Charter/Taxi (Non Scheduled Revenue Flight)

Following an uneventful flight from Moanda, Gabon, the crew initiated the approach in poor weather conditions (rain falls, strong crosswinds and turbulences). After touchdown, the twin engine aircraft skidded then veered off runway to the left. While contacting soft ground, the landing gear collapsed and the left engine was partially torn off. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair. Wind shear conditions are suspected.

After landing on runway 36 at Talcha Airport, the single engine aircraft veered off runway, went down an embankment and came to rest against a house down the runway. All 12 occupants escaped uninjured while the aircraft was damaged beyond repair. Downdrafts on final approach were reported, and the aircraft seemed to be unstable prior to landing.

During climb to cruise, the captain increased left engine power and the engine power lever became jammed in the full forward position. This condition resulted in an engine overtorque and overtemperture condition, and the captain shut down the left engine. After the engine shutdown, both primary flight display screens went blank. The captain reset the right generator and the flight displays regained power and display. Due to the engine shutdown, the captain diverted to a nearby airport and attempted a single-engine precautionary landing in visual flight rules conditions. Based on wind conditions at the airport (290 degrees at 18 knots), runway 27 was being used for operations. During the descent, the crew became confused as to their true heading and were only able to identify runway 27 about a minute before touching down due to a 50-degree difference in heading indications displayed to the crew as a result of the instrument gyros having been reset. Accurate heading information would have been available to the crew had they referenced the airplane’s compass. Having declared an emergency, the crew was cleared to land on any runway and chose to land on runway 18. After touchdown, the captain applied reverse thrust on the right engine and the airplane veered to the right. The airplane flight manual’s single-engine approach and landing checklist indicates that after landing braking and reverse thrust are to be used as required to maintain airplane control. The airplane continued to the right, departed the runway surface, impacted terrain, flipped over, and came to rest inverted. At the point of touchdown, there was about 5,000 feet of runway remaining for the landing roll. The loss of directional control was likely initiated when the captain applied reverse thrust shortly after touchdown, and was likely aggravated by the strong crosswind. Postaccident examination of the airplane showed a clevis pin incorrectly installed by unknown maintenance personnel that resulted in a jammed left engine power lever. No additional anomalies were noted with the airplane or engines that would have precluded normal operation.

Shortly after takeoff from Shabunda Airport, the crew reported engine problems and elected to return. After touchdown, the twin engine airplane was unable to stop within the remaining distance, overran and came to rest against an embankment. All 16 passengers escaped unhurt while both pilots were injured. The aircraft was damaged beyond repair. The exact date of the mishap remains unknown, somewhere during October 2011.

The twin engine aircraft departed Nairobi-Wilson Airport in the morning for a flight to Marsabit and Lodwar, carrying exam documents. While returning to Wilson Airport in the afternoon, the airplane went out of control and crashed in an open field located about 15 km west of Wilson Airport. The pilot and a passenger were killed while the second passenger was seriously injured. The aircraft was destroyed.

Shortly after takeoff from Xakanaka Airstrip on a taxi flight to the Pom Pom Camp located in the Okavango Delta, the single aircraft lost height and crashed, bursting into flames. The pilot and seven passengers were killed while four others were injured. The pilot was a British citizen as the seven passengers killed were respectively four Swedish, on British and two French. The aircraft was totally destroyed by a post crash fire. For unknown reasons, the aircraft caught fire shortly after takeoff.

The pilot stated that after landing, the nose landing gear collapsed. Examination of the airplane nose strut down-lock installation revealed that the strut on the right side of the nose landing gear trunnion was installed incorrectly; the strut installed on the right was a left-sided strut. Incorrect installation of the strut could result in the bearing pulling loose from the pin on the right side of the trunnion, which could allow the nose landing gear to collapse. A review of maintenance records revealed recent maintenance activity on the nose gear involving the strut. The design of the strut is common for the left and right. Both struts have the same base part number, and a distinguishing numerical suffix is added for left side and right side strut determination. If correctly installed, the numbers should be oriented facing outboard. The original MU-2 Maintenance Manual did not address the installation or correct orientation of the strut. The manufacturer issued MU-2 Service Bulletin (SB) No. 200B, dated June 24, 1994, to address the orientation and adjustment. Service Bulletin 200B states on page 8 of 10 that the “Part Number may be visible in this (the) area from the out board sides (Inked P/N may be faded out).”

The aircraft was performing a special flight with tourists above the Himalayan mountains and especially a tour of the Everest in the early morning. While returning to Kathmandu-Tribhuvan Airport, the copilot (PIC) was cleared to descend to 6,000 feet for a landing on runway 02. In marginal weather conditions, he passed below 6,000 feet until the aircraft contacted trees and crashed in hilly and wooded terrain located near the village of Bishanku Narayan, some 6,7 km southeast of the airport. The aircraft was destroyed by impact forces and a post crash fire. A passenger was seriously injured while 18 other occupants were killed. Few hours later, the only survivor died from his injuries. The 16 tourists were respectively 10 Indians, 2 Americans, 1 Japanese and 3 Nepalese.

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°.

The aircraft was chartered by the Lokomotiv Yaroslavl ice hockey team to carry his staff to Minsk to take part to the first game of the Russian 2011-2012 championship. During the takeoff roll from runway 23 at Yaroslavl-Tunoshna Airport, the crew selected flaps down at 20° and the stabilizer in a nose-up position of 8,7°. The aircraft slowly accelerated to 165 km/h due to a residual pressure on the brake pedal. At a speed of 185 km/h and at a distance of 1,350 metres from the runway end, the nose gear lifted off. But the aircraft continued, passed the runway end and rolled for about 400 metres before it took off. Then it collided with various approach lights and the localizer antenna, lost height and eventually crashed on the shore of the Volga River, bursting into flames, 2 minutes after the takeoff roll was initiated. A passenger and the flight engineer were seriously injured while 43 other occupants were killed. Almost a week later, the passenger died from his injuries. Among the passengers were 26 players from the Lokomotiv Yaroslavl ice hockey team, Russian citizens and also Canadian, Czech, Ukrainian, German and Slovak. The Canadian coach Brad McCrimmon, his both assistants, the cameraman, three masseurs, one admin and two doctors were among the victims.