Country

Crash of a Pacific Aerospace PAC 750XL in Grenchen: 1 killed

Date & Time: Feb 18, 2024 at 1404 LT
Operator:
Registration:
HB-TCP
Flight Phase:
Survivors:
No
Schedule:
Grenchen - Grenchen
MSN:
180
YOM:
2011
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The single engine airplane departed Grenchen Airport on a local skydiving mission, carrying 11 skydivers and one pilot. After all skydivers left the airplane, the pilot was returning to his base when he lost control of the airplane that entered a dive and crashed in a grassy area located in the vicinity of the airport. The airplane was totally destroyed and the pilot was killed. All 11 skydivers landed safely.

Crash of a Pacific Aerospace PAC 750XL in Kudjip

Date & Time: Feb 9, 2023 at 1250 LT
Operator:
Registration:
P2-BJD
Flight Phase:
Survivors:
Yes
Schedule:
Giramben - Simbai
MSN:
124
YOM:
2005
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3582
Captain / Total hours on type:
1885.00
Aircraft flight hours:
13811
Aircraft flight cycles:
17220
Circumstances:
The flight was planned to depart Giramben at 12:40, and track North for Simbai Airstrip, Madang Province at 9,000 ft AMSL. According to the pilot, the aircraft was loaded by NCA ground handlers following his instructions. The manifest was completed by one of the ground handler, who stated that the aircraft was loaded by the other ground handlers while he was completing the manifest in the vehicle, due to no proper shed for him to work from. The pilot also stated that at the time the loading was completed, and the passengers had boarded the aircraft, he observed that the winds were variable, blowing directly from the North and from the East as well. Recorded data showed that the aircraft commenced taxiing at 12:44. During the take-off roll, at the expected airborne point, about 500 m down the runway, as the aircraft accelerated with the airspeed approaching 60 knots, the right wheel hit a soft spot on the strip which dramatically reduced the momentum and speed of the aircraft, as described by the pilot. Eyewitnesses reported seeing the aircraft getting airborne briefly and got back on the ground again. The pilot recalled that by the time the aircraft got back on the ground he realized that he had passed the nominated committal point, which was identified during onsite activities to be about 540 m from the threshold of runway 16. The pilot opted to continue with the take-off roll, with full power hoping that the aircraft would regain speed on the remaining part of the strip to get airborne again. The pilot recalled reaching the end of the runway and getting airborne again with an airspeed of 50 kts airborne again, however, the right wheel got caught on the barbed wire of the perimeter fence that ran across to the runway, and subsequently impacted terrain. The pilot stated that he had lost consciousness at the time of the initial impact and therefore, had no recollection from thereon. The investigation found that the aircraft got airborne about 19 m past the end of runway 16. However, the aircraft’s main landing gears got caught on the perimeter fencing wire, subsequently impacting ground about 100 m from the end of the runway, then continued with the momentum and came to rest, in a local village garden about 160 m from the end of the runway. The aircraft was destroyed by impact forces. The pilot and passengers were rescued by the locals and taken to Nazarene General Hospital, Jiwaka Province, for treatment. The pilot, male adult and infant passengers sustained serious injuries, and the female passenger sustained minor injuries.
Probable cause:
The following factors were identified:
- The pilot did not complete a trim sheet for the flight.
- The manifest was completed by a ground handler who was not present at the time the cargo was being loaded by other ground handlers. The manifest was not signed by the ground handler who completed it, nor was it authorized by the pilot before departure.
- Pilot’s lack of supervision of the aircraft’s loading process to ensure cargo is loaded correctly and in accordance with the prescribed limitations and to prevent calculation errors. As a result, it was likely that the aircraft was overweight when it departed.
- Wet strip surface conditions that caused significant resistance during the take-off roll and impeded the aircraft’s ability to reach its required lift off airspeed.
- Pilot’s decision to continue the take-off roll after passing the committal.
- Training deficiencies of ground handlers and the pilot.
- The lack of adequate Quality Assurance systems oversight on the operator’s operating standard procedures.
Final Report:

Crash of a Pacific Aerospace PAC 750XL in Tekin

Date & Time: Jan 26, 2022 at 0943 LT
Operator:
Registration:
P2-BWC
Survivors:
Yes
Schedule:
Kiunga – Oksapmin
MSN:
136
YOM:
2007
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14129
Captain / Total hours on type:
3625.00
Aircraft flight hours:
6752
Aircraft flight cycles:
13861
Circumstances:
The airplane was on a VFR charter flight from Kiunga Airport, Western Province to Tekin Airstrip, Sandaun Province, Papua New Guinea. During the landing roll aircraft sustained a left main landing gear assembly collapse and subsequent runway excursion. There were seven persons onboard: one pilot and six passengers. At 09:06, P2-BWC departed Kiunga Airport and arrived at Tekin circuit area at 09:40. The pilot established the aircraft on the final approach profile, he configured the aircraft for landing by fully extending the flaps and maintained an airspeed of about 80 knots (kts). The pilot also stated that he experienced a downdraft prior to touch down. The aircraft landed at 09:43 with an airspeed of 75 knots as recalled by the pilot. The aircraft touched down about 3m short of the airstrip edge boundary. The investigation determined that due to reduced damping effect of the oleo and/or the tyre of the left main landing gear, the landing gear attachment bolts sustained significant impact stress from the landing impact force and snapped, causing the gear assembly to collapse and separate from the aircraft. Subsequently, the left wing abruptly dropped, and the aircraft began veering to the left, towards the eastern edge of the airstrip. The aircraft continued veering to the left and subsequently the left wingtip struck the outer edge of the extended right-hand flap of P2-BWE, a wreckage of the same aircraft type owned and operated by NASL that was involved in a similar accident on 18 January 2022, causing P2-BWC to abruptly veer further left and skid across the airstrip boundary as the nose-wheel and right main wheel bogged into the ground. The pilot immediately shut down the engine and evacuated the passengers with the assistance of one of the Operator’s personnel who was also a passenger on board. There were no reported injuries and the aircraft sustained significant damage.
Probable cause:
During the landing at Tekin Airstrip, the pilot encountered downdraft and touchdown about 4 metres short of the designated landing threshold. Due to less damping effect on the oleo or the tyre, the landing impact force could have transferred up through the structure and concurrently causing the left main landing gear to collapse. Subsequently, the left wing abruptly dropped and began veering to the left, towards the eastern edge of the airstrip. The aircraft continued veering to the left and subsequently the left wingtip struck the outer edge of the extended right-side flap of P2-BWE, causing it to abruptly veer further left and skid across the airstrip boundary as the nose-wheel and right main wheel bogged into the ground.
Final Report:

Crash of a Pacific Aerospace PAC 750XL in Tekin

Date & Time: Jan 18, 2022 at 0926 LT
Operator:
Registration:
P2-BWE
Survivors:
Yes
Schedule:
Kiunga – Oksapmin
MSN:
161
YOM:
2009
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9305
Captain / Total hours on type:
332.00
Aircraft flight hours:
7549
Aircraft flight cycles:
11178
Circumstances:
The airplane was conducting a single pilot VFR charter flight from Kiunga Airport, Western Province to Tekin Airstrip, Sandaun Province, Papua New Guinea when during the landing roll, the aircraft sustained a left Main Landing Gear (MLG) assembly collapse and subsequent runway excursion. There were eight persons onboard: one pilot and seven passengers. At 08:43, P2-BWE departed Kiunga Airport and arrived at Tekin Airstrip circuit at 09:18. The pilot then tracked towards the Northwest of the airstrip and made a left base turn for approach. The pilot stated that he established the aircraft on final approach with an airspeed of 120 kts. He subsequently configured the aircraft for landing; propeller pitch set to full fine, power set to maintain nominated approach speed, and full flap. The pilot indicated that he reduced airspeed while on approach and maintained an airspeed between 85 and 90 kts. As he flared the aircraft to land, the airspeed was between 75 to 80 kts. The touchdown speed, as he recalled, was 75 kts. The aircraft touched down two metres short of the designated landing threshold of runway18, which had an elevation of 15cm. Reviewing the flight records of the pilot, and from his interview, the AIC deduced that the pilot was not adequately familiar with Tekin Airstrip. The aircraft sustained substantial damaged. All the passengers and pilot evacuated the aircraft without injuries.
Probable cause:
The investigation identified that during touchdown, the aircraft’s main landing gear tyre hit the 15cm elevation at the edge of runway18, resulting in the left MLG assembly weakening. The investigation determined that due to less damping effect on the oleo or the tyre, the landing impact force could have transferred up through the structure and concurrently causing the left MLG assembly to collapse. Following the collapse of the left MLG assembly, the left-wing assembly dropped and hit the ground, the flap detached and began to drag on the surface of the strip creating markings. The aircraft immediately began veering left, towards the edge (boundary) of the airstrip and impacted the drainage ditch adjacent to the runway where it came to rest.
Final Report:

