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

Date & Time: Mar 24, 1989
Type of aircraft:
Operator:
Registration:
CCCP-33463
Survivors:
Yes
MSN:
1G228-13
YOM:
1988
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach, the single engine aircraft entered foggy conditions, struck the ground and crashed. There were no casualties.

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

Date & Time: Mar 16, 1989
Type of aircraft:
Operator:
Registration:
CCCP-41383
Flight Phase:
Survivors:
Yes
MSN:
1G67-01
YOM:
1966
Location:
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed following an engine failure. There were no casualties.
Probable cause:
Engine failure for unknown reasons.

Crash of a Fokker F28 Fellowship 1000 in Dryden: 24 killed

Date & Time: Mar 10, 1989 at 1209 LT
Type of aircraft:
Operator:
Registration:
C-FONF
Flight Phase:
Survivors:
Yes
Schedule:
Thunder Bay - Dryden - Winnipeg
MSN:
11060
YOM:
1972
Flight number:
GX1363
Location:
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
65
Pax fatalities:
Other fatalities:
Total fatalities:
24
Captain / Total flying hours:
24100
Captain / Total hours on type:
82.00
Copilot / Total hours on type:
65
Aircraft flight hours:
20852
Aircraft flight cycles:
23773
Circumstances:
Air Ontario Flight 1363, a Fokker F-28 jet, crashed during takeoff from Dryden Municipal Airport, Ontario, Canada. Of the 69 persons on board, 24 suffered fatal injuries. The aircraft in question, registration C-FONF, had suffered from a malfunctioning auxiliary power unit (APU) for the five days preceding the accident. Throughout the week preceding March 10, Air Ontario maintenance attempted, with limited success, to cure the APU problems. On March 9 it was decided to defer the repair of the APU until the aircraft returned to Toronto on the night of March 10. This meant that the aircraft was dispatched with the APU inoperable. On the morning of March 10, C-FONF departed Winnipeg on a round trip flight to Dryden, Thunder Bay and back as flight 1362/3. Since no external power unit was available at Dryden, the engines couldn't be restarted in case of engine shutdown on the ground. The flight to Thunder Bay was uneventful apart from a slight delay due to poor weather at Thunder Bay. As the aircraft was prepared for the return flight, it appeared that the aircraft was overweight as a result of ten additional passengers having transferred to the flight due to an earlier cancellation. The Air Ontario duty manager decided to off-load fuel and to arrange refuelling at Dryden. This caused an additional delay of 35 minutes. The Fokker F-28 departed Thunder Bay at 11:55 hours EST, about one hour behind schedule. The aircraft landed at Dryden at 11:39 hours CST. It began to snow lightly when the aircraft landed. Between 11:40 and 12:01, Air Ontario 1363 was refuelled with the right engine operating and with the passengers remaining on board the aircraft. This so called 'hot refuelling' procedure was followed because the APU was unserviceable. Eight passengers deplaned in Dryden and seven passengers boarded the aircraft. Meanwhile, snow was accumulating on the wings, forming a layer of 1/8-1/4 inch. No de-icing was done because de-icing with either engine running was prohibited by both Fokker and Air Ontario. The aircraft then taxied to runway 29 for departure, but was instructed to hold as there was a Cessna 150 on approach. The snow was continuing to fall heavily, becoming increasingly thick on the wings. At 12:09 the aircraft started it's takeoff roll on the slush-covered runway 29. There was an accumulation of at least one-half inch of wet, layered snow on the wings of the F-28 as it began its takeoff roll. After a longer than normal takeoff roll, the aircraft was rotated near taxiway Alpha, at approximately the 3500 foot mark. The aircraft lifted off slightly, began to shudder, and then settled back down onto the runway. The takeoff roll then continued and the aircraft was rotated a second time, finally lifting off at approximately the 5700 mark of the 6000 foot runway. It flew over the end of the runway approximately 15 feet above the ground. It thereafter failed to gain altitude and mushed through the air in a nose-high attitude, before commencing to strike trees. The aircraft crashed and came to rest in a wooded area, 3156 feet past the runway end and caught fire.
Probable cause:
The captain, as the pilot-in-command, must bear responsibility for the decision to land and take off in Dryden on the day in question. However, it is equally clear that the air transportation system failed him by allowing him to be placed in a situation where he did not have all the necessary tools that should have supported him in making the proper decision.
Final Report:

Ground accident of a PZL-Mielec AN-2TP in Guryev

Date & Time: Feb 27, 1989
Type of aircraft:
Operator:
Registration:
CCCP-32259
Flight Phase:
Survivors:
Yes
MSN:
1G96-21
YOM:
1968
Location:
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Damaged beyond repair at Guryev Airport after being caught by strong winds while taxiing to takeoff. There were no casualties.

Crash of a Boeing 737-2B1 in Lichinga

Date & Time: Feb 9, 1989
Type of aircraft:
Operator:
Registration:
C9-BAD
Survivors:
Yes
Schedule:
Maputo - Lichinga
MSN:
20786
YOM:
1973
Flight number:
TM195
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
102
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach and landing at Lichinga Airport was completed in heavy rain falls. After touchdown, the aircraft suffered aquaplaning and was unable to stop within the remaining distance. It overran, lost a gear and an engine then came to rest few dozen meters further. All 108 occupants escaped uninjured while the aircraft was damaged beyond.

Crash of a PZL-Mielec AN-2P in Chusovskoy

Date & Time: Feb 8, 1989
Type of aircraft:
Operator:
Registration:
CCCP-07365
Flight Phase:
Survivors:
Yes
MSN:
1G149-69
YOM:
1973
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Chusovskoy Airstrip, while in initial climb, the single engine aircraft collided with a tree and crashed on the ground. All 14 occupants escaped uninjured while the aircraft was damaged beyond repair.

Ground accident of a PZL-Mielec AN-2P in Izhevsk

Date & Time: Feb 7, 1989
Type of aircraft:
Operator:
Registration:
CCCP-70313
Flight Phase:
Survivors:
Yes
MSN:
1G140-17
YOM:
1972
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taxiing at Izhevsk Airport, the single engine aircraft collided with a light pole. There were no casualties but the aircraft was damaged beyond repair.

Crash of a Fokker F27 Friendship 600 in Yangon: 26 killed

Date & Time: Feb 3, 1989 at 0741 LT
Type of aircraft:
Operator:
Registration:
XY-AEK
Flight Phase:
Survivors:
Yes
Schedule:
Yangon - Keng Tung
MSN:
10325
YOM:
1967
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
26
Aircraft flight hours:
36361
Aircraft flight cycles:
45648
Circumstances:
Just after takeoff from runway 03 at Yangon-Mingaladon Airport, the aircraft banked left then struck a tree located about 150 meters past the end of the runway. It descended and crashed in a nose-down attitude of 3°, bursting into flames. Three occupants were injured while 26 others were killed. At the time of the accident, the visibility was poor due to thick fog.
Probable cause:
The assumption that the loss of control during initial climb occurred after the pilot-in-command suffered a spatial disorientation was not ruled out.

Ground fire of an Avia 14PT in Mirny: 3 killed

Date & Time: Jan 26, 1989 at 2025 LT
Type of aircraft:
Operator:
Registration:
CCCP-52066
Flight Phase:
Survivors:
No
MSN:
030 703108
YOM:
1957
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While parked and refueled at the Mirny Ice Station, the aircraft caught fire. Fire brigade arrived on scene in 10 minutes but the aircraft was already destroyed. Three crew members who were preparing the flight scheduled for midnight were killed. At the time of the accident, the outside temperature was -9° C. with good visibility (over 20 km) and a wind of 50 km/h (14 meters per second).
Crew:
Mr. Ananiev,
Mr. Semin,
Mr. Rogovenko.
Probable cause:
The exact cause of the fire could not be determined with certainty.

Crash of a Swearingen SA226TC Metro II in Örnsköldsvik

Date & Time: Jan 21, 1989 at 1747 LT
Type of aircraft:
Operator:
Registration:
OY-ARI
Survivors:
Yes
Schedule:
Örnsköldsvik - Örebro
MSN:
TC-317
YOM:
1979
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2900
Captain / Total hours on type:
500.00
Copilot / Total flying hours:
1025
Copilot / Total hours on type:
268
Aircraft flight hours:
8009
Circumstances:
After takeoff from Örnsköldsvik Airport, while climbing to an altitude of 7,000 feet, the left engine oil pressure warning light sounded. The crew shut down the engine but was unable to feather the propeller. Doing so, a fuse blew and only the right side of the instrument lights remained functional. After being cleared to return, the crew completed a turn but on approach, he was forced to use full elevator and rudder deflection because the left propeller could not be feathered. Misaligned, the aircraft landed 30 meters to the left of the runway then rolled few dozen meters before coming to rest. All 17 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Because the left propeller could not be feathered, this created drag the the crew was forced to compensate with trim and rudder deflection, causing the aircraft to be misaligned on final approach.
The following contributing factors were reported:
- An oil leak in the left engine during initial climb forced the crew to shut it down,
- Power supply problems caused by the left side not having been isolated from the right side,
- Wrong adjustment of the speed control trigger,
- Inadequate following of the checklist.
Final Report: