De Havilland DHC-6 Twin Otter

Randigo

Tara Air

The twin engine airplane departed Pokhara City Airport Runway 04 at 0955LT on a schedule service to Jomsom, carrying 19 passengers and three crew members. After takeoff, the pilot initiated a turn to the left and continued to climb to 12,000 feet (calibrated altitude) when a turn was initiated to the right. In limited visibility, the aircraft impacted the slope of a rocky mountain located in the area of Shikha, some 14 km southwest from the Annapurna Mountain. The wreckage was found the following day. The aircraft disintegrated on impact and all 22 occupants were killed.

Caverton Helicopters

The twin engine airplane departed Yaoundé at 1246LT on a charter flight to Dompta and Belabo, carrying 9 employees of the Cameroon Oil Transportation Company (COTCO) and two crew members. En route, the airplane crashed in unknown circumstances near the village of Nanga Eboko. All 11 occupants were killed.

Rimbun Air

On 15 September 2021, a DHC-6-300 (Twin Otter) aircraft registered PK-OTW was being operated for an unscheduled cargo flight from Douw Aturure Airport (WABI), Nabire, Papua to Bilorai Airport (WAYB), Intan Jaya, Papua. The aircraft was operated by two pilots accompanied by one engineer on board. The filed flight plan for the flight indicated that the aircraft would be operated under Visual Flight Rule (VFR) with fuel endurance of 2 hours 30 minutes. The estimate time departure for the flight was at 0640 LT. At 0610 LT, the pilot received weather observation report from the Bilorai aeronautical communication officer (ACO) that the visibility was 5 up to 7 kilometers, several clouds over the airport and all final areas were clear. About 7 minutes later, the ACO updated the observation report which indicated that the visibility changed to 7 up to 8 kilometers (km). After the cargo loading process and the flight preparation had completed, the aircraft taxied to Runway 16. At 0644 LT, the aircraft departed and climbed to the cruising altitude of 9,500 feet. Prior to the departure, there was no record or report of aircraft system malfunction. The Pilot in Command (PIC) acted as Pilot Monitoring (PM) while the Second in Command (SIC) acted as Pilot Flying (PF). At 0658 LT, the PK-OTW pilot reported to the Nabire air traffic control that the aircraft was at 25 Nm with altitude of 9,500 feet. At 0702 LT, the SIC asked the PIC to have the aircraft control as PF. During flight, the PK-OTW pilots monitored weather information provided by the pilots of two other aircraft that flew ahead of the PK-OTW to Bilorai. Both pilots monitored that the first aircraft (Cessna 208B EX) landed using Runway 27 while the second aircraft (Cessna 208B) would use Runway 09. At 0715 LT, the PIC advised the SIC to use the Runway 27 for landing. At 0719 LT, the SIC made initial contact with the ACO and advised that the aircraft was approaching Bilai at altitude of 9,500 feet and the estimate time arrival at Bilorai was 0726 LT. The ACO acknowledged the pilot report and provided current weather observation as follows “…wind westerly 3 until 5 knots, final 09 open with broken fog and final 27 open, visibility 5 until 7 km, blue sky overhead”. The SIC acknowledged the weather information and advised the ACO would report when the aircraft position was on left downwind Runway 27. At 0721 LT, the SIC read the descent checklist included the item of Landing Data/Approach Briefing and was replied by completed. The Cockpit Voice Recorder (CVR) did not record any pilot’s discussion regarding to the airport minimum safe altitude since the beginning of the recording. At 0723 LT, a pilot of DHC-6-400 aircraft registered PK-OTJ, asked the PK-OTW pilot of the weather condition in Bilorai. The PK-OTJ flew behind the PK-OTW with from Nabire to Bilorai. The SIC then responded that the PK-OTW was on descend and would fly through clouds about 5 Nm to Bilorai. Thereafter, the ACO provided traffic information to PK-OTW pilot that there was an aircraft (Cessna 208B aircraft) on final Runway 09. The PIC who acted as PF acknowledged the traffic information and advised to the ACO that the PK-OTW would join left downwind Runway 27 for the landing approach. At 0725 LT, the SIC advised to the ACO that the aircraft was on left downwind Runway 27. The ACO then advised the PK-OTW pilot to report when on final Runway 27. At 07:26:12 LT, a stall warning recorded in the Cockpit Voice Recorder (CVR) then the PIC asked to the SIC to check the aircraft speed. The SIC responded the aircraft speed was 65 knots. At 07:26:16 LT, the PIC asked to the SIC to advise the ACO that they were making a go around. The SIC then advised the ACO that the PK-OTW was making a go around and was responded to report when on final. The CVR did not record pilot’s discussion about the plan maneuver of the go around. At 07:26:45 LT, the PIC informed that they were making a go around to the PK-OTJ pilot. The PK-OTJ pilot responded that the aircraft was approaching Homeyo and would reduce the speed to make enough separation with the PK-OTW. The PIC then advised the PK-OTJ that the PK-OTW would attempt to land using Runway 09. Based on the data transmitted from the flight following system, at 07:27:57 LT, the aircraft was about 3 Nm outbound from Bilorai on direction of 238°. At 07:28:22 LT, the PK-OTJ pilot advised to the ACO that the aircraft was about 6 nm to Bilai and the pilot intended to make holding maneuver over Bilai to make enough separation with the PK-OTW. At 07:28:33 LT, the SIC advised the PIC that the aircraft was at 8,200 feet and was responded that the PIC initiated turning the aircraft. A few second later, the SIC advised to the PIC that the aircraft was turning, and the aircraft was at 3.2 Nm outbound from Bilorai. At 07:28:38 LT, the last data of the flight following system recorded that the aircraft was on direction of 110°. At 07:29:25 LT, the SIC advised the PIC to fly left. Thereafter, the SIC advised the PIC that the aircraft was passing 8,000 feet. At 07:29:35 LTC, the PIC asked to the SIC about the distance to Bilorai and was responded 2.5 Nm. The SIC, reminded the PIC to fly left as the aircraft flew too close to the terrain. At 07:29:49 LT, the CVR recorded the first impact sound and the CVR recording stopped at 07:29:55 LT. At 0730 LT, the ACO asked the PK-OTW pilot intention as the aircraft was not visible from the ACO working position, and the pilot did not respond the ACO. At about the same time, the ACO heard impact sound that was predicted coming from terrain area on west of Bilorai. The ACO then called the PK-OTW pilot several times without response. Several pilots also attempted to contact the PK-OTW with the same result. The PK-OTW was found on a ridge at elevation of 8,100 feet, about 2 Nm on bearing 260° from Bilorai.

Rimbun Air

The twin engine airplane departed Timika Airport at 1036LT on a cargo flight to Ilaga, carrying one passenger, a crew of four and a load of 1,7 ton of rice. At 1054LT, the crew gave his ETA at Ilaga Airport when the contact was lost about six minutes later. As the airplane failed to arrive at destination, SAR operations were initiated. The wreckage was found four days later in a mountainous terrain, at an altitude of 4,115 meters, about 10 km from Kampung Mamontoga. The aircraft was totally destroyed and all four occupants were killed.

Ethiopian Airlines

The twin engine airplane departed Dire Dawa in the morning on a flight to Harar Meda Airbase located in Debre Zeit, carrying 15 Army officers and three civilians on behalf of the Ethiopian Army. While descending to Harar Meda, the airplane crashed in unknown circumstances in a wooded area located in Mojo, some 17 km southeast of the airfield. The aircraft was totally destroyed and all 18 occupants were killed, among them two children. Operated on behalf of the Ethiopian Army with dual registration ET-AIU/808.

Perris Valley Aviation

The pilot of the twin-engine, turbine-powered airplane reported that, while providing flights for skydivers throughout the day, he had a potential new hire pilot flying with him in the right seat. He added that, on the eighth flight of the day, the new pilot was flying during the approach and "approximately 200 feet south from the threshold of [runway] 15 at approximately 15 feet AGL [above ground level] the bottom violently and unexpectedly dropped out. [He] believe[d] some kind of wind shear caused the aircraft [to] slam onto [the] runway and bounce into the air at a 45 to 60-degree bank angle to the right." The prospective pilot then said, "you got it." The pilot took control of the airplane and initiated a go-around by increasing power, which aggravated the "off runway heading." The right wing contacted the ground, the airplane exited the runway to the right and impacted a fuel truck, and the right wing separated from the airplane. The impact caused the pilot to unintentionally add max power, and the airplane, with only the left engine functioning, ground looped to the right, coming to rest nose down.

Skydive San Marcos

The pilot reported that he was landing in gusty crosswind conditions following a parachute jump flight, and that the gusty conditions had persisted for the previous 10 skydiving flights that day. The pilot further reported that during the landing roll, when the nose wheel touched down, the airplane became "unstable" and veered to the left. He reported that he applied right rudder and added power to abort the landing, but the airplane departed the runway to the left and the left wing impacted a tree. The airplane spun 180 degrees to the left and came to rest after the impact with the tree. The left wing was substantially damaged. The pilot did not report any mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Tara Air

As per the flight plan submitted on 23rd February 2016, the aircraft was scheduled for VFR flight to Jomsom (VNJS) on 24th February with estimated off-block time of 01:00, intended cruising speed of 150 knots, intended level of 10,500 ft and via direct track. The first and second alternate aerodromes were Bhairahawa (VNBW) and Pokhara (VNPK) respectively and estimated elapsed time was 20 minutes with the fuel endurance of 2 hours and 30 minute. Based on the information from the CVR, FDR and ATC records, the following description of the history of the flight was reconstructed: At 01:55, the first-officer contacted Pokhara tower requesting Jomsom and Bhairahawa weather. Upon receiving Jomsom weather which was 8 km visibility towards Lete (arrival track) and foothill partially visible; at 01:56 F/O requested start-up for Jomsom. First-officer then briefed the weather to the captain, in response to this the captain responded by saying 'Let‘s have a look, if not possible we will return' (Translated from Nepali conversation). While performing the 'before start checklist', they received weather of Bhairahawa as closed. After completing the checklist and start-up the first-officer at 02:00 requested taxi clearance. The ATC informed runway change to 22 instead of runway 04 and gave taxi clearance. At 02:03 while taxiing the captain considering bad weather condition expressed his concern over the runway change with F/O but failed to express it to the ATC. As briefed by captain earlier, the control was transferred to F/O and at 02:04 F/O made a normal take-off. At 02:08 the captain reported 5 miles at 6,200 ft to ATC. At 02:09, while passing through 7,000 ft the captain informed the actual weather, which was light haze, mountain not visible but had ground contact, to an ultra-light aircraft upon his request. As per the cockpit conversation, the crew were comparing the base of the cloud which was higher than the day before and proposed to continue climb to 12,500 ft if not on-top of the cloud at 10,500 ft. Around 5 miles before Ghorepani passing 10,100 ft, the captain told that cells were still present so advised F/O to continue climb to 12,000 ft and told that they will proceed till TATOPANI and decide to continue or divert. At 02:14 approaching GHOREPANI and passing 11,400 ft, Captain told F/O to maintain level to be in between the cloud layers and briefed F/O that if they had to divert it would be a left turn. At the same time captain asked repeatedly to F/O if his side was raining for which F/O told and confirmed not visual, after which captain told they would see and decide (regarding continuation of flight). At 02:14:50 while over Ghorepani area at 11,500 ft the EGPWS TERRAIN alert and at 02:14:52 PULL UP warning came while they were not visual and at 02:15:01 it was stated that they were visual and by 02:14:53 the warning stopped. At 02:15 while maintaining 11,500 ft the captain reported ATC that they are at Ghorepani at level 10,500 ft after which frequency changeover to Jomsom tower was given. At 02:15:27 the captain instructed F/O to maintain heading of 3300 and flight level just below the cloud, after which a shallow descent was initiated. At this time captain asked F/O if his side was visual, in response F/O replied somewhat visual. The Captain then instructed F/O to descent to 10,000 ft. Once the descent was started at 02:15:55 passing 11,000 ft an OVERSPEED warning sounded in the cockpit for 2 seconds as the speed reached 152 knots. At 02:16 while passing 10,700 ft captain advised F/O to make a left turn so that it would be easy to turn if required as he was able to see his side. Then F/O asked if left side was visual for which the captain informed that not that side (towards the track) but somewhat visual to the left of him and told that the TRACK TO GO was TO THE LEFT whereas they were actually left of the track and had descended to 10,300 ft. At 02:17:58 EGPWS TERRAIN alert sounded when the aircraft was at 10,200 ft and descending on heading of 3210 with right bank angle of around 30 . At 02:18:06 when the aircraft had descended to 10,100 ft the PULL UP WARNING sounded for which the captain said not to worry and at 02:18:12; when the aircraft was at 10,000 ft the captain took-over the control, continued descent and asked F/O if his side was visual. The F/O informed that right side was not visual at all by which the aircraft had continued shallow descent on heading 3250 with right bank angle reaching up to 130 at 2:18:19 and by 02:18:23 the aircraft once again returned back to 0° bank angle. At 02:18:23 the captain started left bank followed by right bank again while still on a shallow descent until 02:18:27.Upon reaching 9,850 ft (lowest altitude) the aircraft started very shallow climb. At 02:18:35 when aircraft was 9,920 ft the captain told F/O that they reached Landslide (a checkpoint which is on track to Jomsom on the right side of the Kali-Gandaki River). At 02:18:44 when aircraft reached 10,150 ft captain told <U+2015>what I will do is now I will turn to heading of LETTE<U+2016> (another way point on route to Jomsom); while the PULL-UP warning was continuously sounding. At 02:18:49 when the aircraft was at 10,300 ft right bank angle increased up to 16° with pitch up attitude of 7°. At 02:18:52 the captain told that he would start climb when the aircraft had reached 10,350 ft; pitch attitude of 10° and still on right bank. The aircraft reached zero degree bank at 02:18:53 and started shallow left bank with pitch attitude of 12° nose up. By 02:18:57 the bank angle reached 200 left with pitch attitude of 11.8 and altitude of 10,550 ft and captain was still questioning F/O about the visibility towards his side but F/O informed his side not visible completely. The last data recorded in FDR was at 02:19:03 when the altitude had reached around 10,700 ft; pitch attitude of 7° nose up and left bank angle of 25° heading of 335° with EGPWS PULL-UP warning ON.

Aviastar Mandiri

On 2 October 2015, a DHC-6 Twin Otter, registered PK-BRM, was being operated by PT. Aviastar Mandiri as a scheduled passenger flight with flight number MV 7503. The aircraft departed from Andi Jemma Airport, Masamba (WAFM)1 with the intended destination of Sultan Hasanuddin International Airport, Makassar (WAAA) South Sulawesi, Indonesia. On board the flight were 10 persons consisting of two pilots and eight passengers, including one company engineer. The previous flights were from Makassar – Tana Toraja – Makassar – Masamba – Seko - Masamba and the accident flight was from Masamba to Makassar which was the 6th sector of the day. The aircraft departed from Masamba at 1425 LT (0625 UTC2 ) with an estimated time of arrival at Makassar of 0739 UTC. The Pilot in Command (PIC) acted as Pilot Flying (PF) while the Second in Command (SIC) acted as Pilot Monitoring (PM). The flight was conducted under the Visual Flight Rules (VFR) and cruised at an altitude of 8,000 feet. At 0630 UTC, the pilot reported to Ujung Pandang Information officer that the aircraft passed an altitude of 4,500 feet and was climbing to 8,000 feet. The Ujung Pandang Information officer requested the pilot of the estimate time of aircraft position at 60 Nm out from MKS VOR/DME. At 0632 UTC, the pilot discussed about the calculation of estimate time to reach 60 Nm out from MKS and afterward the pilot informed Ujung Pandang Information officer that the estimate at 60 Nm was at 0715 UTC. At 0633 UTC, the Ujung Pandang Information officer informed the pilot to call when reaching 8,000 feet and was acknowledged by the pilot. At 0636 UTC, the pilot informed the Ujung Pandang Information officer that the aircraft had reached 8,000 feet and requested the squawk number (ATC transponder code). The Ujung Pandang Information officer acknowledged and gave the squawk number of A5616, which was acknowledged by the pilot. At 0637 UTC, the pilots discussed to fly direct to BARRU. BARRU is a town located at about 45 Nm north of Makassar. Both pilots agreed to fly direct and the SIC explained the experience of flying direct on the flight before. At 0651 UTC, the PIC told the SIC that he wanted to climb and one second later the CVR recorded the sound of impact.

Skydive Dubai

Following an uneventful skydiving mission over the Dubai Drop Zone, the pilot was returning to his base. Upon landing on runway 06, the twin engine aircraft went out of control, veered off runway to the left, struck an embankment and came to rest with the right wing torn off. The pilot was uninjured and the aircraft was damaged beyond repair.

Rampart Aviation

The airline transport pilot was conducting a cross-country aerial observation flight in the multiengine airplane. The pilot reported that the airplane was on the final leg of the traffic pattern when he reduced the power levers for landing and noticed that the right engine sounded like the propeller was moving toward the beta position. The pilot increased the engine power, and the sound stopped. As the airplane got closer to the runway, he decreased the engine power, and the sound returned. In addition, the airplane began to yaw right. The pilot applied left aileron and rudder inputs to remain above the runway centerline without success. While over the runway, the pilot reduced the engine power to idle, and the airplane continued to yaw right. The pilot applied full power in an attempt to perform a go-around; however, the airplane yawed about 30 degrees off the runway centerline, touched down in the grass, and impacted trees before coming to rest. The right wing, right engine, and right propeller assembly were impact-separated. The right engine propeller came to rest about 50 ft forward of the main wreckage, and it was found in the feathered position. A review of maintenance records revealed that the right propeller had been overhauled and reinstalled on the airplane 2 days before the accident and had operated 9 hours since that time. Subsequent testing of the right propeller governor revealed that it functioned without anomaly; however, the speed settings were improperly configured. Further, the testing revealed that the beta valve travel from the neutral position was out of tolerance. Although this could have let oil pressure port to one side of the spool or the other and, thus, changed the propeller blade angle, it could not be determined whether this occurred during the accident landing. Impact damage precluded examination of the right propeller governor control linkage; therefore, it could not be determined if it was inadequately installed or rigged, which could have resulted in the propeller moving into the beta position. The investigation could not determine why the right propeller moved toward the beta position as engine power was reduced, as reported the pilot.

Trans Maldivian Airways

Flight FLT371301, a Viking Air (De Havilland) DHC-6-300 aircraft with registration mark 8Q-MAN, crashed into the sea approximately 3 km southeast of Kuredu (KUR) at 1733 hrs on 2 July 2015. The aircraft was flying under visual flight rules (VFR) on a charter flight, carrying 11 passengers from Komandoo (KOM) to Kuredu (KUR). According to the operating crew, the aircraft was on final approach, northwest bound, to land at KUR. At approximately 400 feet, on selection of flaps to the fully down position, the aircraft pitched up and the aircraft was vibrating. The pilot flying (PF) could not control the aircraft and asked the PIC to take over the controls. The aircraft was in a nose-high attitude when the PIC took over the controls. The stall warning light illuminated. The PIC applied full left rudder, moved the control column forward and put the power levers to idle to recover the aircraft. The aircraft, however, did not respond to these actions. Flaps were then moved to the fully up position. The PIC was gaining some control at this stage but the aircraft continued turning right, losing height and impacted the sea before he could regain full control of the aircraft. On initial impact the left float detached. The aircraft then bounced and landed on the right float causing the right float to also detach from the aircraft. The right float was, however, trapped between the airframe and the engine for several minutes. With both floats detached from the aircraft and the right float still trapped between the airframe and engine, the aircraft stayed afloat until all passengers and crew evacuated. At the same time the aircraft started tilting left causing water to rush inside and started sinking. All 11 passengers and three crew were able to evacuate the aircraft without injury, before the aircraft completely sank. The accident was notified to the Aircraft Accident Investigation Committee (AICC) at 1750 hrs. Investigation began on the same day. Inspectors arrived at the scene at 2300 hrs, about five and a half hours after the accident occurred.

Hevilift

A DHC-6 Twin Otter aircraft was returning from Woitape, Central Province, to Jacksons Airport, Port Moresby on the morning of 20 September 2014 on a charter flight under the instrument flight rules (IFR). The weather at Woitape was reported to have been clear, but at Port Moresby the reported weather was low cloud and rain. Witnesses reported that the summit of Mt Lawes (1,700 ft above mean sea level (AMSL)) was in cloud all morning on the day of the accident. When the aircraft was 36 nm (67 km) from Port Moresby, air traffic control gave the flight crew a clearance to descend maintaining visual separation from terrain and to track to a left base position for runway 14 right (14R) at Jacksons Airport, Port Moresby. The clearance was accepted by the crew. When the aircraft was within 9.5 nm (17.5 km) of the airport, the pilot in command (PIC) contacted the control tower and said that they were “running into a bit of cloud” and that they “might as well pick up the ILS [instrument landing system] if it’s OK”. The flight crew could not have conducted an ILS approach from that position. They could have discontinued their visual approach and requested radar vectoring for an ILS approach. However, they did not do so. The Port Moresby Aerodrome Terminal Information Service (ATIS), current while the aircraft was approaching Port Moresby had been received by the flight crew. It required aircraft arriving at Port Moresby to conduct an ILS approach. The PIC’s last ILS proficiency check was almost 11 months before the accident flight. A 3-monthly currency on a particular instrument approach is required under PNG Civil Aviation Rule 61.807. It is likely the reason the PIC did not request a clearance to intercept the ILS from 30 nm (55.5 km) was that he did not meet the currency requirements and therefore was not authorized to fly an ILS approach. During the descent, although the PIC said to the copilot ‘we know where we are, keep it coming down’, it was evident from the recorded information that his assessment of their position was incorrect and that the descent should not have been continued. The PIC and copilot appeared to have lost situational awareness. The aircraft impacted terrain near the summit of Mt Lawes and was substantially damaged by impact forces. Both pilots and one passenger were fatally injured in the impact, and one passenger died on the day after the accident from injuries sustained during the accident. Of the five passengers who survived the accident, three were seriously injured and two received minor injuries. One of the fatally injured passengers was not wearing a seat belt.

Nepal Airlines

On 16 February 2014, the Twin Otter (DHC6/300) aircraft with registration number 9N-ABB, owned and operated by Nepal Airlines Corporation (NAC), departed Kathmandu at 0610 UTC (1155 LT) on its schedule flight to Jumla carrying 18 persons on board including 3 crews. Detailed sectors to be covered by the flight No. RA 183/718 was Kathmandu–Pokhara–Jumla-Nepalganj (Night stop). Flight from Kathmandu to Pokhara completed in normal condition. After 17 minutes on ground at Pokhara airport and refueling 9N-ABB departed Pokhara at 0658 for Jumla. After Jumla flight, the aircraft was scheduled to Night stop at Nepalganj. Next day it was to do a series of shuttle flights from Nepalganj. Prevailing westerly weather had a severe impact on most of the domestic flights since last two days. A.M.E. of Engineering Department of NAC who had performed D.I. of 9N ABB had mentioned in his written report to the Commission that he had reminded the diversion of Bhojpur flight of NAC due weather and asked the Captain whether he had weather briefing of the Western Nepal or not. In response to the AME's query the Captain had replied casually that- "weather is moving from west to east and now west is improving". Pilots behavior was reported normal by the ground staffs of Kathmandu and Pokhara airports prior to the commencement of flight on that day. All the pre and post departure procedure of the flight were completed in normal manner. Before departure to Jumla from Pokhara, Pilots obtained Jumla and Bhairahawa weather and seems to be encouraged with VFR Weather at both stations. However, they were unable to make proper assessment of en route weather. PIC decided to remain south of track to avoid the terrain and weather. CVR read out revealed that pilots were aware and concerned about the icing conditions due to low outside air temperature. After around 25 minutes, probably maneuvering to avoid weather, the PIC instructed the co-pilot to plan a route further south of their position, to fly through the Dang valley. The copilot selected Dang in the GPS, on a bearing of 283°, and determined the required altitude was 8500ft. He then raised concerns that the aircraft may not have enough fuel to reach the planned destination. Approximately two and a half minutes before the accident, the PIC initiated a descent, and the copilot advised against this. As per CVR read out, last heading recorded by copilot, approximately one minute before the crash, was 280. The last one minute was a very critical phase of the flight during which PIC said I am entering (perhaps inside the cloud). At that time copilot called Bhairahawa Tower on his own and got latest Bhairahawa weather. While copilot was transmitting its last position report to Bhairahawa Control Tower (approximately 25 miles from Bhairahawa), PIC interrupted and declared to divert Bhairahawa. Bhairahawa Control Tower wanted the pilots to confirm their present position. But crews were very much occupied and copilot said STANDBY. Just few seconds before crash copilot had told PIC not to descend. Copilot also suggested PIC in two occasions - sir don't turn. Very unfortunately aircraft was crashed. The aircraft disintegrated on impact and all 18 occupants were killed.

MASwings

A de Havilland Canada DHC-6 Twin Otter 310, operated by MASwings, sustained substantial damage in an accident at Kudat Airport (KUD), Malaysia. The copilot and one passenger died, four others were injured. MASwings flight MH3002 operated on a domestic flight from Kota Kinabalu Airport (BKI) to Kudat. The captain was the pilot flying for this sector and the first officer was pilot monitoring. As the aircraft was approaching Kudat Airfield, Kudat Tower reported the weather conditions to be: wind at 270 degrees at 17 kts gusting 31 kts. The aircraft continued the approach on runway 04 and leveled off at 500 feet with flaps set at 10°. At this point the crew noticed that the approach for runway 04 had a strong tail wind. This was evident from the indicated airspeed observed by the crew which indicated 100 kts where the airspeed for flaps 10° should be 65kts. The windsock also indicated a tail wind. Noticing the approach for runway 04 was a tail wind condition, the crew decided to go around at a height of 500ft. Maintaining runway heading, the crew initiated a go around climbing to 1,000ft making a left tear drop and reposition for runway 22. On the approach for runway 22 the captain informed the first officer that if they could not land they would return to Kota Kinabalu. The aircraft was aligned with the centerline of runway 22 and 20° flaps was set. The aircraft continued to descend to 300ft. At this point the wind appeared to be calm as the aircraft did not experience any turbulence and the captain told the first officer that he was committed to land. Upon reaching 200ft the captain called for the flaps to be lowered to full down. As they were about to flare the aircraft to land, approximately 20ft above the runway, the aircraft was suddenly hit by a gust of wind which caused the aircraft to veer to the right with the right wing low and left wing high and the nose was pointing 45° to the right of runway 22. The crew decided to go around by applying maximum power; however the aircraft did not manage to climb successfully. The flaps were not raised and were still in the full flaps down position as the crew thought the aircraft was still low hence the flaps were not raised. The aircraft continued to veer to the right with right wing low and managed to only climb at a shallow rate. The aircraft failed to clear the approaching trees ahead and was unable to continue its climb because the airspeed was reducing. The presence of a full flaps configuration made it more difficult for the aircraft to climb. As the aircraft was on full power on both the engines, it continued to fly almost perpendicularly in relation to the runway and at a low height above the ground. The aircraft hit a tree top at the airfield perimeter fencing, disappeared behind the row of trees, hit another tree behind a house. It hit the right rear roof of the house, ploughed through the roof top of the kitchen, toilet and dining area, hit the solid concrete pillars of the car garage and finally hit the lamp post just outside the house fence. It swung back onto the direction of the runway and came to rest on the ground with its left engine still running. A woman and her 11-year old son who were in the living room at the time escaped unhurt.

Nepal Airlines

The Twin Otter (DHC6/300) aircraft with registration number 9N-ABO, owned and operated by Nepal Airlines Corporation (NAC), departed Kathmandu to Pokhara for night stop on 15 May 2013 in order to accomplish up to 5 (five) Pokhara-Jomsom-Pokhara charter flights planned for the subsequent day on 16 May 2013. As per the programme, the aircraft completed first charter flight from Pokhara to Jomsom sector on 16 May 2013 morning after one and half hour waiting on ground due weather. For this second flight, the aircraft departed at 0225 UTC (08:10LT) from Pokhara to Jomsom in the command of Capt. Dipendra Pradhan and Mr. Suresh K.C. as co-pilot. There were 19 passengers including one infant and 3 crew members on board. The aircraft was operating under Visual Flight Rules (VFR). As per the CVR readout there was no reported difficulties and all the pre and post departure procedure and en-route portion of the flight were completed in normal manner. There was no indication of lacking of information and advice from Jomsom Tower. At first contact the co-pilot called Jomsom Tower and reported its position at PLATO (a compulsory reporting point) at 9 miles from Jomsom airport at 12500ft. AMSL. The Jomsom Tower advised runway 24 wind south westerly 08-12 KTS, QNH 1020, Temp 13 degree and advised to report downwind for runway 24.The co-pilot accepted by replying to join downwind for runway 24. There was no briefing and discussion between the two pilots regarding the tail wind at the airport. The PIC, then, took over the communication function from co-pilot and called Jomsom Tower, requesting to use runway 06 instead of runway 24, despite the advice of tower to use runway 24 to avoid tail wind effect in runway 06. Jomsom Tower repeated the wind speed to be 08-12 KTS for the runway 06, to which the PIC read back the wind and answered to have ”no problem”. As per the PIC request the Jomsom Tower designated runway 06 for landing and advised to report on final runway 06. The PIC did read back the same. The pre landing checklist was used, flaps with full fine in propeller rpm were taken and full flaps was also taken before touchdown. In the briefing of “missed approach” the PIC had answered to be “standard”. The aircraft touched down runway of Jomsom airport at 0245 UTC (08:30LT) at a distance of approximately 776 ft, far from the threshold of runway 06. After rolling 194 ft. in the runway, the aircraft left runway and entered grass area in the right side. The aircraft rolled around 705 ft in the grass area and entered the runway again. The maximum deviation from the runway edge was 19 ft. The Commission has observed that when aircraft touched down the runway, it was not heading in parallel to the runway centreline. After touchdown the aircraft rolled around 194ft on the runway, left the paved area and started rolling in the grass area in the right side. During the landing roll, when the aircraft was decelerating, the co-pilot had raised the flaps as per the existing practice of carrying out “after the landing “checks". As per the observation of passenger seated just behind the cockpit, after touchdown of the aircraft there was no communication between pilot and co-pilot. It seemed that pilot was busy in cockpit and facing problem. It was obvious that PIC was in dilemma in controlling aircraft. He added power to bring aircraft into the runway with an intention to lift up the aircraft. He did not brief anything to copilot about his intention and action. He started adding power with the intention of lifting up, but the aircraft was already losing its speed, due to extension of flaps by co-pilot without briefing to PIC and use of brakes (light or heavy, knowingly and unknowingly) simultaneously by the PIC. The accelerating aircraft with insufficient speed and lift to take off ran out of the runway 24 end, continued towards the river, hit the barbed fence and gabion wall with an initial impact and finally fell down into the edge of river. The left wing was rested in the mid of the river preventing the aircraft submerged into the river.

Lao Air

Shortly after takeoff from Sam Neua-Nathong Airport, while in initial climb, the twin engine aircraft collided with trees, lots height and crashed in a small river located 200 metres past the runway end. All 18 occupants were injured, five seriously. The aircraft was damaged beyond repair.

Kenn Borek Air

The aircraft departed South Pole Station, Antarctica, at 0523 Coordinated Universal Time on 23 January 2013 for a visual flight rules repositioning flight to Terra Nova Bay, Antarctica, with a crew of 3 on board. The aircraft failed to make its last radio check-in scheduled at 0827, and the flight was considered overdue. An emergency locator transmitter signal was detected in the vicinity of Mount Elizabeth, Antarctica, and a search and rescue effort was initiated. Extreme weather conditions hampered the search and rescue operation, preventing the search and rescue team from accessing the site for 2 days. Once on site, it was determined that the aircraft had impacted terrain and crew members of C-GKBC had not survived. Adverse weather, high altitude and the condition of the aircraft prevented the recovery of the crew and comprehensive examination of the aircraft. There were no indications of fire on the limited portions of the aircraft that were visible. The accident occurred during daylight hours.

Peruvian Air Force - Fuerza Aérea del Perú

The seaplane landed hard in the Caballococha's Laguna. Upon landing on water, the right float was torn off, the aircraft overturned and sank. All 11 occupants were rescued and the aircraft was damaged beyond repair. It was performing a flight from Iquitos on behalf of the 42nd Group of the Peruvian Air Force.

Arctic Sunwest Charters

The float-equipped de Havilland DHC-6-300 Twin Otter (registration C-GARW, serial number 367) was landing at the float-plane base (CEN9) located in Yellowknife, Northwest Territories, along the western shore of Great Slave Lake, beside the area known as Old Town. There were 2 crew members and 7 passengers on board, and the first officer was the pilot flying. On touchdown, the aircraft bounced, porpoised and landed hard on the right float. The flight crew initiated a go-around; the aircraft lifted off at low speed in a nose-high, right-wing-low attitude, and it continued in a right turn towards the shore. As the turn continued, the aircraft’s right wing contacted power lines and cables before the float bottoms impacted the side of an office building. The aircraft then dropped to the ground on its nose and cart-wheeled into an adjacent parking lot. Both crew members were fatally injured, 4 passengers were seriously injured, and 3 passengers sustained minor injuries. The aircraft was substantially damaged. The 406-megahertz emergency locator transmitter activated. There was no fire. The accident occurred at 1318 Mountain Daylight Time.

Trans Maldivian Airways

The 8Q-TMD aircraft took-off from water runway of Male’ International Airport North Bound Left (NL) at 0820 hrs local time on 11 July 2011 for a routine training flight bound to Maadhiggaru Falhu (a lagoon located approximately 15 nautical miles south west of the Male’ International Airport). The sky was clear with good visibility and wind 8-10 knots from west and south west. During the training 5 landings and take-offs were made simulating different conditions of flight. Crew confirmed that all these landings and take-offs were made inside the lagoon except the last landing where the crew decided to land on open water outside the lagoon. Crew were simulating single engine landing with a tail wind. As per the crew, the aircraft initial touch down was smooth. However, they stroke a wave which made the aircraft bounce up for about 20 feet. With the low power the aircraft hit the water again, resulting in multiple float attachments to break. Both front and main spreader bars broke and floats rose up twisted, hitting the engine bottom cowlings. Propeller cut was found on top front of both floats.

Desert Sand Aircraft Leasing

The airplane had not been flown for about 5 months and the purpose of the accident flight was a maintenance test flight after both engines had been replaced with higher horsepower models. Witnesses observed the airplane depart and complete two uneventful touch-and-go landings. The airplane was then observed to be struggling to gain altitude and airspeed while maneuvering in the traffic pattern. One witness, who was an aircraft mechanic, reported that he observed the airplane yawing to the left and heard noises associated with propeller pitch changes, which he believed were consistent with the "Beta" range. The airplane stalled and impacted trees in a wooded marsh area, about 1 mile from the airport. It came to rest about 80-degrees vertically. Examination of the wreckage did not reveal any preimpact malfunctions; however, the lack of flight recorders and the condition of the wreckage precluded the gathering of additional relevant information. Damage observed to both engines and both propellers revealed they were likely operating at symmetrical power settings and blade angles at the time of the impact, with any differences in scoring signatures likely the result of impact damage. The reason for the yawing and the noise associated with propeller pitch changes that were reported prior to the stall could not be determined.

Ecuadorian Air Force - Fuerza Aérea Ecuatoriana

The crew departed Shell Mera-Río Amazonas Airport at 1530LT on a flight to Tena on behalf of the ECORAE's Institute, a government supply and support program for isolated population in the center of Ecuador. Fifteen minutes after takeoff, the twin engine aircraft crashed in unknown circumstances near Santa Clara, about 30 km northeast of Shell Airport. A crew survived while five other occupants were killed. The only survivor died few hours later.

Tara Air

The twin engine aircraft departed Lamidanda Airport at 1508LT on a flight to Kathmandu. Shortly after departure, the crew was cleared to climb to 10,500 feet but ATC ask them to maintain 8,500 feet due to traffic. The captain disagreed with this ATC instruction and continued to climb. The copilot asked the captain to accept the ATC proposal so finally, the captain cleared the copilot (who was the pilot in command) to descend to 8,500 feet despite the fact it was risky due to the mountainous terrain. Few minutes later, the aircraft entered clouds when the right wing impacted ground. The aircraft crashed in a rocky area located on the Palunge Hill, near Okhaldhunga. The wreckage was found the following morning. The aircraft was destroyed by impact forces and all 22 occupants were killed. IMC conditions prevailed at the time of the accident due to low visibility (cloudy conditions).

Kenn Borek Air

The crew was performing a supply mission in the Nunavut with three scientists on board. Equipped with ski, the aircraft landed on the snow covered terrain some 168 km north of Alert Air Base. After landing, the aircraft came to a halt when the right ski punctured the ice and the aircraft partially sunk while both engines were still running. All five occupants escaped uninjured and were evacuated two hours later by the crew of a Bell 407 to Resolute Bay. Damaged beyond repair, the aircraft was abandoned on site and later cancelled from registry in November 2011.

Airlines PNG

On 11 August 2009, a de Havilland Canada DHC-6 Twin Otter aircraft, registered P2-MCB, with two pilots and 11 passengers, was being operated on a scheduled regular public transport service from Port Moresby to Kokoda Airstrip, Papua New Guinea (PNG). At about 1113, the aircraft impacted terrain on the eastern slope of the Kokoda Gap at about 5,780 ft above mean sea level in heavily-timbered jungle about 11 km south-east of Kokoda Airstrip. The aircraft was destroyed by impact forces. There were no survivors. Prior to the accident the crew were manoeuvring the aircraft within the Kokoda Gap, probably in an attempt to maintain visual flight in reported cloudy conditions. The investigation concluded that the accident was probably the result of controlled flight into terrain: that is, an otherwise airworthy aircraft was unintentionally flown into terrain, with little or no awareness by the crew of the impending collision.

Merpati Nusantara Airlines - MNA

On the morning of Sunday, 2 August 2009, a de Havilland DHC-6 Twin Otter aircraft, registered PK-NVC, operated by PT. Merpati Nusantara Airlines as flight number MZ-7960D, departed from Sentani Airport, Jayapura for Oksibil Airport. The flight was planned in accordance with the visual flight rules (VFR). There were 15 persons on board; two pilots, one engineer, 10 adult passengers and two infants. The estimated flight time was 50 minutes. The fuel on board was sufficient for 2 hours and 50 minutes flight time. About 15 minutes prior to the estimated time of arrival at Oksibil the crew of another aircraft informed the Twin Otter crew that the weather in the Oksibil area was partly cloudy. There were no further reports of radio transmissions from the Twin Otter, and it did not arrive at Oksibil. A search was initiated at the time the aircraft would have run out of fuel. On the morning of 4 August 2009, searchers located the wreckage of the Twin Otter at an elevation of about 9,300 feet about 6 Nm from Oksibil. The aircraft was destroyed by impact forces, and all of the occupants were fatally injured.

Aviastar Mandiri

The twin engine aircraft departed Dekai Airport at 1530LT on a cargo flight to Wamena, carrying three crew members and a load of 1,600 kilos of various goods. Between 1554LT and 1600LT, the crew was in contact with Wamena. At 1601LT, while cruising at an altitude of 9,600 feet in limited visibility, the aircraft collided with a mountain slope. The wreckage was found a day later about 19 km southeast from Wamena. The aircraft disintegrated on impact and all three occupants were killed.

Maldivian Air Taxi

The 8Q-MAG aircraft departed at 0945hrs, with 3 crew and 4 passengers on board, for a Photo Flight around the Lagoon of Halaveli (North Ari Atoll) from the floating platform ( fixed to jetty) of Halaveli (North Ari Atoll). The sky was clear with good visibility and wind, 8-10 knots, from westerly direction. The estimated flight time for the flight was 40 minutes. The aircraft took off westbound. After levelling the aircraft the co-pilot gave his seat to the cameraman, one of the passengers. The co-pilot remained at third row left seat from thereon until the aircraft met the accident. According to the crew and passengers the aircraft made few orbits (right bank) around the island at the initial levelled height and, then descended lower heights and made few more orbits around the lagoon for photography. The passenger seated at the cabin wearing the headset informed the PIC that they got all the shots they wanted and now he could land. PIC started a descending turn (right bank) while keeping the passenger at the co-pilot seat in order to give a different view to him. Before the PIC could complete the turn, the right wing and/or float hit the water. The accident resulted in both wings being broken at the root. Left float was detached and right float got stuck, between the engine and the fuselage, blocking the co-pilot exit. Empennage was twisted upside down. The depth of the lagoon at the site of wreckage was about 1 meter. All the passengers and crew were able to escape the aircraft without any fatalities.

Transwest Air

The aircraft was taking off from a ski strip east of and parallel to Runway 36 at La Ronge. After the nose ski cleared the snow, the left wing rose and the aircraft veered to the right and the captain, who was the pilot flying, continued the take-off. The right ski, however, was still in contact with the snow. The aircraft became airborne briefly as it cleared a deep gully to the right of the runway. The aircraft remained in a steep right bank and the right wing contacted the snow-covered ground. The aircraft flew through a chain link fence and crashed into trees surrounding the airport. The five passengers and two crewmembers evacuated the aircraft with minor injuries. There was a small fire near the right engine exhaust that was immediately extinguished by the crew.

Yeti Airlines

The aircraft departed Kathmandu-Tribhuvan Airport at 0651LT on a regular schedule service to the Lukla-Tenzing-Hillary Airport. On approach to runway 06, the crew encountered poor visibility due to foggy conditions. Despite the pilot did not establish any visual contact with the ground, he continued the approach when, on short final, the aircraft struck a rock and crashed just below the runway 06 threshold, bursting into flames. The captain was seriously injured while 18 other occupants were killed, among them 12 Germans, 2 Australians and 5 Nepalese.

Maldivian Air Taxi

14th July 2008 was a Monday; the busiest day of the week where there is an average of 150-200 movements. 8Q-MAS completed six sectors prior to the accident, with the same flight crew. Sixteen pieces of baggage were loaded, in the aft cabin, with total weight of 458 lbs. The flight manifest signed by Pilot in Command indicated that the aircraft was loaded up to 11874 lbs. The aircraft was boarded with 14 passengers (7 females, 6 males and 1 child) and the flight manifest used approved weights of 77 lbs Child, 181 lbs for male and 141 lbs for female to calculate the aircraft weight. The aircraft had 930 lbs of fuel. This particular aircraft was a short nose twin otter aircraft, with main loading in aft cabin. The MAT seaplane operation was based on a day VFR, non-schedule and a self dispatch system. All pre-flight duties were completed by the crew. The weather was windy and sea was rough. The aircraft departed at 12.11 hrs from MAT dock at Male International Airport, Water Aerodrome to Adaaran Club Bathala with 14 passengers total: 10 passengers to Adaaran Club Bathala, 2 passengers to Nika Maldives and 2 Passengers to W Retreat and Spa (Fesdu). The estimated flight time to destination was 20 minutes. The W Retreat and Spa Maldives Resort’s Speed Boat (Angelina) (a 34 ft Triana Express) was moored at a buoy (located at 04 04’ 43.6” N, 072 56’ 37.1” E) used by MAT to moor the aircrafts for night stops. The floating platform was located (04 04’ 43.5”N, 072 56’ 38.8”E) east of the buoy. The distance between the floating platform and buoy is around 165 feet. Around 12:30 the aircraft approached for landing near the floating platform. The wind was on a westerly direction 20 to 25 knots and the aircraft approached for a westbound landing. The aircraft made an orbit over the lagoon to inspect the water. The aircraft did a touchdown and was cutting the wave tops to find an appropriate location to stop, when it hit a big wave and was airborne. The aircraft veered to the left. The PIC declared to do a go around. The crew action was 10 degree flap, full throttle and Max Prop RPM. On climb the aircraft collided with the Speed Boat and the aircraft veered to the right and PIC was able to land on LH float.

Chilean Air Force - Fuerza Aérea de Chile

The crew departed Puerto Montt-El Tepual for a training flight. En route, the twin engine aircraft collided with the cables of a 23,000 volts powerline and crashed on a hilly terrain, bursting into flames. All three crew members were killed.

Wiggins Airways

The pilot contacted air traffic control and requested clearance to taxi for departure approximately an hour after the scheduled departure time. About 4 minutes later, the flight was cleared for takeoff. A witness observed the airplane as it taxied, and found it strange that the airplane did not stop and "rev up" its engines before takeoff. Instead, the airplane taxied into the runway and proceeded with the takeoff without stopping. The airplane took off quickly, within 100 yards of beginning the takeoff roll, became airborne, and entered a steep left bank. The bank steepened, and the airplane descended and impacted the ground. Post accident examination of the wreckage revealed that the pilot's four-point restraint was not fastened and that at least a portion of the cockpit flight control lock remained installed on the control column. One of the pre-takeoff checklist items was, "Flight controls - Unlocked - Full travel." The airplane was not equipped with a control lock design, which, according to the airframe manufacturer's previously issued service bulletins, would "minimize the possibility of the aircraft becoming airborne when take off is attempted with flight control locks inadvertently installed." In 1990, Transport Canada issued an airworthiness directive to ensure mandatory compliance with the service bulletins; however, the Federal Aviation Administration did not follow with a similar airworthiness directive until after the accident.

Waha Oil Company

The crew was completing a local training flight at Sidra Airport when the accident occurred in unknown circumstances. The aircraft came to rest in a sandy area with its undercarriage and left wing sheared off. Both pilots evacuated safely.

Argentinian Air Force - Fuerza Aérea Argentina

Shortly after takeoff from Comodoro Rivadavia Airport, while climbing, the crew encountered an unexpected situation and was forced to attempt an emergency landing. The aircraft crash landed in a desert area located about 10 km from the airport. While all six occupants escaped uninjured, the aircraft was damaged beyond repair.

Air Serv International

The crew departed Punia on a ferry flight to Goma. About 10 minutes into the flight, while cruising at a relative low altitude, the aircraft collided with power lines. The crew attempted an emergency landing when the aircraft crashed in the Lowa River located about 30 km northeast of Punia, coming to rest upside down. Both pilots escaped with minor injuries while the aircraft was damaged beyond repair.

Air Moorea

On Thursday 9 August 2007, the DHC-6 aeroplane registered F-OIQI was scheduled to fly a public transport flight (QE1121) between Moorea and Tahiti Faa’a with a pilot and 19 passengers on board. The flight, with an average duration of 7 minutes, is performed under VFR at a planned cruise altitude of 600 feet. The following information is derived from the on-board audio recording and witness statements. At 21 h 53 min 22, startup was authorised. The pilot made the safety announcement in English and in French: “Ladies and Gentlemen, hello and welcome on board. Please fasten your seatbelts”. At 21 h 57 min 19, the air traffic controller cleared the aeroplane to taxi towards holding point Bravo on runway 12. At 21 h 58 min 10, the aeroplane was cleared to line up. It taxied up the runway and lined up at the level of the second taxiway. At 22 h 00 min 06, the aeroplane was cleared for takeoff. Six seconds later the engines were powered up. At 22 h 00 min 58, the pilot retracted the flaps. At 22 h 01 min 07, propeller speed was reduced. At 22 h 01 min 09 the pilot uttered an expression of surprise. Two GPWS warnings sounded, propeller speed increased and four further GPWS warnings sounded. The aeroplane struck the surface of the sea at 22 h 01 min 20. One minute and eight seconds elapsed between engine power-up and the end of the audio recording. Fourteen bodies were recovered during the rescue operations. Some aeroplane debris, including parts of the right main gear and seat cushions were recovered by fishermen and the rescue team. Some days later, at a depth of seven hundred metres, a fifteenth body was recovered during operations to recover the flight recorder, both engines, the instrument panel, the front part of the cockpit including engine and flaps controls, the flaps jackscrews and the tail section. It was noted that the rudder and elevator control cables were broken off in their forward parts and that the elevator pitch-up control cable had, in its aft part, a second failure whose appearance was different from that observed on the other failures that were examined.

Liard Air

At approximately 1235 Pacific daylight time, the Liard Air Limited de Havilland DHC-6-100 Twin Otter (registration C-FAWC, serial number 108) was taking off from a gravel airstrip near the Northern Rockies Lodge at Muncho Lake on a visual flight rules flight to Prince George, British Columbia. After becoming airborne, the aircraft entered a right turn and the right outboard flap hanger contacted the Alaska Highway. The aircraft subsequently struck a telephone pole and a telephone cable, impacted the edge of the highway a second time, and crashed onto a rocky embankment adjacent to a dry creek channel. The aircraft came to rest upright approximately 600 feet from the departure end of the airstrip. An intense post-impact fire ensued and the aircraft was destroyed. One passenger suffered fatal burn injuries, one pilot was seriously burned, the other pilot sustained serious impact injuries, and the other two passengers received minor injuries.

Peruvian Air Force - Fuerza Aérea del Perú

The Twin Otter departed Iquitos Airport at 1137LT on a flight to Pucallpa with intermediate stops in Requena, Orellana, Pampa Hermosa and Contamana. While descending to Pampa Hermosa in marginal weather conditions, the aircraft crashed in a mountainous area located few km from the airport. Seven passengers were rescued while 13 other occupants were killed.

French Air Force - Armée de l'Air

The Twin Otter departed Al-Gorah on a flight to Sainte-Catherine, carrying 8 passengers (among them six membres of the French Air Force) and one Canadian pilot. En route, he contacted ATC and reported technical problems. While attempting an emergency landing, the aircraft collided with a Jordan truck carrying glass and crashed, bursting into flames. Both truck drivers were slightly injured while the aircraft was destroyed and all 9 occupants were killed. The flight was operated by the French Air Force on behalf of the Multinational Force and Observers (MFO) based in the Sinai area. French Air Force members killed: Cptn Laurence Briançon-Forest, Lt Guillaume Pike, SgtC Yann Poilly, SgtC Laurent Pottier, SgtC Hervé Bouffenie, Sgt Julien Flégo.

Trigana Air Service

The twin engine aircraft departed Mulia on a special flight to Ilaga, carrying a delegation of nine people flying to Ilaga to visit several districts of the Irian Jaya province on behalf of a talks between several administrations. While cruising at an altitude of 10,500 feet in marginal weather conditions, the aircraft struck Mt Puncak Jaya. The wreckage was found the following day. All 12 occupants were killed.

Quantum Leap Skydiving Center

On July 29, 2006, about 1345 central daylight time, a de Havilland DHC-6-100, N203E, registered to Adventure Aviation, LLC, and operated by Skydive Quantum Leap as a local parachute operations flight, crashed into trees and terrain after takeoff from Sullivan Regional Airport (UUV), near Sullivan, Missouri. The pilot and five parachutists were killed, and two parachutists were seriously injured. The flight was operated under 14 Code of Federal Regulations (CFR) Part 91 with no flight plan filed. Visual meteorological conditions prevailed. According to photographic evidence provided by a witness, the pilot taxied the airplane onto runway 24 from the intersecting taxiway, which is about 1,700 feet from the runway’s west end, and began a takeoff roll to the west from that location, rather than using the runway’s entire 4,500-foot length. Photographic evidence depicting the airport windsock shows that the airplane departed into a moderate headwind. Witnesses at the airport reported seeing the airplane take off and climb to about treetop height. Several witnesses reported hearing a “poof” or “bang” noise and seeing flames and smoke coming from the right engine. One witness reported that, after the noise and the emergence of flames, the right propeller was “just barely turning.” Photographic evidence shows that, at one point after the flames occurred, the airplane was about one wingspan (about 65 feet) above the runway. One witness estimated that the airplane climbed to about 150 feet. Witnesses reported that the airplane lost some altitude, regained it, and then continued to fly low above the treetops before turning to the right and disappearing from their view behind the tree line. Another witness in the backyard of a residence northwest of the airport reported that she saw the airplane flying straight and level but very low over the trees before it dived nose first to the ground. She and her father called 911, and she said that local emergency medical service personnel arrived within minutes. The airplane impacted trees and terrain and came to rest vertically, nose down against a tree behind a residence about 1/2 mile northwest of the end of runway 24.

Yeti Airlines

The twin engine aircraft departed Nepalganj Airport on a domestic service to Jumla with an intermediate stop in Surkhet, carrying six passengers, three crew members and a load consisting of bags containing grains for a total of 941 kilos. While approaching Jumla Airport, the crew was informed that runway 27 was in use with a wind from 240 at 4 knots. For unknown reasons, the captain started the approach to runway 09 at 1201LT. At an excessive speed, he missed the runway, initiated a go-around procedure and passed to the right of the tower. Then, he started a steep turn to the left when the aircraft lost height and speed and crashed in a field located 500 meters east of the airport, bursting into flames. The aircraft was totally destroyed by impact forces and a post crash fire and all 9 occupants were killed.

Air São Tome e Principe

The twin engine aircraft departed Santo Antonio Airport on a local training flight, carrying four pilots. While on approach to runway 29, the aircraft went out of control and crashed in the sea few km offshore. All four occupants were killed.

NatureAir

Following an uneventful flight from San José-Tobías Bolaños Airport, the crew started the descent to Tamarindo Airport runway 07. On short final, at a height of about 500 feet, control was lost and the aircraft crashed in a wooded area located 2 km short of runway. All eight occupants were injured while the aircraft was destroyed.