Crash of a Piper PA-46-310P Malibu off Qaqortoq

Date & Time: Jul 29, 2024 at 1333 LT
Operator:
Registration:
D-EOSE
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Goose Bay – Narsarsuaq
MSN:
46-08010
YOM:
1986
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17802
Captain / Total hours on type:
107.00
Aircraft flight hours:
3590
Circumstances:
The crew was returning to Europe after taking part to the AirVenture airshow in Oshkosh. Following a fuel stop in Goose Bay, the crew continued to Narsarsuaq, Greenland. The initial cruise level was FL210, but after a short while, ATC instructed the pilot to descend to FL180. The pilot set the cruise power to 65% (26.5' Manifold Pressure (MP) and 2,400 revolutions per minute (rpm)), and the Fuel Flow (FF) leaned to 14 US gallons per hour (gph) with a Turbine Inlet Temperature (TIT) of 50° Fahrenheit (F) Lean of Peak (LOP). The weather en route was 'nice' and mostly VMC, and the Outside Air Temperature (OAT) at FL180 was approximately -10° to -15° Celsius (C). The pilot contacted Nuuk Information (ATS unit Flight Information Center (FIC) Nuuk) when the aircraft entered Nuuk Flight Information Region (FIR). At 1304LT, in preparation for landing in BGBW, the pilot reported a descent from FL180 to 11,000 feet inbound to the IFR reporting point SIMNI (located at the Greenlandic coastline, 45 nm south-west of BGBW). The pilot initiated a 500 feet per minute descent and kept the cruise power setting at 65%. While passing FL160, the pilot and the passenger briefly noticed an 'unusual, electrical, and not very strong smell'. The cabin altitude started increasing by a rate of 3,000 fpm, and the pilot realized 'something was wrong'. Shortly after, the CABIN ALTITUDE annunciator warning light illuminated, indicating a cabin altitude above 10,000 feet. As the aircraft was below an altitude of 15,000 feet and descending, the pilot considered the time of useful consciousness and opted not to don the oxygen masks. At 1316LT, the pilot declared an urgency situation to Nuuk Information: 'Pan-Pan, Pan-Pan, Pan-Pan. We have an air conditioning problem and a low oil pressure indication'. The MP dropped from 26” to 17-18” and the pilot moved the throttle lever forward without any effect. All Cylinder Head Temperatures (CHT) indicated 'normal and balanced', and the pilot moved the mixture control full forward to the rich position. The engine almost stopped, and the pilot retarded the mixture control back to the previous position. The aircraft pitch was adjusted to obtain the best glide airspeed of 90 knots. At 1317LT, while descending through 12,000 feet, the pilot declared a distress situation to Nuuk Information: 'Mayday, Mayday, Mayday. We have high rpm now and will try to make it to the shore'. The pilot activated the aircraft Emergency Locator Transmitter (ELT). A surveillance aircraft from the RDAF and an inspection ship from the RDN were on patrol in the area. The Danish Armed Forces Arctic Command allocated both to provide assistance. While descending through 7,000 feet altitude, the propeller rpm increased to 3,000 rpm, and 30 seconds later, the oil pressure indicated zero. The pilot pulled back the mixture handle to the idle/cut-off position and stopped the engine to avoid major mechanical damage. The pilot observed on his knee-mounted tablet that the predicted gliding distance of the aircraft fell short of the coastline. At 1326LT, the pilot informed Nuuk Information of the expected ditching position: 60° 30' N 46° 45' W. The pilot and the passenger prepared to ditch by checking the location of the life raft in the cabin, zipping up their survival suits (which they were already wearing up to their waists), and tightening their seat belts. At 1329LT, as the aircraft was passing 3,300 feet descending, the RDAF surveillance aircraft spotted the aircraft gliding on a north-easterly course over a low overcast. At approximately 1,700 feet, the aircraft entered the cloud layer, and exited below at approximately 700 feet. The RDAF surveillance aircraft lost sight of the aircraft as it entered the cloud layer. In order to safely descend below the cloud layer in VMC, the flight crew of the RDAF surveillance aircraft had to fly to the coastline, descend, and fly back towards the expected ditching position below the cloud layer. The visibility below the cloud layer was 'good', and the sea surface had 'only low swells'. At 1333LT, the pilot selected flap setting 2 (20°), slowed down the aircraft to minimum airspeed, and flared the aircraft straight ahead. The aircraft bounced slightly on the sea surface once, before hitting the sea surface a second time. The aircraft decelerated fairly abruptly – 'similar to a hard brake in a car' – and stopped in a wings-level position, floating on the surface. The pilot and the passenger released their seat belts, went into the aft cabin, and opened the top part of the aircraft entrance door, which was above the water level. They manoeuvred the life raft through the entrance door into the water and inflated the raft. The pilot and the passenger threw a few personal items into the raft and stepped directly from the aircraft into the raft. At 1340LT, at position 60° 34' N 46° 50' W, the RDAF surveillance crew spotted the life raft with the pilot and passenger. For the next 45 minutes, the RDAF surveillance aircraft circled overhead the life raft. At approximately 1400LT, the pilot contacted Nuuk FIC via satellite telephone. At 1423LT, a rescue crew in a rigid-hulled inflatable boat (RHIB) dispatched from the RDN inspection ship and picked up the pilot and passenger. The aircraft sank approximately 2 hours after the ditching.
Probable cause:
An engine failure during descent resulted in a ditching off the southwest coast of Greenland. The AIB could not determine the exact cause of the engine failure, but it was likely due to a seeping oil leak.
A combination of the following factors made the accident survivable:
- The pilot declared an urgency followed by an emergency to ATS, and a nearby RDAF surveillance aircraft obtained visual contact with the gliding aircraft.
- The pilot successfully landed the aircraft on calm sea.
- The pilot and the passenger wore survival suits and carried a life raft on board, which they boarded upon safely evacuating the aircraft.
- After 50 minutes, personnel from a nearby RDN inspection ship arrived and rescued the pilot and passenger.
Final Report:

Crash of a Piper PA-46-350P Malibu near Makkovik: 1 killed

Date & Time: May 1, 2019 at 0816 LT
Operator:
Registration:
N757NY
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Goose Bay - Narsarsuaq
MSN:
46-36657
YOM:
2015
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3500
Captain / Total hours on type:
20.00
Copilot / Total flying hours:
1300
Copilot / Total hours on type:
0
Circumstances:
On 01 May 2019 at 0723, the aircraft departed CYYR on a VFR flight plan direct to BGBW. The ferry pilot, who was the pilot-in-command, occupied the left seat while the co-owner occupied the right seat. The aircraft climbed to 2000 feet ASL and proceeded on a direct track to destination. The altitude and heading did not change significantly along the route, therefore it is likely that the autopilot was engaged. At 0816, the aircraft collided with a snow-covered hill 2250 feet in elevation, located 35 nautical miles (NM) southeast of Makkovik Airport (CYFT), Newfoundland and Labrador. The impact happened approximately 200 feet below the top of the hill. The aircraft came to rest in deep snow on steep sloping terrain. The aircraft sustained significant damage to the propeller, nose gear, both wings, and fuselage. Although the cabin was crush-damaged, occupiable space remained. There was no post-impact fire. The ferry pilot was seriously injured and the co-owner was fatally injured. The Joint Rescue Coordination Centre (JRCC) in Halifax received an emergency locator transmitter (ELT) signal from the aircraft at 0823. The ferry pilot carried a personal satellite tracking device, a personal locator beacon (PLB) and a handheld very high frequency (VHF) radio, which allowed communication with search and rescue (SAR). Air SAR were dispatched to the area; however, by that time, the weather had deteriorated to blizzard conditions and aerial rescue was not possible. Ground SAR then deployed from the coastal community of Makkovik and arrived at the accident site approximately 4 hours later because of poor weather conditions and near zero visibility. The ferry pilot and the body of the co-owner were transported to Makkovik by snowmobile. The following day, they were airlifted to CYYR.
Probable cause:
Controlled flight into terrain.
Final Report:

Crash of a Piaggio P.180 Avanti near Kangerlussuaq

Date & Time: Oct 16, 2009 at 1140 LT
Type of aircraft:
Operator:
Registration:
N108GF
Flight Type:
Survivors:
Yes
Schedule:
Kuwait – Antalya – Vienna – Stornoway – Keflavik – Narsarsuaq – Goose Bay – Bangor – Denton
MSN:
1086
YOM:
2004
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
105.00
Aircraft flight hours:
1035
Aircraft flight cycles:
716
Circumstances:
The accident flight was a part of a ferry flight from Kuwait to USA. The flight departed from Keflavik, Iceland with planned destination Narsarsuaq, Greenland. The commander did not get visual contact with the runway on the instrument approach to Narsarsuaq and the flight diverted towards Kangerlussuaq, Greenland. During the flight towards Kangerlussuaq, the amount of fuel became critical low and the aircraft landed on the Greenlandic icecap. The aircraft was destroyed during the landing attempt. The commander suffered minor injuries. The accident occurred in daylight and under visual meteorological conditions (VMC).
Probable cause:
After the flight was airborne from BIKF, the flight was restricted by ATC to cruise at FL200 instead of FL280. The lower flight altitude and the power setting used resulted in a reduction of the final reserve to approximately zero minutes. At that time the commander was not concerned about the final reserve because the flight to BGBW was only a two hours flight and as the aircraft before take-off from BIKF had fuel for more than three hours and 40 minutes of flight. During the approach to BGBW the flight never came below the clouds and was in IMC during the entire final approach. The most likely cause was that the aircraft was not following the NDB DME 07 approach procedure descent profile. Consequently the commander did not get visual contact during the approach and he had to make a missed approach. During the diversion to the alternate aerodrome, BGSF the flight was altitude restricted by ATC to FL190. One engine was intentionally stopped during the diversion to BGSF. The consequence was a reduction of the aircraft range. A shallow descent was initiated approximately 57 minutes before ETA over BGSF. The shallow descent profile did consume more fuel than a steeper descent profile. The commander decided to make a precautionary landing in the terrain. The aircraft was destroyed during the landing attempt on the rugged and bumpy surface of the icecap.
Final Report: