Ground accident of a Rockwell Aero Commander 500 in Treasure Cay: 1 killed

Date & Time: Jul 10, 1995 at 1430 LT
Registration:
N89M
Flight Phase:
Survivors:
Yes
Schedule:
Treasure Cay – West Palm Beach
MSN:
500-0659-18
YOM:
1958
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On July 10, 1995, about 1430 eastern daylight time, an Aero Commander 500, N89M, registered to Candy Yellow Apple, Inc., leased to and operated by Palm Beach Aviation, experienced separation of a propeller blade during the ground roll to takeoff from the Treasure Cay Airport, Treasure Cay, Bahamas. The nonscheduled, international, passenger flight was operating under 14 CFR Part 135. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed for the flight. The airplane was substantially damaged and the airline transport- rated pilot and five passengers were not injured. One passenger was fatally injured. The flight was originating at the time of the accident.
Probable cause:
The pilot stated that after applying full power to takeoff during the ground roll, he heard a loud sound then aborted the takeoff. Examination of the airplane revealed that 1 of the 2 propeller blades from the right propeller separated from the propeller hub and penetrated the cabin.

Crash of a De Havilland DHC-2 Beaver in Pine Lake: 5 killed

Date & Time: Jun 18, 1995 at 1525 LT
Type of aircraft:
Operator:
Registration:
C-FGBC
Flight Phase:
Survivors:
No
Schedule:
Tukanee Lake – Pine Lake – White River – Wawa
MSN:
199
YOM:
1952
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Crashed in unknown circumstances shortly after takeoff from Pine Lake, killing all five occupants.

Crash of a PZL-Mielec AN-2R in Kanlykul

Date & Time: Jun 17, 1995
Type of aircraft:
Operator:
Registration:
UK-33058
Flight Phase:
Survivors:
Yes
Schedule:
Kanlykul - Kanlykul
MSN:
1G218-45
YOM:
1986
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On a crop spraying flight for the sovkhoz (state farm) Sry-Altyn (Kanlykul district of Karakalpakstan) when the engine lost power shortly after take off from an airstrip located some 43 km northwest from Nukus. At a height of some 15-20 metres, the crew attempted a forced landing in a field when the left main gear struck a 2.5 metres high dam and the aircraft suffered substantial damage. Both pilots escaped unhurt.
Probable cause:
Engine failure for unknown reasons.

Crash of a Grumman G-21E Turbo Goose in DuPage: 2 killed

Date & Time: Jun 13, 1995 at 1955 LT
Type of aircraft:
Registration:
N121H
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
DuPage - DuPage
MSN:
1211
YOM:
1942
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4200
Captain / Total hours on type:
400.00
Circumstances:
This was the first flight of the Grumman G-21 in two years. Also, the pilot had not flown the G-21 for two years. Before taking off, the pilot reported that three takeoffs and landings would be needed for purposes of becoming current. After takeoff, he flew the airplane approximately one hour and made two full stop landings. During the third takeoff, the airplane was described as lifting off in a short distance and going into a nose high attitude below an altitude of 100 feet. The airplane then rolled left, struck the ground in a steep descent, and burned. Witnesses reported that the engines were providing power until impact; the engines and propellers had evidence of rotational damage. The flap actuators were found extended to a position that equated with 30° of flaps (half flaps). Four G-21 pilots were interviewed. According to them, flaps were not normally used for takeoff in this airplane. They reported that the turboprop engines had substantial power for the weight of the airplane, especially when the plane was not loaded, and that the G-21 would tend to become airborne quickly with flaps extended. No pre impact mechanical problem was noted during the investigation.
Probable cause:
The pilot allowed excessive nose-up rotation of the airplane during lift-off, and failed to obtain and/or maintain adequate airspeed, which resulted in an inadvertent stall and collision with the terrain. Factors relating to the accident were: the pilot's lack of recent experience in the make and model of airplane, and the use of flaps during a light weight takeoff.
Final Report:

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.