ASN Wikibase Occurrence # 199327
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Friday 1 September 2017 |
Time: | 16:10 LT |
Type: | Cessna U206G Stationair |
Owner/operator: | Waters Aero-marine Inc |
Registration: | N4615X |
MSN: | U20605513 |
Year of manufacture: | 1979 |
Total airframe hrs: | 7359 hours |
Engine model: | Continental IO-520F |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Cumberland County, NE of Harpswell, ME -
United States of America
|
Phase: | Landing |
Nature: | Ferry/positioning |
Departure airport: | Rockland-Knox County Regional Airport, ME (RKD/KRKD) |
Destination airport: | Portland International Jetport, ME (PWM/KPWM) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot reported that, while en route to his destination, he heard a 'loud bang,' followed by a complete loss of engine power. After determining that the airplane was not within gliding distance of the nearest airport, the pilot performed an off-airport landing, during which the airplane impacted a small drainage ditch, nosed over, and came to rest inverted, resulting in substantial damage.
Disassembly of the engine revealed mechanical damage in multiple locations inside the crankcase. The No. 1 main bearings had shifted slightly out of the support and displayed deformation. The No. 2 main bearings displayed bearing shift signatures. One was missing, and the other had extruded out of the bearing support. Multiple pieces of the missing bearing were found in the oil sump. The No. 3 main bearings were intact and had moved in a clockwise direction when viewed from the back of the engine, had shifted slightly out of the support, and the oil passage holes were partially blocked. The crankshaft was fractured at the crankshaft cheek between the No. 2 main journal and the No. 2 connecting rod journal. The No. 2 connecting rod journal and connecting rod bearings displayed incipient signatures of lubrication distress.
Review of the engine maintenance records revealed that, about 500 flight hours before the accident, all the cylinders had been replaced with overhauled cylinders and new pistons had been installed along with reconditioned lifters and seals.
If a bearing shifts for any reason after removal of one or more cylinders, or during replacement of one or more cylinders, the oil holes in the bearing can become misaligned with the oil passages in the crankcase, partially cutting off the oil supply to the bearing. If the engine is then put back into service, the reduced oil supply to the bearing can cause increased heat and friction that can result in the bearing shifting more, further reducing its oil supply. Eventually, the bearing can shift enough to cause the oil supply to be cut off completely, resulting in a catastrophic failure. This is usually referred to as a "spun bearing."
To prevent a spun bearing, the manufacturer specified a multiple-step torquing process for proper cylinder installation. The process required that the through bolt nuts be torqued on both sides of the engine, even if only one cylinder was being installed. The manufacturer warned that "failure to torque through bolt nuts on both sides of the engine can result in a loss of main bearing crush with main bearing shift and subsequent engine failure." Given the observed damage, it is likely that maintenance personnel did not apply sufficient torque to the cylinder flange nuts and through bolts during installation of the cylinders, which resulted in shifting of the Nos. 1, 2, and 3 main bearings, a loss of lubrication, and failure of the crankshaft.
Probable Cause: A total loss of engine power due to maintenance personnel's failure to apply proper torque to the cylinder flange nuts and through bolts, which resulted in shifting of the Nos. 1, 2, and 3 main bearings, loss of lubrication, and failure of the crankshaft.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | ERA17LA307 |
Status: | Investigation completed |
Duration: | 4 years and 4 months |
Download report: | Final report |
|
Sources:
NTSB ERA17LA307
FAA register:
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=4615X
History of this aircraft
Other occurrences involving this aircraft
6 October 2017 |
N4615X |
Penobscot Island Air |
0 |
Brunswick Executive Airport, Cumberland County, ME |
|
sub |
Location
Revision history:
Date/time | Contributor | Updates |
02-Sep-2017 05:38 |
Geno |
Added |
02-Jul-2022 18:36 |
ASN Update Bot |
Updated [Time, Operator, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative, Category, Accident report] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation