Crash of a Pilatus PC-12/45 in the Sea of Okhotsk

Date & Time: Jul 8, 2001 at 1345 LT
Type of aircraft:
Operator:
Registration:
N660NR
Flight Phase:
Survivors:
Yes
Schedule:
Hakodate - Magadan
MSN:
356
YOM:
2000
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On July 8, 2001, approximately 1345 local time (0245UTC), a Pilatus PC-12/45, N660NR, registered to a US private owner, operated by Jeflyn Aviation, Inc. doing business as Access Air, and being flown by a US certificated airline transport rated pilot, was presumed destroyed following a ditching in the Sea of Okhotsk, Western Pacific Ocean. The pilot sustained minor injuries and the three remaining Japanese passengers were uninjured. Instrument meteorological conditions prevailed, and an IFR flight plan had been filed and activated. The flight, which was returning to the United States following a round-the-world trip, was being operated under 14CFR91 as a business trip. The aircraft had originated from Hakodate, Japan, departing 0910 hours local time and was destined for Magadan, Russia. The pilot reported in a telephonic interview that the aircraft was established in cruise at 8,100 meters altitude when he felt a vibration followed by a rapid increase in the engine's Turbine Temperature Indication (TTI). He reported that the TTI reached 1144 degrees during which there was a compressor stall. He shut the engine down, feathered the propeller, and initiated a power off emergency descent. During the emergency descent the pilot radioed a mayday on 121.5 MHz, set his transponder to code 7700, and manually activated the emergency locator beacon. The aircraft descended through multiple cloud layers during which the pilot and passengers prepared for the ditching. The pilot reported that upon breaking through the bottom of the last overcast layer, at 100 feet above the water, he encountered swells of approximately 8-12 feet height. He ditched the aircraft on the crest of a swell and the aircraft came to a stop floating in an upright, level attitude. All four occupants exited the aircraft through the main cabin door into a life raft. Over a period of several hours the occupants lost sight of the floating aircraft and after about 15 hours they were picked up by a Russian container ship and airlifted to Sakhalin Island.
Probable cause:
Engine failure for unknown reasons.

Crash of a Tupolev TU-154M in Burdakovka: 145 killed

Date & Time: Jul 4, 2001 at 0208 LT
Type of aircraft:
Operator:
Registration:
RA-85845
Survivors:
No
Schedule:
Yekaterinburg – Irkutsk – Vladivostok
MSN:
86A735
YOM:
1986
Flight number:
XF352
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
136
Pax fatalities:
Other fatalities:
Total fatalities:
145
Aircraft flight hours:
20953
Aircraft flight cycles:
11387
Circumstances:
The airplane departed Yekaterinburg Airport on a regular schedule flight (XF352) to Vladivostok with an intermediate stop at Irkutsk. The flight departed Yekaterinburg at 1947LT and climbed to the assigned cruising altitude of 10,100 metres. Some three hours into the flight, at 0150LT, the crew started the descent to Irkutsk Intl Airport. The copilot was the pilot-in-command. At 0205LT, the crew reported at 2,100 metres with the runway in sight. At this time, the aircraft' speed was 540 km/h. The maximum speed at which the landing gear may be lowered was 400 km/h. At 0206:56 the airplane leveled off at 900 metres with an airspeed still at 420 km/h. The first officer asked for gear down and the speed further decreased to 395 km/h with engines at idle. When the gear was down and locked, the airplane entered a left bank angle of 20-23°. The airspeed continued to drop to 365 km/h while the recommended speed was 370 km/h at this stage of the flight. Power was added slowly. This was only just sufficient for maintaining an altitude of 850 metres at 355-360 km/h. At 0207:46, while still in the left hand turn, the angle of attack increased to 16,5° because the autopilot attempted to maintain altitude with a decreasing speed. An aural warning sounded, informing the crew about a high angle of attack. The first officer attempted to correct this by using the control column and disconnected the autopilot. Because he deflected the control column to the left, the left bank increased to the maximum permissible value of -30° to -44°, and then to -48°. In a nose down attitude, the speed increased to 400 km/h then the aircraft entered clouds. By night, the crew lost visual contact with the ground and was not able to observe the natural horizon. In such conditions, the captain took over controls but alternately deflected the steering wheel to the left and right. An intensive deflection of steering control to the right caused a positive angular acceleration of +4,4° per second. The captain reacted by deflecting the steering wheel to the left again. The first officer now realized that the airplane was in a severe left bank of -45° and indicated that they should be rolling to the right. Because of an increase in vertical descent rate of 20 metres per seconds, one of the crew members pulled the control column. The airplane pitched up rapidly then entered a stall and a subsequent flat spin before crashing in an open field 22 seconds later. The aircraft was totally destroyed by impact forces and a post crash fire and all 145 occupants were killed.
Probable cause:
The accident was the consequence of a wrong approach configuration on part of the flying crew. The following contributing factors were identified:
- Poor control actions on part of the crew, which caused the aircraft to enter a super critical angle of attack followed by a stall and a spin,
- Violation of interactions by the crew regarding the separation of responsibilities for piloting established by the pilot-in-command,
- Lack of proper control to maintain flight parameters during the approach, in reference to the TU-154 flight operations manual,
- Poor crew interactions.

