Region
code

PNG

Crash of a Pacific Aerospace PAC 750XL in Kudjip

Date & Time: Feb 9, 2023 at 1300 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
Circumstances:
The single engine airplane departed Giramben Airstrip on a taxi flight to Simbai with three passengers and one pilot on board. Shortly after takeoff, while climbing in heavy rain falls, it crashed near Kudjip, about seven km southeast of the airfield. The airplane broke in two and all four occupants were injured.

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 Cessna 402C in Papa Lealea

Date & Time: Jul 26, 2020 at 1246 LT
Type of aircraft:
Operator:
Registration:
VH-TSI
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Papa Lealea - Mareeba
MSN:
402C-0492
YOM:
1981
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On 26 July 2020, at 12:46 local time (02:46 UTC), a Cessna 402C aircraft, registered VH-TSI collided with trees during an aborted take-off at an uncommissioned field near Papa-Lealea, about 16 nm North-West of Port Moresby, Papua New Guinea. The pilot, during interview with the AIC, stated that he departed at 09:30 that day from Mareeba Airport, Queensland Australia and tracked towards the North North-East with a planned track set slightly left of Jacksons International Airport, Port Moresby, National Capital District, Papua New Guinea. As the aircraft neared the Southern shoreline (within the Caution Bay area), he diverted left and began tracking towards the North West along the coast in order to avoid flying over villages in the area. He subsequently crossed over land before turning back to approach the intended landing field. As the aircraft approached to land, the outboard section of the left wing was clipped by a tree and separated from the aircraft. According to the pilot, he continued on with the approach and landed on the field at about 12:20. The pilot reported that he had flown to and within Papua New Guinea in the past and was familiar with the area and airspace. He confirmed that after departing Mareeba, he switched off the transponder. After shutting down the aircraft, the aircraft was refuelled with jerrycans full of fuel (AvGas) and loaded with cargo by persons waiting on the ground. The pilot reported that he estimated that a distance of 800 m would be required for the take-off. According to the pilot, at about 12:40, he lined up and commenced his take-off roll from the Southern end of the field. As the aircraft lifted off, he noticed that the airspeed indicator (ASI) was not working. He also observed that the aircraft was not achieving a positive rate of climb. He subsequently pulled the throttles back and manoeuvred the aircraft back towards the ground. The aircraft touched down with a speed that the pilot described as higher than normal, with about 400 m of usable field remaining. The aircraft continued off the end of the field and into the bushes clipping trees along the way until it came to rest. The pilot informed the AIC that he was the sole occupant of the aircraft, and sustained minor injuries as a result of the occurrence. The aircraft was substantially damaged. The investigation confirmed that the fire to the left wing and engine was a post-accident event and was deliberate. The pilot was later arrested and a load of 500 kilos of cocaine distributed in 28 bales was found at the scene.
Probable cause:
The investigation determined that the separation of the outboard section of the left wing, clipped by a tree during the approach to land phase, affected the ability of the left wing to produce lift. The investigation could not conclusively determine the actual weight and balance of the aircraft as it was not possible to determine the quantity and quality of fuel on board, nor the weight and distribution of the cargo that was on board. The evidence gathered during the investigation did not allow the AIC to discard overweight, balance or centre of gravity issues due to improper loading or restrain of the cargo as factors contributing to the inability of the aircraft to obtain a positive rate of climb during take-off. The evidence of tire marks found by the investigators on the uncommissioned field indicated that the aircraft touched down about 400 m before the end of the field, distance that was not enough for the aircraft to come to a stop, continuing its landing roll into the bushes and impacting trees until it got to its final position. The investigation determined that the aircraft was not airworthy at the time of the accident and was unserviceable for the conduct of the flight. The investigation also determined that there was no proper document control to conduct timely scheduled maintenance and that there was no record of a certificate of airworthiness (CoA) at the time of the accident.
Final Report:

Crash of a Britten-Norman BN-2A Islander in Saidor Gap: 1 killed

Date & Time: Dec 23, 2017 at 1010 LT
Type of aircraft:
Operator:
Registration:
P2-ISM
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Derim - Lae
MSN:
227
YOM:
1970
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1982
Captain / Total hours on type:
139.00
Aircraft flight hours:
32232
Circumstances:
On 23 December 2017, at 00:10 UTC (10:10 local), a Britten Norman BN-2A Islander aircraft, registered P2-ISM (ISM), owned and operated by North Coast Aviation, impacted a ridge, at about 9,500 ft (6°11'29"S, 146°46'11"E) that runs down towards the Sapmanga Valley from the Sarawaget Ranges, Morobe Province. The pilot elected to track across the Sarawaget ranges (See figure 1), from Derim Airstrip to Nadzab Airport, Morobe Province, not above 10,000 ft. The track flown from Derim was to the northwest 6.5 nm (12 km) to a point 0.8 nm (1.5 km) westsouthwest of Yalumet Airstrip where the aircraft turned southwest to track to the Saidor Gap. GPS recorded track data immediately prior to the last GPS fix showed that the aircraft was on a shallow descent towards the ridge. The aircraft impacted the ridge about 150 m beyond the last fix. There were no reports of a transmission of an ELT distress signal. During the search for the aircraft, what appeared to be the right aileron was found hanging from a tree near the top of the heavily-timbered, densely-vegetated ridge. The remainder of the wreckage was found about 130 m from the aileron along the projected track. The aircraft impacted the ground in a steep nose-down, right wing-low attitude. The majority of the aircraft wreckage was contained at the ground impact point. The aircraft was destroyed by impact forces. The pilot, the sole occupant, who initially survived, was reported deceased by the rescue team on 27 December 2017 at 22:10. The pilot had made contact with one of the operator’s pilots at 16:15 on 23 December. The pilot’s time of death, recorded on the Death Certificate, was 10:40 am local on 24 December. Rescuers felled trees on the steep heavily timbered, densely vegetated slope about 20 metres from the wreckage and constructed a helipad.
Probable cause:
Cloud build up along the pilot’s chosen route may have forced him to manoeuvre closer than normal to the ridge, in order to avoid flying into the cloud. The aircraft’s right wing struck a tree protruding from the forest canopy during controlled flight into terrain. It is likely that the right aileron mass balance became snagged on the tree and rapidly dislodged the aileron from the wing. The loss of roll control, and the aerodynamic differential, forced the aircraft to descend steeply through the forest and impacted terrain.
Final Report:

Crash of a Britten-Norman BN-2T Islander in Kiunga: 12 killed

Date & Time: Apr 13, 2016 at 1420 LT
Type of aircraft:
Operator:
Registration:
P2-SBC
Survivors:
No
Schedule:
Oksapmin – Kiunga
MSN:
3010
YOM:
1983
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
4705
Captain / Total hours on type:
254.00
Aircraft flight hours:
2407
Aircraft flight cycles:
2886
Circumstances:
On the afternoon of 13 April 2016, a Pilatus Britten Norman Turbine Islander (BN-2T) aircraft, registered P2-SBC, operated by Sunbird Aviation Ltd, departed from Tekin, West Sepik Province for Kiunga, Western Province, as a charter flight under the visual flight rules. On board were the pilot-in-command (PIC) and 11 passengers (eight adults and three children). The aircraft was also carrying vegetables. The pilot reported departing Oksapmin at 13:56. The pilot had flight planned, Kiunga to Oksapmin to Kiunga. However, the evidence revealed that without advising Air Traffic Services, the pilot flew from Oksapmin to Tekin. On departure from Tekin the pilot transmitted departure details to ATS, stating departure from Oksapmin. The recorded High Frequency radio transmissions were significantly affected by static and hash. The weather at Kiunga was reported to be fine. As the aircraft entered the Kiunga circuit area, the pilot cancelled SARWATCH with Air Traffic Services (ATS). The pilot did not report an emergency to indicate a safety concern. Witnesses reported that during its final approach, the aircraft suddenly pitched up almost to the vertical, the right wing dropped, and the aircraft rolled inverted and rapidly “fell to the ground”. It impacted the terrain about 1,200 metres west of the threshold of runway 07. The impact was vertical, with almost no forward motion. The aircraft was destroyed, and all occupants were fatally injured.
Probable cause:
The aircraft’s centre of gravity was significantly aft of the aft limit. When landing flap was set, full nose-down elevator and elevator trim was likely to have had no effect in lowering the nose of the aircraft. Unless the flaps had been retracted immediately, the nose-up pitch may also have resulted in tail plane stall, exacerbating the pitch up. The wings stalled, followed immediately by the right wing dropping. Recovery from the stall at such a low height was not considered possible.
Other factors:
Other factors is used for safety deficiencies or concerns that are identified during the course of the investigation, that while not causal to the accident, nevertheless should be addressed with the
aim of accident and serious incident prevention, and the safety of the travelling public.
a) Following the reweighing of SBC, the operator did not make adjustments to account for the shift of the moment arm as a result of the reweighing. Specifically, a reduction of allowable maximum weight in the baggage compartment.
b) The pilot, although signing the flight manifest on previous flights attesting that the aircraft was loaded within c of g limits, had not computed the c of g. No documentation was available to confirm that the pilot had computed the c of g for the accident flight, or any recent flights.
c) All of the High Frequency radio transmissions between Air Traffic Services and SBC were significantly affected by static interference and a lot of hash, making reception difficult, and many transmissions unclear and unreadable. This is a safety concern to be addressed to ensure that vital operational radio transmissions are not missed for the safety of aircraft operations, and the travelling public.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 near Port Moresby: 4 killed

Date & Time: Sep 20, 2014 at 0935 LT
Operator:
Registration:
P2-KSF
Survivors:
Yes
Site:
Schedule:
Woitape - Port Moresby
MSN:
528
YOM:
1977
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
19290
Captain / Total hours on type:
5980.00
Copilot / Total flying hours:
432
Copilot / Total hours on type:
172
Aircraft flight hours:
34327
Aircraft flight cycles:
46302
Circumstances:
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.
Probable cause:
The following contributing factors were identified:
- The flight crew continued the descent in instrument meteorological conditions without confirming their position.
- The flight crew’s assessment of their position was incorrect and they had lost situational awareness
- The flight crew deprived themselves of the “Caution” and “Warning” alerts that would have sounded about 20 sec and about 10 sec respectively before the collision, by not deactivating the EGPWS Terrain Inhibit prior to departure from Woitape.
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:

Crash of a Cessna 208B Grand Caravan in Kibeni: 3 killed

Date & Time: Nov 25, 2013 at 1340 LT
Type of aircraft:
Operator:
Registration:
P2-SAH
Survivors:
Yes
Schedule:
Kamusi – Purari – Vailala – Port Moresby
MSN:
208B-1263
YOM:
2007
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2200
Captain / Total hours on type:
800.00
Circumstances:
On 25 November 2013, a Cessna Aircraft Company C208B Grand Caravan, registered P2-SAH and operated by Tropicair, departed Kamusi, Western Province, for Purari River, Gulf Province, at 0312 UTC on a charter flight under the instrument flight rules (IFR). There were 10 persons on board; one pilot and nine passengers . Earlier in the day, the aircraft had departed Port Moresby for Kamusi from where it flew to Hivaro and back to Kamusi before the accident flight. SAH was due to continue from Purari River to Vailala and Port Moresby. The pilot reported that the takeoff and climb from Kamusi were normal and he levelled off at 9,000 ft and completed the top-of-climb checklist. Between Kamusi and Purari River the terrain is mostly flat and forest covered, with areas of swampland and slow-moving tidal rivers. Habitation is very sparse with occasional small villages along the rivers. The pilot recalled that the weather was generally good in the area with a cloud base of 3,000 ft and good visibility between build-ups. The pilot reported that approximately 2 minutes into the cruise there was a loud ‘pop’ sound followed by a complete loss of engine power. After configuring the aircraft for best glide speed at 95 kts, the pilot turned the aircraft right towards the coast and rivers to the south, and completed the Phase-1 memory recall items for engine failure in flight. He was assisted by the passenger in the right pilot seat who switched on the Emergency Locator Transmitter (ELT) and at 0332 broadcast MAYDAY due engine failure on the area frequency. Checking the database in the on-board Global Positioning System (GPS), the pilot found the airstrip at Kibeni on the eastern side of the Palbuna River. The pilot, assisted by the passenger next to him, tried unsuccessfully to restart the engine using the procedure in the aircraft’s Quick Reference Handbook (QRH). The passenger continued to give position reports and to communicate with other aircraft. At about 3,000 ft AMSL the pilot asked for radio silence on the area frequency so he could concentrate on the approach to Kibeni airstrip, flying a left hand circuit to land in a south westerly direction. He selected full flaps during the final stages of the approach, which arrested the aircraft’s rate of descent, but the higher than normal speed of the aircraft during the approach and landing flare caused it to float and touch down half way along the airstrip. The disused 430 metre long Kibeni airstrip was overgrown with grass and weeds. It was about 60 ft above the river and 120 ft above mean sea level, with trees and other vegetation on the slope down to the river. The aircraft bounced three times and, because the aircraft’s speed had not decayed sufficiently to stop in the available length, the pilot elected to pull back on the control column in order to clear the trees that were growing on the slope between the airstrip and the river. The aircraft became airborne, impacting the crown of a coconut palm (that was almost level with the airstrip) as it passed over the trees. The pilot banked the aircraft hard left in an attempt to land/ditch along the river and avoid trees on the opposite bank. He then pushed forward on the control column to avoid stalling the aircraft and levelled the wings before the aircraft impacted the water. The aircraft came to rest inverted with the cockpit and forward cabin submerged and immediately filled with water. After a short delay while he gained his bearings under water, the pilot was able to undo his harness and open the left cockpit door. He swam to the rear of the aircraft, opened the right rear cabin door, and helped the surviving passengers to safety on the river bank. He made several attempts to reach those still inside the aircraft. When he had determined there was nothing further he could do to reach them, he administered first aid to the survivors with materials from the aircraft’s first aid kit. After approximately 20 minutes, villagers arrived in a canoe and transported the pilot and surviving passengers to Kibeni village across the river. About 90 minutes after the accident, rescuers airlifted the survivors by helicopter to Kopi, located 44 km north east of Kibeni.
Probable cause:
The engine power loss was caused by the fracture of one CT blade in fatigue, which resulted in secondary damage to the remainder of the CT blades and downstream components. The fatigue originated from multiple origins on the pressure side of the blade trailing edge. The root cause for the fatigue initiation could not be determined with certainty. All other damages to the engine are considered secondary to the primary CT blades fracture.
Final Report:

Crash of an ATR42-320F in Madang

Date & Time: Oct 19, 2013 at 0915 LT
Type of aircraft:
Operator:
Registration:
P2-PXY
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Madang – Tabubil – Kiunga
MSN:
87
YOM:
1988
Flight number:
PX2900
Location:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7110
Captain / Total hours on type:
3433.00
Copilot / Total flying hours:
3020
Copilot / Total hours on type:
2420
Aircraft flight hours:
24375
Circumstances:
On 19 October 2013, an Avions de Transport Régional ATR42-320 freighter, registered P2-PXY (PXY) and operated by Air Niugini, was scheduled to fly from Madang to Tabubil, Western Province, as flight PX2900 carrying a load tobacco for a client company. There were three persons on board; the pilot in command (PIC), a copilot, and a PNG experienced DHC-8 captain whose function was to provide guidance during the approach into Tabubil. The PIC was the handling pilot and the copilot was the support monitoring pilot. The flight crew taxied to the threshold end of runway 25 intending to use the full length of the runway. The take-off roll was normal until the PIC tried to rotate at VR (speed for rotation, which the flight crew had calculated to be 102 knots). He subsequently reported that the controls felt very heavy in pitch and he could not pull the control column back in the normal manner. Flight data recorder (FDR) information indicated that approximately 2 sec later the PIC aborted the takeoff and selected full reverse thrust. He reported later that he had applied full braking. It was not possible to stop the aircraft before the end of the runway and it continued over the embankment at the end of the runway and the right wing struck the perimeter fence. The aircraft was substantially damaged during the accident by the impact, the post-impact fire and partial immersion in salt water. The right outboard wing section was completely burned, and the extensively damaged and burnt right engine fell off the wing into the water. Both propellers were torn from the engine shafts and destroyed by the impact forces.
Probable cause:
The following findings were identified:
- The investigation found that Air Niugini’s lack of robust loading procedures and supervision for the ATR 42/72 aircraft, and the inaccurate weights provided by the consignor/client company likely contributed to the overload.
- The mass and the centre of gravity of the aircraft were not within the prescribed limits.
- The aircraft total load exceeded the maximum permissible load and the load limit in the forward cargo zone ‘A’ exceeded the zone ‘A’ structural limit.
- There was no evidence of any defect or malfunction in the aircraft that could have contributed to the accident.
Final Report: