor judgment on part of the crew regarding the existing flight conditions,
- Inadequate assessment of the distance between the aircraft and the ground,
- Continuation of the flight at an unsafe altitude for the area,
- Complacency and indiscipline of the crew,
- Poor flight planning,
- Lack of operational supervision.
Final Report:

Crash of a PZL-Mielec AN-2P in Przełęcz Koscierska

Date & Time: Sep 12, 2005
Type of aircraft:
Operator:
Registration:
1464
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
1G114-64
YOM:
1970
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft suffered an engine failure and crashed in a wooded area located near Przełęcz Koscierska, about 55 km southwest of Krakow. All 11 occupants were slightly injured while the aircraft was destroyed.
Probable cause:
Engine failure for unknown reasons.

Crash of a PZL-Mielec AN-2R near Ekimchan: 3 killed

Date & Time: Sep 4, 2005 at 1255 LT
Type of aircraft:
Operator:
Registration:
RF-00901
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ekimchan - Udskoye - Chumikan
MSN:
1G171-22
YOM:
1976
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft departed Ekimchan on a flight to Chumikan with an intermediate stop in Udskoye, carrying two pilots, one passenger and a load of food. Eight minutes after takeoff, while flying in poor weather conditions, the single engine aircraft struck the slope of Mt Bryus (1,767 metres high) located in the Selemja Mountain Range, some 19 km east of Ekimchan. The wreckage was found 12 days later, at an altitude of 1,560 metres. All three occupants were killed.
Probable cause:
Controlled flight into terrain after the crew decided to continue the flight under VFR mode in IMC conditions. It is possible that the crew lost his sense of orientation shortly after takeoff.

Crash of a Grumman S2F-1 Tracker in Valgorge: 2 killed

Date & Time: Aug 20, 2005 at 1000 LT
Type of aircraft:
Operator:
Registration:
F-ZBFE
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Marseille - Marseille
MSN:
32
YOM:
1957
Flight number:
Pélican 17
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3400
Copilot / Total flying hours:
5300
Circumstances:
The aircraft departed Marseille-Marignane and was dispatched in an area west of Aubenas to fight a forest fire with one other Tracker, one De Havilland DHC-8 and two Canadair CL-415. After a first Tracker successfully dropped its retardant, the second Tracker approached the area when it collided with hilly terrain and crashed, bursting into flames. Both pilots were killed.
Crew:
Régis Huillier, pilot,
Albert Pouzoulet, pilot.

Crash of a Boeing 737-31S near Grammatiko: 121 killed

Date & Time: Aug 14, 2005 at 1203 LT
Type of aircraft:
Operator:
Registration:
5B-DBY
Flight Phase:
Survivors:
No
Site:
Schedule:
Larnaca – Athens – Prague
MSN:
29099
YOM:
1998
Flight number:
ZU522
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
115
Pax fatalities:
Other fatalities:
Total fatalities:
121
Captain / Total flying hours:
16900
Captain / Total hours on type:
5500.00
Copilot / Total flying hours:
7549
Copilot / Total hours on type:
3991
Aircraft flight hours:
17900
Aircraft flight cycles:
16085
Circumstances:
On 14 August 2005, a Boeing 737-300 aircraft, registration number 5B-DBY, operated by Helios Airways, departed Larnaca, Cyprus at 06:07 h for Prague, Czech Republic, via Athens, Hellas. The aircraft was cleared to climb to FL340 and to proceed direct to RDS VOR. As the aircraft climbed through 16 000 ft, the Captain contacted the company Operations Centre and reported a Take-off Configuration Warning and an Equipment Cooling system problem. Several communications between the Captain and the Operations Centre took place in the next eight minutes concerning the above problems and ended as the aircraft climbed through 28 900 ft. Thereafter, there was no response to radio calls to the aircraft. During the climb, at an aircraft altitude of 18 200 ft, the passenger oxygen masks deployed in the cabin. The aircraft leveled off at FL340 and continued on its programmed route. At 07:21 h, the aircraft flew over the KEA VOR, then over the Athens International Airport, and subsequently entered the KEA VOR holding pattern at 07:38 h. At 08:24 h, during the sixth holding pattern, the Boeing 737 was intercepted by two F-16 aircraft of the Hellenic Air Force. One of the F-16 pilots observed the aircraft at close range and reported at 08:32 h that the Captain’s seat was vacant, the First Officer’s seat was occupied by someone who
2 was slumped over the controls, the passenger oxygen masks were seen dangling and three motionless passengers were seen seated wearing oxygen masks in the cabin. No external damage or fire was noted and the aircraft was not responding to radio calls. At 08:49 h, he reported a person not wearing an oxygen mask entering the cockpit and occupying the Captain’s seat. The F-16 pilot tried to attract his attention without success. At 08:50 h, the left engine flamed out due to fuel depletion and the aircraft started descending. At 08:54 h, two MAYDAY messages were recorded on the CVR. At 09:00 h, the right engine also flamed out at an altitude of approximately 7 100 ft. The aircraft continued descending rapidly and impacted hilly terrain at 09:03 h in the vicinity of Grammatiko village, Hellas, approximately 33 km northwest of the Athens International Airport. The 115 passengers and 6 crew members on board were fatally injured. The aircraft
was destroyed.
Probable cause:
Direct Causes:
1. Non-recognition that the cabin pressurization mode selector was in the MAN (manual) position during the performance of the:
a) Preflight procedure;
b) Before Start checklist; and
c) After Takeoff checklist.
2. Non-identification of the warnings and the reasons for the activation of the warnings (cabin altitude warning horn, passenger oxygen masks deployment indication, Master Caution), and continuation of the climb.
3. Incapacitation of the flight crew due to hypoxia, resulting in continuation of the flight via the flight management computer and the autopilot, depletion of the fuel and engine flameout, and impact of the aircraft with the ground.
Latent causes
1. The Operator’s deficiencies in organization, quality management and safety culture, documented diachronically as findings in numerous audits.
2. The Regulatory Authority’s diachronic inadequate execution of its oversight responsibilities to ensure the safety of operations of the airlines under its supervision and its inadequate responses to findings of deficiencies documented in numerous audits.
3. Inadequate application of Crew Resource Management (CRM) principles by the flight crew.
4. Ineffectiveness and inadequacy of measures taken by the manufacturer in response to previous pressurization incidents in the particular type of aircraft, both with regard to modifications to aircraft systems as well as to guidance to the crews.
Contributing Factors to the Accident:
1. Omission of returning the pressurization mode selector to AUTO after unscheduled maintenance on the aircraft.
2. Lack of specific procedures (on an international basis) for cabin crew procedures to address the situation of loss of pressurization, passenger oxygen masks deployment, and continuation of the aircraft ascent (climb).
3. Ineffectiveness of international aviation authorities to enforce implementation of corrective action plans after relevant audits.
Final Report:

Crash of a Canadair CL-415 in Calvi: 2 killed

Date & Time: Aug 1, 2005 at 1005 LT
Type of aircraft:
Operator:
Registration:
F-ZBEO
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ajaccio - Ajaccio
MSN:
2011
YOM:
1995
Flight number:
Pélican 36
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
After take-off from Ajaccio Airport and a first scooping, the fleet composed of three planes with respective callsigns Pelican 44, Pelican 36 and Pelican 37 intervened on a fire at Piétramaggiore, near Calvi, Corsica, France. A first sector of the fire zone was treated by six passes. During the two following passages, the fleet dropped on another sector of the fire. Pelican 36 began its last scooping in the Gulf of Revellata at heading 250°, three minutes and fourteen seconds before the accident. At the end, it gained height and continued the circuit to arrive on the drop axis. The "doubling" action consists of releasing the water load at the precise location of the previous aircraft's release. During the last turn, it reached an altitude of 2,160 feet. Pelican 36 was observed on a trajectory estimated to be consistent by the crew of the following aircraft (Pelican 37) a few seconds before it passed over the drop site. However, video evidence shows that the track of Pelican 36 is further west than that of Pelican 44, which preceded it, and over higher terrain. One and a half seconds before the flight recorder stopped, the aircraft was in a right turn at an altitude of 1,360 feet. The angle of roll to the right and increasing was then 17°. While the elevators were nearly stable, the altitude stored by the flight recorder increased to 1,500 feet in one and a half seconds. After that the tail section of the aircraft separated from the fuselage. The aircraft then impacted the side of a mountain and broke up.
Crew:
Ludovic Piasentin, pilot,
Jean-Louis de Bénédict, copilot.
Probable cause:
Environmental area:
The load case studied during the investigations did not explain the observed fuselage failure. However, the characteristics of the upward aerological disturbance caused by the fire are likely to have generated airframe stresses of an order of magnitude close to that of the loads capable of causing the fuselage to fail. Given the uncertainties encountered during the evaluation of the parameters of the rising air column that affected the accuracy of the research results concerning the effects of the stresses on the airframe, the aerological phenomenon encountered represents a possible cause of the event.
Technical Area:
The research undertaken to find in-flight loads capable, in the context of the event, of breaking the intact fuselage without damaging the empennage was unsuccessful. Detailed observation of the airframe did not reveal any damage prior to the occurrence. However, the results of these investigations do not rule out the existence of such damage, so the hypothesis of prior damage to the airframe cannot be totally rejected.

Crash of a Cessna 208B Grand Caravan in Hierba Buena: 2 killed

Date & Time: Jul 26, 2005 at 0940 LT
Type of aircraft:
Operator:
Registration:
TG-APG
Flight Phase:
Survivors:
No
Site:
Schedule:
Retalhuleu – Cuilco
MSN:
208B-1087
YOM:
2004
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew departed Retalhuleu on a special flight to Cuilco. En route, while proceeding to a mosquito control mission, the single engine airplane crashed in unknown circumstances on Mt Pinopa. Both pilots were killed.

Crash of an Antonov AN-24B near Malabo: 60 killed

Date & Time: Jul 16, 2005 at 1000 LT
Type of aircraft:
Operator:
Registration:
3C-VQR
Flight Phase:
Survivors:
No
Site:
Schedule:
Malabo – Bata
MSN:
7 99 011 04
YOM:
1967
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
54
Pax fatalities:
Other fatalities:
Total fatalities:
60
Circumstances:
After takeoff from Malabo Airport, the airplane encountered difficulties to gain sufficient height. It continued in a flat attitude until it impacted a hillside located about 19 km east of the airport, near Baney. The aircraft was totally destroyed and all 60 occupants were killed, among them several students flying to the continent for holidays.
Probable cause:
It was reported that the manifest showed a total of 35 passengers instead of 54. The aircraft, bought by Aerolineas de Guinea Ecuatorial in February 2002, was supposed to have its 1,000-hours maintenance check around January 2004, but due to financial problems, the company was unable to comply. The aircraft was sold to Equatair without the appropriate maintenance program completed in due time.

Crash of a Cessna T207 Turbo Skywagon on West Amatuli Island: 3 killed

Date & Time: Jul 1, 2005 at 1200 LT
Operator:
Registration:
N1621U
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Homer - Homer
MSN:
207-0221
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
8432
Aircraft flight hours:
7416
Circumstances:
The airline transport certificated pilot and the two pilot-rated passengers traveled to Alaska for a Title 14, CFR Part 91 personal flying vacation. The pilot received a VFR check-out in a rented airplane, and was the only person authorized by its owner to fly it. The pilot obtained a weather briefing for the day of the accident flight, and queried an FAA automated flight service station (AFSS) specialist about VFR conditions for a sightseeing flight. The FSS specialist stated, in part, "Well, it doesn't really look good probably anywhere today..." The area forecast included areas of marginal VFR and IFR conditions, and an AIRMET for mountain obscuration. The cloud and sky conditions included scattered clouds at 1,500 feet in light rain showers, with areas of isolated ceilings below 1,000 feet, and visibility below 3 statute miles in rain showers and mist. The weather briefing included a report from a pilot who was about 23 miles north of the accident scene about 2 hours before the accident airplane departed. The pilot reported fog and mist to the water, and said he was unable to maintain VFR. Five minutes after receiving the weather briefing, the accident pilot again called the AFSS and requested the telephone number to an automated weather observing system, located south of the point of departure, where VFR conditions were forecast. Local fishing charter captains reported fog in the area of the islands where the accident occurred. One vessel captain reported hearing an airplane in the vicinity of the islands, but could not see it because of the fog. The pilot did not file a flight plan, nor did he indicate any planned itinerary. The airplane was reported overdue two days after departure. The accident wreckage was located an additional two days later on the north cliff face of a remote island. The airplane had collided with the island at high speed, about 800 feet mean sea level, and a post crash fire had incinerated the cockpit and cabin area.
Probable cause:
The pilot's continued VFR flight into instrument meteorological conditions, which resulted in an in-flight collision with an island cliff during cruise flight. A factor contributing to the accident was fog in the area of the accident.
Final Report: