Accident Mooney M20R Ovation 3 GX N120GX,
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ASN Wikibase Occurrence # 241113
 
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Date:Wednesday 9 September 2020
Time:09:35 LT
Type:Silhouette image of generic M20P model; specific model in this crash may look slightly different    
Mooney M20R Ovation 3 GX
Owner/operator:DWH LLC
Registration: N120GX
MSN: 29-0459
Year of manufacture:2006
Total airframe hrs:1166 hours
Engine model:Continental IO-550-G(7)B
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Alligator Alley, Broward County, FL -   United States of America
Phase: En route
Nature:Private
Departure airport:Naples, FL (FA37)
Destination airport:Fort Lauderdale-Executive Airport, FL (FXE/KFXE)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot completed a multi-day cross-country trip on the day prior to the accident flight during which he noted an increase in the engine's oil consumption. The purpose of the accident flight was a planned trip for a scheduled oil change, where he also intended to ask the maintainer about the oil consumption. Prior to departing on the accident flight, he performed a preflight inspection and noted that the engine oil level was about 6.5 quarts. While in cruise flight about 20 minutes after departure, the engine lost all power. The pilot performed a successful forced landing to the right shoulder of an interstate highway, where the airplane came to a stop. As the pilot and passenger prepared to disembark, a truck struck the airplane's left wing from behind, resulting in substantial damage to the wing. The pilot reported that the oil level after the accident was between 6 and 6.5 quarts.

A review of data recorded by the airplane's avionics system revealed that during two previous legs of the cross-country trip the oil pressure began to gradually decrease and fluctuate about midway through each flight. During the last leg, the oil pressure decreased continuously throughout the entire flight. During the accident flight, the oil pressure remained in the green range until just prior to the loss of engine power.

During the most recent annual inspection, the engine oil was noted as excessively dirty and contaminants (“gunk') were found in the oil filter pleats. Contaminated oil is commonly caused by an excessive interval between oil changes and/or excessive wear of the piston rings, neither of which appear to have occurred in this case. The oil change intervals were consistently within the manufacturer's specifications and there was no significant loss of cylinder compression (a potential indicator of piston ring wear) noted during the last annual inspection. There were no anomalies noted with the oil and no debris noted in the oil filter during the following oil change, which was the last change before the accident flight.

Although the damage to the engine components was consistent with thermal damage due to a lack of lubrication, given the reported oil quantity after the accident and during the previous trip, as well as the gradual decreases in the recorded oil pressure on the previous flights, it is unlikely that the damage resulted from too little oil in the sump. The gradually decreasing oil pressure during the previous flights suggests a possible problem with the oil pump, an oil leak or restriction, or excessive oil temperature, no evidence of which was found during the examination. It is possible that the overheating and subsequent damage to the bearings began during one of the previous flights when the oil pressure decreased. The reasons for the decreased oil pressure and the increased oil consumption could not be determined.

The engine had never been overhauled, and at the time of the accident had reached just over half of the recommended operating hours between overhauls. However, it was 14 years old, which is 2 years past the recommended calendar time between overhauls. Had the engine been overhauled at the recommended calendar time, it is likely that the issue with the lubricating system could have been addressed or prevented.

Probable Cause: A total loss of engine power because of the overheating and failure of the connecting rod bearings due to a lack of lubrication for reasons that could not be determined.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA20LA327
Status: Investigation completed
Duration: 2 years and 4 months
Download report: Final report

Sources:

NTSB ERA20LA327
FAA register: https://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N120GX

Location

Revision history:

Date/timeContributorUpdates
09-Sep-2020 22:16 Geno Added
10-Sep-2020 02:08 RobertMB Updated [Aircraft type, Source]
10-Sep-2020 02:16 RobertMB Updated [Aircraft type, Departure airport]

Corrections or additions? ... Edit this accident description

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