Crash of an Antonov AN-2 off Volzhsky: 3 killed

Date & Time: Jun 2, 2001
Type of aircraft:
Operator:
Flight Phase:
Survivors:
No
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The single engine aircraft was engaged in a local skydiving mission in the region of Volgograd. After some of the skydivers jumped out, the pilot decided to return to his departure point and two passengers remained in the cabin. For unknown reasons, the pilot started a quick descent when, at an altitude of 1,000 metres, he lost control of the airplane that entered a dive and crashed at a speed of 310 km/h in the Akthuba River located near Volzhsky. The aircraft was destroyed and all three occupants were killed.
Probable cause:
For unknown reasons, the pilot initiated a rapid descent when, apparently, the passenger who was seating on the copilot seat (and was not wearing his seatbelt), fell on the control column, causing the aircraft to become uncontrollable.

Crash of an Antonov AN-12B in Myakotino: 7 killed

Date & Time: May 22, 2001 at 1635 LT
Type of aircraft:
Operator:
Registration:
RA-12135
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Rzhev – Morshansk
MSN:
00 347 002
YOM:
1970
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was performing a cargo flight to Morshansk with a load consisting of a jet fighter engine. Seven minutes after takeoff from Rzhev Airport, while climbing to an altitude of 2,600 meters, the aircraft went out of control, entered a spin and crashed in a swampy and wooded area located in Myakotino, southeast of Rzhev. All seven crew members were killed. It is believed that control was lost following an engine failure and after the crew was unable to feather its propeller.

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

Date & Time: Apr 27, 2001 at 1131 LT
Type of aircraft:
Operator:
Registration:
RA-40997
Flight Phase:
Survivors:
Yes
Schedule:
Novoaleksandrovsk - Novoaleksandrovsk
MSN:
1G217-37
YOM:
1986
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a crop spraying mission in Novoaleksandrovsk. Shortly after takeoff, while at a height of about 50 metres, the crew raised the flaps when the engine failed. The crew elected to restart the engine but without success. In such situation, the captain attempted an emergency landing when the aircraft crash landed in a field and eventually collided with trees. Both pilots were injured and the aircraft was damaged beyond repair.
Probable cause:
The engine failed because the fuel used by the operator was not approved nor suitable for such engine.

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

Date & Time: Apr 25, 2001 at 1730 LT
Type of aircraft:
Operator:
Registration:
RA-17832
Flight Phase:
Survivors:
Yes
Schedule:
Nekrasovskaya - Nekrasovskaya
MSN:
1G204-33
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was dispatched at Nekrasovskaya to perform a crop spraying mission for the farm 'Rossia'. While flying at an insufficient height of 5 metres, the copilot saw power cables and elected to gain height to avoid the collision. But the captain took over control and plunged the aircraft to pass below the line. The power cables struck the tail that was partially torn off. The aircraft nosed down and crashed in an open field, bursting into flames. Both pilots were seriously injured and the aircraft was destroyed by fire.
Probable cause:
The accident was the consequence of the combination of the following factors:
- Poor flight preparation on part of the crew who failed to locate various obstacles situated in and around the spraying area,
- The captain took the decision to complete the mission at an insufficient height of five metres while the minimum height was fixed at 20 metres,
- Poor crew coordination.

Crash of a PZL-Mielec AN-2T in Kobyay

Date & Time: Apr 23, 2001 at 1745 LT
Type of aircraft:
Operator:
Registration:
RA-01122
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Pokrovsk – Magan – Kobyay – Sangar
MSN:
1G238-04
YOM:
1990
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
2135
Aircraft flight cycles:
3112
Circumstances:
The aircraft departed Pokrovsk on an ambulance flight to Sangar with intermediate stops in Magan and Kobyay. On approach to Kobyay Airport, the aircraft was too high and its speed was excessive. Rather than initiating a go-around procedure, the captain continued the approach and landed 375 metres pas the runway threshold (the runway length is 600 metres). Unable to stop within the remaining distance, the aircraft overran, collided with various obstacles and came to rest 50 metres further. The crew did not report the incident to the company and decided to take off few minutes later. After liftoff, the aircraft was unable to gain sufficient speed and height. It struck trees and crashed in a snow covered terrain, bursting into flames. All 13 occupants were injured, among them five seriously. The aircraft was destroyed by fire.
Probable cause:
It was determined that the captain was intoxicated at the time of the accident and that he started the mission from Pokrovsk already drunk. He took the decision to take off from Kobyay Airstrip despite the propeller blades have been damaged during the previous overrun.