Crash of a Pacific Aerospace PAC 750XL near Oksibil: 8 killed

Date & Time: Aug 11, 2018 at 1420 LT
Operator:
Registration:
PK-HVQ
Survivors:
Yes
Site:
Schedule:
Tanah Merah – Oksibil
MSN:
144
YOM:
2009
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
13665
Captain / Total hours on type:
1468.00
Aircraft flight hours:
4574
Aircraft flight cycles:
5227
Circumstances:
On 11 August 2018, a PAC 750XL aircraft registered PK-HVQ was being operated by PT. Marta Buana Abadi (Dimonim Air) on unscheduled passenger flight from Tanah Merah to Oksibil. At the day of the occurrence the meteorological condition at Oksibil was below the requirement of Visual Flight Rule (VFR) weather minima and did not improve. Being aware that some flights had performed flight to Tanah Merah to Oksibil and returned, the pilot decided to fly to Oksibil. At 1342 LT, on daylight condition the PK-HVQ aircraft departed from Tanah Merah to Oksibil, on board the aircraft were one pilot, one observer pilot and 7 passengers. According to the passenger and cargo manifest, the total weight of passenger and the baggage were 473 kg. Prior to the departure, there was no record or report of aircraft system malfunction. At 1411 LT, the PK-HVQ pilot made initial contact to Oksibil Tower controller and reported that the aircraft was maintaining altitude of 7,000 feet over and the estimate time arrival at Oksibil would be 0520 UTC (1420 LT). The Oksibil Tower controller advised the pilot of the latest meteorological condition that the visibility was 1 up to 2 km and most of the area were covered by cloud. At 1416 LT, the pilot reported that the aircraft position was over Oksibil Aiport and the Oksibil Tower controller instructed the pilot to continue the flight to the final runway 11 and to report when the runway had in sight. The Oksibil Tower controller and pilots of other aircraft called the pilot but no reply. On the following day, the aircraft was found on a ridge of mountain about 3.8 Nm north west of Oksibil on bearing 331° with elevation about 6,800 feet. Eight occupants were fatally injured and one occupant was seriously injured.
Probable cause:
The KNKT concluded the contributing factors as follows:
- The VFR weather minimum requirement that was not implemented properly most likely had made the pilot did not have a clear visual to the surrounding area.
- Considering that the Pilot in Command (PIC) had lack knowledge of the terrain surrounding the Oksibil area, and the absence of voice alert from the TAWS when the aircraft flying close to terrain, resulted in the PIC did not have adequate awareness to the surrounding terrain while flying into clouds and continued to fly below the terrain height until the aircraft impacted the terrain.
Final Report:

Crash of a Pacific Aerospace 750XL Falcon 3000 near Tiniroto: 2 killed

Date & Time: Dec 12, 2016 at 0857 LT
Operator:
Registration:
ZK-JPU
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
117
YOM:
2005
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8518
Captain / Total hours on type:
3210.00
Aircraft flight hours:
8028
Circumstances:
At approximately 0500 hrs, 12 December 2016, the pilot of ZK-JPU, arrived at Gisborne Aerodrome. The pilot was accompanied by the operator’s recently employed (trainee) loader driver and already at the hangar was a senior loader driver. The pilot conducted the preflight checks of the aircraft for the day’s agricultural aircraft operations. Earlier that morning the Managing Director of the operator had called the pilot of ZK-JPU. The Managing Director requested that after finishing the first aerial topdressing task at Tauwharetoi Station and prior to the next planned task at Waimaha Station, the pilot complete a task at Pembroke Station. This was because the Managing Director was unwell and unable to undertake the Pembroke Station task as planned. The pilot of ZK-JPU agreed to the additional task. The original work plan for the day was for both loader drivers to attend the first task at Tauwharetoi Station, with the senior loader driver providing oversight for the trainee loader driver. The pilot and the senior loader driver were then to proceed to the second task of the day, while the trainee loader driver was scheduled to return to the aerodrome with the loader truck from the first task. The expectation was for the pilot to go straight from the Tauwharetoi Station task to the Pembroke Station task and then proceed to Waimaha Station. ZK-JPU departed Gisborne Aerodrome at approximately 0515 hrs with the pilot and both loader drivers on board. The aircraft was to operate from a nearby private airstrip where the loader truck was already located, as the task had been commenced the previous week. The aircraft landed at the airstrip at approximately 0530 hrs and the pilot assisted the senior loader driver to get the truck ready, double-checking the calibration of the weigh scales and fuel drain, before commencing the task at approximately 0600 hrs. On the day of the accident another pilot from the same operator, who was operating a similar Pacific Aerospace Ltd 750XL, ZK-XLA, was aerial topdressing an area of Bushy Knoll Station, operating off the Tongataha airstrip. Bushy Knoll Station is to the north of Tauwharetoi Station, alongside the route to the next two tasks scheduled for ZK-JPU at Pembroke and Waimaha Stations. The pilot of ZK-XLA commenced operating at approximately 0555 hrs and completed two to three loads before hearing the pilot of ZK-JPU over the radio at approximately 0615 hrs. The brief conversation that followed consisted of an exchange of greetings and description of locations and intentions. Both pilots then continued with their tasks without further direct communication. On completion of the first task the pilot of ZK-JPU landed at the private airstrip and instructed the senior loader driver to pack up the gear and head back to base. The senior loader driver refuelled the aircraft with 100 litres of fuel, packed up the gear and gave the trainee loader driver the radio which had been used to communicate with the pilot. After a 15 minute break the pilot of ZK-JPU was observed by the senior loader driver getting into the left seat of the aircraft and the trainee loader driver into the right seat. The senior loader driver observed ZK-JPU take off, and then departed the airstrip in the loader truck, to return to the aerodrome. At approximately 0850 the pilot of ZK-XLA received a radio call from the pilot of ZKJPU asking “are you breaking left or right?” followed by the pilot of ZK-JPU stating “I am to your left”. ZK-JPU was then observed by the pilot of ZK-XLA flying behind and to the left of ZK-XLA. The pilot of ZK-XLA advised the pilot of ZK-JPU that he was “sowing the boundary of Bushy Knoll Station […] finishing my run and […] turning right to head back to the airstrip”. Spanning the valley near the boundary of Bushy Knoll Station, near to where the pilot of ZK-XLA was operating were a set of 110 kV high voltage power lines (consisting of six wires termed ‘conductors’, supported by towers). These conductors comprised the two circuits supplying electricity to Gisborne and the East Coast region. The span traverses the valley approximately east-west and the height above terrain at the mid-span of the bottom two conductors (the lowest point of the span) was approximately 200 ft. At 0857 hrs the power supply to Gisborne and the East Coast was interrupted. Finishing the topdressing run, the pilot of ZK-XLA commenced a right climbing turn in order to return to the airstrip and sighted ZK-JPU over his right shoulder. At this point the pilot of ZK-XLA noted that something was trailing from the left wing of ZKJPU. Realising that the item trailing from ZK-JPU’s wing was a wire, the pilot of ZKXLA transmitted “you are trailing wire’’, however no response was received from ZK-JPU. The pilot of ZK-XLA witnessed ZK-JPU continue down the valley, slowly rolling to the left before impacting terrain, approximately 700 m further to the south. A postimpact fire ensued with the pilot of ZK-XLA observing “a lot of black smoke”. The pilot of ZK-XLA immediately commenced circling the accident site and attempted to call the operator via cellphone. Unable to make contact the pilot activated the emergency communications facility on the flight following equipment installed in the aircraft and reported the accident to Gisborne Tower. The accident occurred in daylight at 0857 hrs, approximately 24 NM W of Gisborne Aerodrome, at Latitude: S 38° 44' 30.85" Longitude: E 177° 28' 37.41".
Probable cause:
Conclusions
3.1 The aircraft struck six 110 kV high voltage power lines.
3.2 The pilot likely experienced inattentional blindness, in that the pilot’s attention was likely engaged on the other aircraft and thus the pilot failed to perceive the visual stimuli.
3.3 The pilot was appropriately rated and licensed to conduct the flight.
3.4 Research has shown that striking a wire that the pilot was aware of usually occurred because something changed, such as a last minute change of plan.
3.5 The pilot elected to change the plan at the last minute and detour during the positioning flight to an area where a pilot from the same operator was also conducting aerial topdressing.
3.6 The pilot did not conduct a hazard briefing for the area about to be flown and thus did not afford himself the most accurate and well informed mental model of the area the pilot elected to operate in.
3.7 Several human factors likely influenced the pilot’s decision-making and risk perception leading to the decision to change the original plan and deviate from the minimum heights as stipulated by CAR 91.311 and operators SOPs.
3.8 The safety investigation did not identify any mechanical defects which may have contributed to the accident.
3.9 The accident was not survivable.
Final Report:

Crash of a Pacific Aerospace 750XL in Chilkhaya: 2 killed

Date & Time: Feb 26, 2016 at 1305 LT
Operator:
Registration:
9N-AJB
Flight Phase:
Survivors:
Yes
Schedule:
Nepalgunj - Jumla
MSN:
160
YOM:
2009
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The single aircraft departed Nepalgunj at 1230LT bound for Jumla. About 35 minutes into the flight, the crew encountered an unexpected situation and attempted an emergency landing in a field. The aircraft eventually collided with an earth bank and came to rest near the village of Chilkhaya. Both pilots were killed and all 9 passengers were injured. The aircraft destroyed.

Crash of a Pacific Aerospace PAC750XL in Ninia: 1 killed

Date & Time: Aug 12, 2015 at 0748 LT
Operator:
Registration:
PK-KIG
Survivors:
Yes
Schedule:
Wamena – Ninia
MSN:
170
YOM:
2010
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1537
Captain / Total hours on type:
395.00
Aircraft flight hours:
757
Aircraft flight cycles:
1315
Circumstances:
On 12 August 2015, a PAC-750XL aircraft, registered PK-KIG, was being operated by PT. Komala Indonesia on an unscheduled passenger flight from Wamena Airport (WAJW) Papua to Ninia Airstrip , Yahukimo, Papua that was located on radial 127° from Wamena with a distance of approximately 26 Nm. At 0733 LT (2233 UTC), the aircraft departed from Wamena Airport with an estimated time of arrival at Ninia of 2248 UTC. The flight was uneventful until approaching Ninia. On board the aircraft were one pilot, one engineer and 4 passengers. According to the pilot statement, an airspeed indicator malfunction occurred during flight. Video footage taken by a passenger showed that, during the approach at an altitude of approximately 6,500 feet, the airspeed indicators indicated zero and the aural stall warning activated. The aircraft then flew on the left side and parallel to the runway. Thereafter the aircraft climbed, turned left and impacted the ground about 200 meters south-west of the runway. The engineer on board was fatally injured, one passenger had minor injuries and the other occupants, including the pilot, were seriously injured. Two occupants were evacuated to a hospital in Jayapura Airport and four others, including the fatally injured, were evacuated to a hospital in Wamena.
Probable cause:
The following findings were identified:
1. Continuing the flight with both airspeed indicators unserviceable increased the complexity of the flight combined with high-risk aerodrome increased the pilot workload.
2. The improper corrective action at the time of the aural stall warning activating on the final approach, and the aircraft flew to insufficient area for a safe maneuver.
3. The unfamiliarity to the airstrip resulted in inappropriate subsequent escape maneuver and resulted in the aircraft stalling.
4. The pilot was not provided with appropriate training and familiarization to fly into a high-risk airstrip
Final Report:

Crash of a Pacific Aerospace PAC 750XL in Taupo Lake

Date & Time: Jan 7, 2015 at 1216 LT
Operator:
Registration:
ZK-SDT
Flight Phase:
Survivors:
Yes
Schedule:
Taupo - Taupo
MSN:
122
YOM:
2005
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
588
Captain / Total hours on type:
14.00
Circumstances:
On 7 January 2015 a Pacific Aerospace Limited 750XL aeroplane was being used for tandem parachuting (or ‘skydiving’) operations at Taupō aerodrome. During the climb on the fourth flight of the day, the Pratt & Whitney Canada PT6A-34 engine failed suddenly. The 12 parachutists and the pilot baled out of the aeroplane and landed without serious injury. The aeroplane crashed into Lake Taupō and was destroyed.
Probable cause:
The following findings were identified:
- The first compressor turbine blade failed after a fatigue crack, which had begun at the trailing edge, propagated towards the leading edge. The blade finally fractured in tensile overload. The separated blade fragment caused other blades to fracture and the engine to stop.
- The fatigue crack in the trailing edge of the blade was likely initiated by the trailing edge radius having been below the specification for a new blade.
- The P&WC Repair Requirement Document 725009-SRR-001, at the time the blades were overhauled, had generic requirements for trailing edge thickness inspections but did not specify a minimum measurement for the trailing edge radius.
- The higher engine power settings used by the operator since August 2014 were within the flight manual limits. Therefore it was unlikely that the operator’s engine handling policy contributed to the engine failure.
- The operator had maintained the engine in accordance with an approved, alternative maintenance programme, but the registration of the engine into that programme had not been completed. The administrative oversight did not affect the reliability of the engine or contribute to the blade failure.
- It was likely that the maintenance provider had not followed fully the engine manufacturer’s recommended procedure for inspecting the compressor turbine blades. It could not be determined whether the crack might have been present, and potentially detectable, at the most recent borescope inspection.
- The operator had not equipped its pilots with flotation devices to cover the possibility of a ditching or an emergency bale-out over or near water.
- The pilot had demonstrated that he was competent and he had the required ratings. However, it was likely that the operator’s training of the pilot in emergency procedures was inadequate. This contributed to the pilot making a hasty exit from the aeroplane that jeopardized others.
Final Report:

Crash of a PAC-750XTOL in Golgubip

Date & Time: Jul 19, 2014 at 1143 LT
Operator:
Registration:
P2-RNB
Survivors:
Yes
Schedule:
Kiunga – Golgubip
MSN:
190
YOM:
2013
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2930
Captain / Total hours on type:
1900.00
Aircraft flight hours:
143
Circumstances:
A Pacific Aerospace PAC P-750 XTOL single engine aircraft was chartered to transport store goods and six passengers from Kiunga to Golgubip. Although Golgubip is in mountainous terrain and the weather in the area is often poor, the pilot was tasked to fly there without ever having been to Golgubip before. The terrain to the north north east of Golgubip rises gradually behind the airstrip. Visual illusions which may affect the pilot’s perception of height and distance can be associated with airstrips situated in terrain of this kind. On arrival at Golgubip, the pilot orbited and positioned the aircraft for landing. During the final approach he decided to discontinue the approach and to initiate a go-around procedure. The aircraft impacted terrain approximately 500 metres northwest of the airstrip and was substantially damaged. The six passengers were unhurt while the pilot sustained serious injuries. The pilot was treated in Golgubip following the accident, and was airlifted the next day to Tabubil, where he was admitted to hospital. It was later reported that the GPWS alarm sounded on approach until the final impact.
Probable cause:
Loss of control on final approach, maybe following visual illusions.
Final Report: