Ground explosion of a Douglas DC-9-32 in Atlanta

Date & Time: Jun 8, 1995 at 1908 LT
Type of aircraft:
Operator:
Registration:
N908VJ
Flight Phase:
Survivors:
Yes
Schedule:
Atlanta - Miami
MSN:
47321
YOM:
1969
Flight number:
VJA597
Crew on board:
5
Crew fatalities:
Pax on board:
57
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9500
Captain / Total hours on type:
3500.00
Copilot / Total flying hours:
3800
Copilot / Total hours on type:
552
Aircraft flight hours:
63000
Circumstances:
As ValuJet Flight 597 began its takeoff roll, a 'loud Bang' was heard by the occupants, the right engine fire warning light illuminated, the crew of a following airplane reported to the ValuJet crew that the right engine was on fire, and the takeoff was rejected. Shrapnel from the right engine penetrated the fuselage and the right engine main fuel line, and a cabin fire erupted. The airplane was stopped on the runway, and the captain ordered evacuation of the airplane. A flight attendant (F/A) received serious puncture wounds from shrapnel and thermal injuries; another F/A and 5 passengers received minor injuries. Investigation revealed that an uncontained failure of the right engine had occurred due to fatigue failure of its 7th stage high compressor disc. The fatigue originated at a stress redistribution hole in the disc. Analysis of fatigue striation measurements indicated that the fatigue crack had originated before the disc was last overhauled at a repair station (Turk Hava Yollari) in 1991, but was not detected. Also, investigation of the repair station revealed evidence concerning a lack of adequate recordkeeping and a failure to use 'process sheets' to document the step-by-step overhaul/inspection procedures.
Probable cause:
Failure of Turk Hava Yollari maintenance and inspection personnel to perform a proper inspection of a 7th stage high compressor disc, thus allowing the detectable crack to grow to a length at which the disc ruptured, under normal operating conditions, propelling engine fragments into the fuselage; the fragments severed the right engine main fuel line, which resulted in a fire that rapidly engulfed the cabin area. The lack of an adequate record keeping system and the failure to use 'process sheets' to document the step-by-step overhaul/inspection procedures contributed to the failure to detect the crack and, thus, to the accident.
Final Report:

Crash of a Fletcher FU-24-954 in Lake Grassmere: 1 killed

Date & Time: Jun 7, 1995 at 1100 LT
Type of aircraft:
Operator:
Registration:
ZK-EMU
Flight Phase:
Survivors:
No
Site:
Schedule:
Lake Grassmere - Lake Grassmere
MSN:
274
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4930
Captain / Total hours on type:
235.00
Circumstances:
Shortly after takeoff from a field located in Lake Grassmere, while completing the 8th sortie of the morning, the pilot lost control of the airplane that crashed on hilly terrain. The aircraft was destroyed and the pilot was killed.
Probable cause:
Pilot incapacitation was the probable cause of this accident. The incapacitation of this pilot was an unusual event, and could not have been predicted or prevented by any reasonable or effective medical screening process.
Final Report:

Crash of a Short SC.7 Skyvan 3 Variant 400 in Hohenems

Date & Time: Jun 7, 1995
Type of aircraft:
Operator:
Registration:
OE-FDL
Flight Phase:
Survivors:
Yes
Schedule:
Hohenems - Hohenems
MSN:
1904
YOM:
1972
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft departed Hohenems-Dornbirn Airport on a local skydiving mission, carrying 23 skydivers and one pilot. After takeoff from runway 05, while climbing to a height of about 50 metres, the pilot encountered difficulties to gain height and elected to make an emergency landing when the right wing struck a tree. The aircraft stalled and crashed in an open field located 500 metres from the runway end. Four occupants, including the pilot, were injured. All 20 other occupants escaped uninjured. The aircraft was damaged beyond repair.
Probable cause:
It is possible that the aircraft was operated beyond its MTOW permissible limit.

Crash of a Beechcraft C-45 Expeditor in Bradburn lake

Date & Time: Jun 5, 1995 at 1040 LT
Type of aircraft:
Operator:
Registration:
C-FSFH
Flight Phase:
Survivors:
Yes
Schedule:
Bradburn Lake - Selkirk
MSN:
5840
YOM:
1943
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9000
Captain / Total hours on type:
700.00
Aircraft flight hours:
15748
Circumstances:
The Beech 18 seaplane was departing a fishing camp at Bradburn Lake, Manitoba, for its third flight of the day en route to the operator's base at Selkirk. After boarding the passengers and loading the baggage for the flight, the pilot taxied the aircraft to a position near the southwest shore of the lake and started the take-off run on an approximate heading of 015° true. During the take-off run, after the aircraft was "on the step," the pilot noticed a yaw to the left. He corrected the yaw with the aircraft's rudders and with differential engine power. Shortly thereafter, at about 60 miles per hour (mph), the yaw recurred and worsened. The left float separated from the aircraft and the left wing struck the water. The aircraft turned sharply to the left, stopped in the water, and came to rest on its left wing tip in about 15 feet of water. The pilot and the six passengers were not injured; they exited the sinking aircraft and swam to shore. The accident occurred at 1040 central daylight saving time (CDT) during daylight hours at latitude 51°55'N and longitude 95°35'W.
Probable cause:
The left front swivel fitting attachment bolt probably moved out of position because the securing nut was either not installed or came off in service. A series of failures ensued, culminating in the separation of the left float from the aircraft.
Final Report:

Crash of a Rockwell Grand Commander 680 in North Bend: 3 killed

Date & Time: Jun 1, 1995 at 1554 LT
Operator:
Registration:
N6877S
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
North Bend - North Bend
MSN:
680-462-132
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1450
Aircraft flight hours:
4785
Circumstances:
Approximately two minutes after takeoff, witnesses saw the airplane pull up sharply into a steep climb from underneath an 800-foot ceiling. The airplane went into an uncontrolled, nearly vertical dive and impacted into a river. The pilot did not hold multi-engine or instrument ratings. Individuals who knew the pilot, including an instructor who had flown with him, stated that they had doubted the pilot's competence but that the pilot had been confident of his own flying ability.
Probable cause:
The pilot initiating flight into weather conditions beyond what he was capable of handling. The pilot's overconfidence in his personal ability and the low ceiling were factors in the accident.
Final Report:

Crash of a Convair CV-440 Metropolitan in San Borja: 1 killed

Date & Time: May 22, 1995
Operator:
Registration:
CP-2142
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Borja - La Paz
MSN:
120
YOM:
1953
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
After takeoff from San Borja-Capitán Germán Quiroga Guardia Airport, while in initial climb, the copilot reported an engine failure. The crew attempted an emergency landing when the aircraft crashed in an open field located near the airport and came to rest, broken in several parts. Four people were injured and a passenger was killed.
Probable cause:
Engine failure for unknown reasons.

Crash of a Piper PA-31T Cheyenne in Liuli

Date & Time: May 16, 1995 at 1311 LT
Type of aircraft:
Registration:
5Y-FKI
Flight Phase:
Flight Type:
Survivors:
Yes
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3500
Circumstances:
Shortly after takeoff from Liuli Airstrip, while climbing, the pilot made a sharp turn to avoid a sand dune when he lost control of the aircraft that crashed on the ground. There were no casualties but the aircraft was written off.

Crash of a Fletcher FU-24-950 near Taupo

Date & Time: May 8, 1995 at 0720 LT
Type of aircraft:
Operator:
Registration:
ZK-EMB
Flight Phase:
Survivors:
Yes
MSN:
252
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
332
Captain / Total hours on type:
44.00
Circumstances:
Sole on board, the pilot was engaged in a crop spraying mission in the region of Taupo. Shortly after takeoff, while climbing at low height, the pilot initiated a right turn when the aircraft lost height and crashed in a pasture about 11 km northeast of Taupo. The aircraft was destroyed and the pilot was seriously injured.
Probable cause:
The following findings were reported:
- During a turning manoeuvre at a low height, the aircraft stalled and squashed onto the ground in a wing level attitude, at a high rate of descent,
- The height of the aircraft above the ground at the time afforded the pilot little opportunity for recovery,
- The pilot probably reverted to an unsafe flying practice he had adopted during his earlier training,
- The unsafe practice had been recognised by a previous instructor who, when not successful in correcting it, had discontinued the pilot's training,
- The final instructor had no reason to be concerned about the pilot's flying as he had exhibited no dangerous trends and flew as instructed,
- Had the final instructor been aware of a previous trait of the pilot to perform unsafe manoeuvres he might have been able to correct it,
- The causal factors in this accident were a lack of continuity in training records, pressure the pilot believed he was under to achieve maximum productivity in his flying with a minimum of delay, the pilot's apparent refusal to accept cautions in relation to his ability, and the Fletcher aircraft's performance during the execution of a limit manoeuvre too close to terrain.
Final Report:

Crash of an Antonov AN-2 in Sibay: 3 killed

Date & Time: May 4, 1995 at 1042 LT
Type of aircraft:
Operator:
Registration:
RA-19550
Flight Phase:
Survivors:
Yes
Schedule:
Sibay - Magnitogorsk
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft departed Sibay on a special flight to Magnitogorsk, carrying five members of the Civil Defense and two pilots. The purpose of the mission was to fly over the Ural River to study and predict flood activity. After takeoff, while in initial climb, the crew initiated a left turn when the aircraft entered an uncontrolled descent and struck the ground in a nose down angle of 40° about 1,280 metres from the runway end. A pilot and two passengers were killed while four other occupants were injured. The aircraft was destroyed.
Probable cause:
It was determined that the crew failed to prepare the flight according to published procedures and failed to follow the pre-takeoff checklist. It was found that the tail assembly was locked with a clamp that was installed by a ground mechanic and not removed prior to departure.

Crash of a Mitsubishi MU-2B-60 Marquise in Neuquén: 2 killed

Date & Time: May 3, 1995 at 2050 LT
Type of aircraft:
Operator:
Registration:
LV-MOP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Neuquén – Bahía Blanca – Buenos Aires
MSN:
742
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The twin engine aircraft was completing a cargo flight from Neuquén to Buenos Aires-Ezeiza Airport with an intermediate stop in Bahía Blanca, carrying two pilots on behalf of Encotesa. Shortly after departure from Neuquén-Juan Domingo Perón Airport, while climbing by night, the crew informed ATC about his ETA in Bahía Blanca when control was lost. The aircraft crashed in Chimpay, in the suburb of Neuquén, about 4 km northeast of the airport, bursting into flames. Both pilots were killed.
Crew:
Horacio Ovidio Filippini, pilot,
Valerio Augusto Diehl, pilot.
Probable cause:
The exact cause of the accident remains unclear. The crew did not send any distress call prior to the loss of control. It is believed that the accident was the consequence of a possible in-flight fire or toxic fumes emanating in the cabin due the presence of polyethylene stored in several boxes that were not properly packed according to dangerous goods transportation procedures.