Crash of a Pilatus PC-6/B2-H4 Turbo Porter near Yahatma: 3 killed

Date & Time: Sep 22, 2011 at 1313 LT
Operator:
Registration:
PK-UCE
Flight Phase:
Survivors:
No
Site:
Schedule:
Pagai - Wamena
MSN:
943
YOM:
2004
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
11312
Captain / Total hours on type:
2647.00
Aircraft flight hours:
5774
Aircraft flight cycles:
6662
Circumstances:
On 22 September 2011, a PC 6 Pilatus Porter aircraft, registration PK-UCE was being operated by Yayasan Jasa Aviasi Indonesia (YAJASI) departed from Pagai to Wamena. The aircraft departed at 0403 UTC1 (1303 LT) and estimated to arrive at Wamena was at 0436 UTC. Aircraft cruise at altitude of 10,000 feet and conducted under Visual Flight Rules (VFR) and followed the visual route via North Gap corridor, which one of visual route to Wamena. Prior to enter the North Gap corridor at time 0413 UTC, the pilot sent a message via a system they called AFFIS to the company Flight Following Officer at Sentani Airport, which was the operation base. The pilot also sent a blind transmission message through Wamena Tower radio frequency. This was local procedure, to submit the message consists of position, altitude and destination to make the other aircraft pilots aware each other. As in the intern YAJASI flight following procedure, pilot should send message when the flying passes the North Gap corridor. In this flight, until the normal elapsed time, the pilot did not send any message to their Flight Following Officer at Sentani that the flight has passed the North Gap corridor. Since there was no message nor radio contact from the pilot until the ETA in Wamena, the Flight Following Officer at Sentani informed to the other personnel at the operation base, and alarmed to the other YAJASI aircraft which were flying in that area to start search the PK-UCE. Some other aircrafts which were flying in the vicinity also contacted to search the PKUCE. PK-UCE was found in mountain location adjacent to Pass Valley airstrip. The accident site was at coordinate S 030 54’ 54.4’’, E 1390 02’ 24.3”, the aircraft was hit the trees and the ground where the elevation was about 7500 feet , the propeller blades was not on feather and bent rearward, the left wing was broken and the aircraft stopped on heading about 85°.
Probable cause:
The pilot decided to descend from the cruise altitude 10000 feet to penetrate the area of marginal weather was most likely not as what his perceive. The pilot avoided the cloud to the left of the VFR route guidance and most likely that the space available was less than the requirement stated for the Weather Minimum class F.
Final Report:

Crash of a Cessna 208B Grand Caravan near Notnare: 2 killed

Date & Time: Sep 9, 2011 at 1230 LT
Type of aircraft:
Operator:
Registration:
PK-VVE
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Wamena - Kenyam
MSN:
208B-1287
YOM:
2007
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1546
Captain / Total hours on type:
1315.00
Copilot / Total flying hours:
927
Copilot / Total hours on type:
147
Aircraft flight hours:
3926
Aircraft flight cycles:
5267
Circumstances:
A Cessna 208B Grand Caravan I was destroyed when it crashed in the Yahukimo District, Indonesia. Both crew members were killed. The airplane was being operated on a non-scheduled cargo flight from Wamena Airport to Kenyam Aerodrome in Papua, Indonesia. The flight was being conducted under visual flight rules (VFR) and the pilot reported to ATC that the planned altitude was 9,500 feet. On board the aircraft were two pilots, a manifested load of diesel drums and grocery items, and a non-manifested load of 25 bags of rice weighing 827 lb (375 kg). The takeoff weight, based on the manifested cargo and the additional load of rice was estimated by the investigation to be 9,681 lb (4,391 Kg) which was 619 lb (281 Kg) above the certificated maximum takeoff weight. Also, the aircraft Centre of Gravity (C of G) was outside the certificated C of G envelope. The aircraft took off from Wamena runway 15 at 12:17 local time. The aircraft was then flown along a track toward Kenyam which was consistent with the route used by other company pilots and previously flown by the pilot in command. The additional loading contributed to a reduced rate of climb during the flight which resulted in the aircraft being below 10,000 ft as it approached the high terrain. This altitude was 1,500 ft lower than the altitude specified in the operator's route guide for operations between Wamena and Kenyam, and lower than the altitude flown by other company pilots when operating in the area, including three other flights on the day of the accident which overflew the high terrain between 11,200 and 12,500 ft. At 12:29:43, as the aircraft approached the high terrain at an altitude of 9,538 ft, the airspeed commenced decreasing which was accompanied by the average rate of climb increasing to about 390 fpm. It is probable that the pilots recognized the proximity of the terrain and attempted to improve the aircraft's angle of climb by decelerating towards the best angle of climb speed of 72 kts. The recorded data showed that 31 seconds after the airspeed started to decrease, the engine power varied with a maximum engine torque of 1,675 ft/lb being recorded at 12:30:30 with changes in the other engine parameters being consistent with a selection of a higher power setting. This is likely to have been associated with the pilot's attempts to improve terrain clearance. The recorded data then showed the aircraft in a descending right turn for about 6 seconds. The altitude reduced over a period of 4 seconds from 9,865 ft to 9,728 ft at an average rate of descent of about 2,000 fpm. This turn was likely to have been initiated to either avoid cloud or improve terrain clearance. The aircraft subsequently commenced to roll to the left at 12:30:35 with the left roll continuing for the following 14 seconds. It was likely that the left turn was initiated to avoid either cloud or terrain. During the left turn, the angle of bank reached a maximum value of 46° and the aircraft descended from 9,728 ft to 9,045 ft at a high rate of descent. The airspeed also increased from 92 kts to 122 kts during the descent. The engine power was reduced to idle soon after the aircraft commenced descending which was most likely due to the handling pilot attempting to recover from the high descent rate and increasing airspeed. The recorded data indicated that three EGPWS alerts activated during the descent. The aircraft had stopped descending at 12:30:50 and had commenced climbing with a reducing left angle of bank when the airplane impacted terrain at an elevation of 9,100 feet.
Probable cause:
Factors that contributed to the accident are as follows:
a. The aircraft was loaded to a weight in excess of the maximum certificated takeoff weight.
b. The aircraft climb performance was adversely affected by the aircraft being operated above the certificated maximum takeoff weight.
c. The aircraft approached high terrain along the proposed route at an altitude which was below that specified in the operator's route guide.
d. The aircraft entered a high rate of descent during a terrain avoidance maneuver.
e. Recovery from the abnormal flight path was not achieved before the aircraft collided with terrain.
Final Report:

Crash of a PZL-Mielec AN-2R near Sasha: 1 killed

Date & Time: Sep 3, 2011 at 1200 LT
Type of aircraft:
Operator:
Registration:
UR-17739
Flight Phase:
Survivors:
No
MSN:
1G202-59
YOM:
1983
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Sole on board, the pilot was completing a crop spraying mission between the villages of Sasha and Kostyukivka. While manoeuvring at low height, the single engine aircraft hit tree tops, stalled and crashed, bursting into flames. The aircraft was destroyed by impact forces and a post impact fire and the pilot was killed.

Crash of a Cessna T207A Turbo Stationair 8 in Nightmute

Date & Time: Sep 2, 2011 at 1335 LT
Operator:
Registration:
N73789
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Tununak - Bethel
MSN:
207-0629
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1670
Captain / Total hours on type:
216.00
Aircraft flight hours:
19562
Circumstances:
On September 2, 2011, about 1335 Alaska daylight time, a Cessna 208B airplane, N207DR, and a Cessna 207 airplane, N73789, collided in midair about 9 miles north of Nightmute, Alaska. Both airplanes were being operated as charter flights under the provisions of 14 Code of Federal Regulations (CFR) Part 135 in visual meteorological conditions when the accident occurred. The Cessna 208B was operated by Grant Aviation Inc., Anchorage, Alaska, and the Cessna 207 was operated by Ryan Air, Anchorage, Alaska. Visual flight rules (VFR) company flight following procedures were in effect for each flight. The sole occupant of the Cessna 208B, an airline transport pilot, sustained fatal injuries. The sole occupant of the Cessna 207, a commercial pilot, was uninjured. The Cessna 208B was destroyed, and the Cessna 207 sustained substantial damage. After the collision, the Cessna 208B descended uncontrolled and impacted tundra-covered terrain, and a postcrash fire consumed most of the wreckage. The Cessna 207’s right wing was damaged during the collision and the subsequent forced landing on tundra-covered terrain. Both airplanes were based at the Bethel Airport, Bethel, Alaska, and were returning to Bethel at the time of the collision. The Cessna 208B departed from the Toksook Bay Airport, Toksook Bay, Alaska, about 1325, and the Cessna 207 departed from the Tununak Airport, Tununak, Alaska. During separate telephone conversations with the National Transportation Safety Board (NTSB) investigator-in-charge on September 2, the chief pilot for Ryan Air, as well as the director of operations for Grant Aviation, independently reported that both pilots had a close personal relationship. During an initial interview with the NTSB IIC on September 3, in Bethel, the pilot of the Cessna 207 reported that both airplanes departed from the neighboring Alaskan villages about the same time and that both airplanes were en route to Bethel along similar flight routes. She said that, just after takeoff from Tununak, she talked with the pilot of the Cessna 208B on a prearranged, discreet radio frequency, and the two agreed to meet up in-flight for the flight back to Bethel. She said that, while her airplane was in level cruise flight at 1,200 feet above mean sea level (msl), the pilot of the Cessna 208B flew his airplane along the left side of her airplane, and they continued to talk via radio. She said that the pilot of the Cessna 208B then unexpectedly and unannounced climbed his airplane above and over the top of her airplane. She said that she immediately told the pilot of the Cessna 208B that she could not see him and that she was concerned about where he was. She said that the Cessna 208B pilot then said, in part: "Whatever you do, don't pitch up." The next thing she recalled was moments later seeing the wings and cockpit of the descending Cessna 208B pass by the right the side of her airplane, which was instantaneously followed by an impact with her airplane’s right wing. The Cessna 207 pilot reported that, after the impact, while she struggled to maintain control of her airplane, she saw the Cessna 208B pass underneath her airplane from right-to-left, and it began a gradual descent, which steepened as the airplane continued to the left and away from her airplane. She said that she told the pilot of the Cessna 208B that she thought she was going to crash.She said that the pilot of the Cessna 208B simply stated, “Me too.” She said that she watched as the Cessna 208B continued to descend, and then it entered a steep, vertical, nose-down descent before it collided with the tundra-covered terrain below. She said that a postcrash fire started instantaneously upon impact. Unable to maintain level cruise flight and with limited roll control, the Cessna 207 pilot selected an area of rolling, tundra-covered terrain as a forced landing site. During touchdown, the airplane’s nosewheel collapsed, and the airplane nosed down. The Cessna 207’s forced landing site was about 2 miles east of the Cessna 208B’s accident site.
Final Report:

Crash of a Cessna 208B Grand Caravan near Nightmute: 1 killed

Date & Time: Sep 2, 2011 at 1335 LT
Type of aircraft:
Operator:
Registration:
N207DR
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Toksook Bay - Bethel
MSN:
208B-0859
YOM:
2000
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3719
Captain / Total hours on type:
875.00
Aircraft flight hours:
8483
Circumstances:
A Cessna 208B and a Cessna 207 collided in flight in daylight visual meteorological conditions. The Cessna 208B and the Cessna 207 were both traveling in an easterly direction. According to the Cessna 207 pilot, the airplanes departed from two neighboring remote Alaskan villages about the same time, and both airplanes were flying along similar flight routes. While en route, the Cessna 207 pilot talked with the Cessna 208B pilot on a prearranged, discreet radio frequency, and the two agreed to meet up in flight for the return to their home airport. The Cessna 207 pilot said that the pilot of the Cessna 208B flew his airplane along the left side of her airplane while she was in level cruise flight at 1,200 feet mean sea level and that they continued to talk via the radio. Then, unexpectedly and unannounced, the pilot of the Cessna 208B maneuvered his airplane above and over the top of her airplane. She said that she immediately told the Cessna 208B pilot that she could not see him and that she was concerned about where he was. She said that the Cessna 208B pilot then said, in part: "Whatever you do, don't pitch up." The next thing she recalled was seeing the wings and cockpit of the descending Cessna 208B pass by the right side of her airplane, which was instantly followed by an impact with her airplane's right wing. She said that after the collision, the Cessna 208B passed underneath her airplane from right-to-left before beginning a gradual descent that steepened as the airplane continued to the left. It then entered a steep, vertical, nose-down descent before colliding with the tundra-covered terrain below followed by a postcrash fire. Unable to maintain level cruise flight, the Cessna 207 pilot selected an area of rolling, tundra-covered terrain as a forced landing site. An examination of both airplanes revealed impact signatures consistent with the Cessna 208B's vertical stabilizer impacting the Cessna 207's right wing. A portion of crushed and distorted wreckage, identified as part of the Cessna 208B's vertical stabilizer assembly, was found embedded in the Cessna 207's right wing. The Cessna 208B's severed vertical stabilizer and rudder were found about 1,000 feet west of the Cessna 208B's crash site.
Probable cause:
The pilot's failure to maintain adequate clearance while performing an unexpected and unannounced abrupt maneuver, resulting in a midair collision between the two airplanes.
Final Report:

Crash of an Antonov AN-2 near Choigan-Khole Lake: 1 killed

Date & Time: Aug 22, 2011
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Petropavlovka - Toora-Khem
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The single engine aircraft was performing an on-demand flight from Petropavlovka to Toora-Khem with seven fishermen and a pilot who want to go to a remote fish camp located in the natural reserve of Azas. While flying at low altitude, the aircraft went out of control and crashed on the shore of the Choigan-Khole Lake, near the Sorug River. While all seven passengers escaped with minor injuries, the pilot was killed. It appears that the aircraft was not registered and did not have any certificate of airworthiness. Therefore, the flight was considered as illegal and no flight plan was filed.

Crash of a Piaggio P.166S Albatross near Tzaneen: 6 killed

Date & Time: Aug 14, 2011 at 1030 LT
Type of aircraft:
Registration:
ZS-NJX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Tzaneen - Johannesburg
MSN:
446
YOM:
1973
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
4286
Aircraft flight hours:
6180
Circumstances:
Two aircraft, ZS-NJX and ZU-MMI, with 6 and 7 people on board respectively, took off from Tzaneen aerodrome (FATZ) on 14 August 2011 at approximately 0820Z, engaged in private flights with the intention of landing at Rand Airport (FAGM) on the same day. As both aircraft had not arrived at Rand Airport at their expected time of arrival, numerous attempts were made to contact the aircraft and these were unsuccessful. The search and rescue mission was initiated to try and locate these aircraft. The search and rescue mission was based around the area where the aircraft were believed to have had last contact with each other and with other traffic. Unfortunately due to bad weather in and around the area of last contact of these aircraft, they could only be located approximately two days after they had collided with a mountain in the Lekgalametse valley. Both aircraft were destroyed by post-impact fire and all the occupants of both aircraft were fatally injured.
Probable cause:
The accident was the consequence of a controlled flight into terrain.
Contributory factors:
- Lack of proper flight planning,
- Low Clouds.
Final Report:

Crash of a Piaggio P.166S Albatross near Tzaneen: 7 killed

Date & Time: Aug 14, 2011 at 1030 LT
Type of aircraft:
Operator:
Registration:
ZU-MMI
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Tzaneen - Johannesburg
MSN:
462
YOM:
1973
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
2893
Aircraft flight hours:
4501
Circumstances:
Two aircraft, ZS-NJX and ZU-MMI, with 6 and 7 people on board respectively, took off from Tzaneen aerodrome (FATZ) on 14 August 2011 at approximately 0820Z, engaged in private flights with the intention of landing at Rand Airport (FAGM) on the same day. As both aircraft had not arrived at Rand Airport at their expected time of arrival, numerous attempts were made to contact the aircraft and these were unsuccessful. The search and rescue mission was initiated to try and locate these aircraft. The search and rescue mission was based around the area where the aircraft were believed to have had last contact with each other and with other traffic. Unfortunately due to bad weather in and around the area of last contact of these aircraft, they could only be located approximately two days after they had collided with a mountain in the Lekgalametse valley. Both aircraft were destroyed by post-impact fire and all the occupants of both aircraft were fatally injured.
Probable cause:
The accident was the consequence of a controlled flight into terrain.
Contributory factors:
- Lack of proper flight planning,
- Low Clouds.
Final Report:

Crash of a Cessna 207 Skywagon near McGrath: 2 killed

Date & Time: Aug 13, 2011 at 1940 LT
Operator:
Registration:
N91099
Flight Phase:
Survivors:
Yes
Site:
Schedule:
McGrath - Anvik - Aniak
MSN:
207-0073
YOM:
1969
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
25000
Captain / Total hours on type:
10000.00
Aircraft flight hours:
31618
Circumstances:
The commercial pilot departed with five passengers on an on-demand air taxi flight between two remote Alaskan villages separated by mountainous terrain. When the airplane did not reach its destination, the operator reported the airplane overdue. After an extensive search, the airplane's wreckage was discovered in an area of steep, tree-covered terrain, about 1,720 feet msl, along the pilot's anticipated flight path. The flight was conducted under visual flight rules, but weather conditions in the area were reported as low ceilings and reduced visibility due to rain, fog, and mist. There is no record that the pilot obtained a weather briefing before departing. According to a passenger who was seated in the front, right seat, next to the pilot, about 20 minutes after departure, as the flight progressed into mountainous terrain, low clouds, rain and fog restricted the visibility. At one point, the pilot told the passenger, in part: "This is getting pretty bad." The pilot then descended and flew the airplane very close to the ground, then climbed the airplane, and then descended again. Moments later, the airplane entered "whiteout conditions," according to the passenger. The next thing the passenger recalled was looking out the front windscreen and, just before impact, seeing the mountainside suddenly appear out of the fog. A postaccident examination did not reveal any evidence of a mechanical malfunction. A weather study identified instrument meteorological conditions in the area at the time of the accident. Given the lack of mechanical deficiencies with the airplane and the passenger's account of the accident, it is likely that the pilot flew into instrument meteorological conditions while en route to his destination, and subsequently collided with mountainous terrain.
Probable cause:
The pilot's decision to continue visual flight rules flight into instrument meteorological conditions, which resulted in an in-flight collision with mountainous terrain.
Final Report:

Crash of an Antonov AN-12AP near Omsukchan: 11 killed

Date & Time: Aug 9, 2011 at 1532 LT
Type of aircraft:
Operator:
Registration:
RA-11125
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Komsomolsk-on-Amur – Magadan – Keperveyem
MSN:
3 3 410 06
YOM:
1963
Flight number:
LN9209
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
15297
Captain / Total hours on type:
6263.00
Copilot / Total flying hours:
3939
Copilot / Total hours on type:
3838
Aircraft flight hours:
18709
Aircraft flight cycles:
9172
Circumstances:
The four engine aircraft departed Komsomolsk-on-Amur Airport on a cargo service (flight LN9209) to Keperveyem with an intermediate stop in Magadan, carrying 17,43 tons of various goods, two passengers and a crew of nine. The aircraft departed Komsomolsk-on-Amur Airport at 1437LT. At 1520LT, while cruising at an altitude of 7,500 metres about 430 km northeast from his departure point, the crew informed ATC about a fuel leak on the engine n°1, requested a descent to 6,600 metres then the clearance to return to Komsomolsk-on-Amur. After the engine n°1 caught fire, the crew declared an emergency and started an emergency descent. Out of control, the aircraft crashed on the slope of a mountain located about 82 km southwest from Omsukchan. The aircraft disintegrated on impact and the debris were found a day later at an altitude of 1,006 metres. All 11 occupants were killed. This Antonov AN-12 was the oldest model still in commercial service in Russia.
Probable cause:
The probable causes of the crash were:
Following the inflight shut down of engine number one and feathering of the number one propeller the longitudinal (roll) control of the aircraft was lost due to load-bearing properties of the left wing and possible damage to the left hand aileron control wiring resulting in the aircraft's uncontrolled excessive roll to the left and subsequent impact with terrain. The fire started in the tail section of the #1 engine nacelle and spread forward and onto the wing. The fire was most likely fed by fuel leaking from a fuel line connection to the low pressure fuel pump at engine #1, the fuel most likely ignited due to contact with hot engine parts. Due to the disintegration of the aircraft and fire damage it was not possible to establish the location of fuel leaks and the cause with certainty. The inability of the fire suppression system to extinguish such a fire in its early stages as well as the lack of checklists/guidelines in the aircraft's flight manual for fuel leaks inside the engine nacelle contributed to the delay of more than 2 minutes to shut the engine down. The mountainous terrain underneath the aircraft, low level overcast cloud and lack of time due to continued fire did not permit the crew to select a proper site for an emergency landing.
Final Report: