Crash of a Piper PA-46-350P Malibu off Mayport: 2 killed

Date & Time: Dec 20, 2018 at 0904 LT
Registration:
N307JM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Kissimmee - Princeton
MSN:
46-36253
YOM:
2000
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
390
Captain / Total hours on type:
30.00
Aircraft flight hours:
3785
Circumstances:
The aircraft impacted the Atlantic Ocean near Mayport, Florida. The private pilot and pilot-rated passenger were fatally injured. The airplane was destroyed. The airplane was privately owned and operated under the provisions of Title 14 Code of Federal Regulations Part 91. Instrument meteorological conditions prevailed at the time and the flight was operating on an instrument flight rules (IFR) flight plan. The personal flight originated from Kissimmee Gateway Airport, Orlando, Florida, about 0821, and was destined for Princeton Airport, Princeton/Rocky Hill, NJ. According to preliminary air traffic control radar and voice data provided by the Federal Aviation Administration (FAA), at 0859:02, one of the airplane's occupants contacted the Jacksonville Air Route Traffic Control Center (ZJX ARTCC) R-73 sector controller and reported passing through Flight Level (FL) 220 for FL230. The controller advised the pilot there were moderate and some heavy precipitation along the route of flight extending for 200 nautical miles. The occupant acknowledged the controller and advised they would be watching the weather. FAA radar data indicated at 0900:22 the flight reached FL227. Preliminary review of weather data revealed that this altitude was above the freezing level, and at that time the flight entered an area of weather radar returns with intensities between 10 to 30 dBZ (which equated to light to moderate precipitation). While in the weather radar-indicated precipitation, the flight climbed to FL230. At 0902:14, while at the edge of the precipitation, the airplane started a slight left turn before entering a right turn at 0902:28 at FL226. The turn had not been directed by the controller or announced by either occupant. Between 0902:28 and 0903:10, the airplane descended from FL226 to FL202. At 0903:10, the airplane was descending through FL202 when the controller attempted to contact the flight, but there was no reply. The controller attempted to communicate with the flight several more times, and at 0903:27 in response to one attempt, while at 14,500 feet mean sea level (msl), an occupant advised, "were not ok we need help." The controller asked the pilot if he was declaring an emergency and "whats going on." At 0903:35, while at 12,600 feet msl an occupant stated, "I'm not sure whats happening", followed by, "I have anti-ice and everything." At 0903:40 the controller asked the flight if it could maintain altitude, an occupant responded that they could not maintain altitude. The controller provided vectors to a nearby airport west of their position, but the flight did not reply to that transmission or a subsequent query. At about 0904:32 (which was the last communication from the airplane), while at 3,300 feet msl, an occupant advised the controller that the airplane was inverted and asked for assistance. The last radar recorded position with altitude read-out of the flight was at 0904:40, at an altitude of 1,700 feet msl, and 30.40069° north latitude and -81.3844° west longitude. The U.S. Coast Guard initiated a search for the missing airplane, but the wreckage was not located and the search was suspended on December 22, 2018. A privately-funded search for the airplane was initiated and the wreckage was located and recovered on February 6, 2019. The recovered wreckage was retained for further investigation.
Probable cause:
An in-flight loss of control following an encounter with supercooled large droplet icing conditions, which ultimately resulted in an uncontrolled descent and subsequent inflight breakup. Also causal was the pilot’s failure to maintain an appropriate airspeed for flight in icing conditions.
Final Report:

Crash of a Piper PA-46-350P Malibu Mirage in Hurricane

Date & Time: Oct 21, 2018 at 1500 LT
Registration:
N413LL
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hurricane - Salt Lake City
MSN:
46-36413
YOM:
2007
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7000
Captain / Total hours on type:
1500.00
Aircraft flight hours:
1088
Circumstances:
Shortly after takeoff, the pilot smelled smoke. As he began to turn the airplane back to the airport, the engine lost total power. He conducted a forced landing in a field just short of the airport, during which the airplane struck a metal fence and pipe. All occupants egressed, and the pilot then noticed that a fire had erupted under the airplane's engine cowling. Postaccident examination revealed that the airplane sustained fire damage to the roof and forward end of the baggage compartment along with the engine accessory area between the firewall and aft air baffles. Further examination revealed that one of the engine exhaust crossover pipe assemblies was misaligned at the slip joint. An engine manufacturer service bulletin (SB) called for inspections of the exhaust system slip and flange joints to identify misaligned exhaust components. The last maintenance event occurred about 7 1/2 flight hours before the accident, during which the SB was performed and resulted in the replacement of crossover pipes. The mechanic who had performed the most recent maintenance did not follow the correct procedures for reinstallation of the crossover pipe, and the inspector who reviewed his work did not examine the installation as it progressed but instead inspected the pipes after they were installed and essentially hidden from view by their protective heat shield. As a result of the misaligned engine exhaust crossover pipe, hot exhaust gases escaped into the engine compartment and started a fire, which compromised critical engine fuel and oil lines, and resulted in the loss of engine power.
Probable cause:
The mechanic's failure to properly align the engine exhaust crossover pipe during replacement, and his supervisor's failure to properly inspect the installation, which resulted in an in-flight fire and the loss of engine power.
Final Report:

Crash of a Piper PA-46-310P Malibu in Prescott

Date & Time: May 29, 2018 at 2115 LT
Registration:
N148ME
Flight Type:
Survivors:
Yes
Site:
Schedule:
Santa Ana – Prescott
MSN:
46-8608009
YOM:
1986
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3100
Captain / Total hours on type:
3.00
Circumstances:
According to the pilot, about 15 minutes before reaching the destination airport during descent, the engine lost power. The pilot switched fuel tanks, and the engine power was momentarily restored, but the engine stopped producing power even though he thought it "was still running all the way to impact." The pilot conducted a forced landed on a highway at night, and the right wing struck an object and separated from the airplane. The airplane came to rest inverted. According to the Federal Aviation Administration (FAA) aviation safety inspector (ASI) that performed the postaccident airplane examination, the fuel lines to the fuel manifold were dry, and the fuel manifold valves were dry. He reported that the fuel strainer, the diaphragm, and the fuel filter in the duel manifold were unremarkable. Fuel was found in the gascolator. The FAA ASI reported that, during his interview with the pilot, "the pilot changed his story from fuel exhaustion, to fuel contamination." The inspector reported that there were no signs of fuel contamination during the examination of the fuel system. According to the fixed-base operator (FBO) at the departure airport, the pilot requested 20 gallons of fuel. He then canceled his fuel request and walked out of the FBO.
Probable cause:
The pilot's improper fuel planning, which resulted in fuel exhaustion and the subsequent total loss of engine power.
Final Report: