Aircraft Accident/Incident Report

Groveland, California 95321
Monday, May 13, 2002 13:55 PDT

NTSB Narrative Summary Released at Completion of Accident

The airplane collided with multiple trees during an attempted forced landing in mountainous terrain following a catastrophic engine failure in cruise. The flight was obtaining VFR flight following from air route traffic control center (ARTCC) when the facility lost radar and radio contact. The airplane came to rest near the edge of an elliptical meadow, which was about 1 mile long by 1/4 mile wide, with the long axis oriented east and west. The meadow was in mountainous terrain and surrounded by trees over 100 feet tall. The debris path was along the eastern edge of the meadow on a magnetic bearing of 210 degrees. Multiple large trees were observed with broken branches and major impact marks on their trunks. The crankcase had a 3-inch diameter hole in it above cylinder number 3. Examination of the engine found that the crankshaft fractured and separated at the rear of the number 4 cheek. The fracture was at the forward radius of the number 2 main bearing journal. Smeared metal was on the fracture surfaces. A metallurgical examination determined that a large portion of the fracture surface exhibited smooth crack arrest markings typical of fatigue propagation. Failure of the crankshaft was caused by a fatigue crack in the cheek between the number 3 rod journal and the number 2 main bearing journal. The fracture of the crankshaft caused the additional damage to the engine, including the separation of the numbers 3 and 4 connecting rods from their respective journals, and would have led to a complete loss of engine power. The origin of the fatigue fracture was in the transition between the number 2 main bearing journal surface and the forward fillet radius, approximately 0.036 inches below the surface of the journal. No metallurgical anomalies or manufacturing process errors were found to explain the fatigue initiation. This failure is very similar to a number of others investigated by the Safety Board's Materials Laboratory in the past, with a fatigue crack initiating just below the hardened case layer. As with many of those previous events, there were no material or microstructural defects that could be identified as the root cause of the fatigue initiation. The crankshaft met design material specifications.

NTSB Probable Cause Narrative

a catastrophic engine failure due to the fatigue fracture and failure of the crankshaft. A factor contributing to the accident was the unsuitable nature of the mountainous terrain for a successful forced landing. The precipitating cause of the fatigue fracture could not be determined.

Event Information

Type of Event Accident
Event Date 5/13/2002
Event Day of the Week Monday
Time of Event 1355
Event Time Zone Pacific Daylight Time
Event City GROVELAND
Event State CALIFORNIA
Event Country --
Zipcode of the event site 95321
Event Date Year 2002
Event Date Month 5
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 375021N
Event Location Longitude 1195129W
Event Location Airport --
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness Not pertinent
Investigator's weather source Weather Observation Facility
Time of the weather observation 1353 Pacific Daylight Time
Direction of event from weather observation facility (degrees) 245
Weather Observation Facility ID MOD
Elevation of weather observation facility 97
Distance of event from weather observation facility (units?) 55
Time Zone of the weather observation PDT
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 27
Dew Point at event time (in degress fahrenheit) -1
Wind Direction (degrees magnetic) 330
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 3
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.06
Density Altitude (feet) 1350
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Fatal
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal 2
Injury Total Minor --
Injury Total None --
Injury Total Serious --
Injury Total All 2
Investigating Agency NTSB
NTSB Docket Number (internal use) 19361
NTSB Notification Source
NTSB Notification Date May 13 2002 12:00AM
NTSB Notification Time 1604
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Mar 28 2006 1:55PM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office FAA-FAT-Flight Standards District Office

Aircraft Involved

Aircraft #1

Aircraft Registration Number N761LX
NTSB Number LAX02FA163
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed None
Flight plan Was Activated? No
Damage Destroyed
Aircraft Fire Ground
Aircraft Explosion Ground
Aircraft Manufacturer's Full Name Cessna
Aircraft Model T210M
Aircraft Series Identifier --
Aircraft Serial Number 21062351
Certified Max Gross Weight 3600
Aircraft Category Airplane
Aircraft Registration Class U.S. Registered/U.S. Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 6
Number of Engines 1
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Annual
Date of Last Inspection Jul 1 2001 12:00AM
Airframe hours since last inspection 23
Airframe Hours 1920
ELT Installed Yes
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name R. P. WEDDELL & SONS
Aircraft Owner Street Address --
Aircraft Owner City CARSON CITY
Aircraft Owner State NV
Aircraft Owner Country USA
Aircraft Owner Zipcode 89706
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City --
Operator State --
Operator Country --
Operator Zip code --
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) Personal
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code FUL
Departure City FULLERTON
Departure State CA
Departure Country USA
Departure Time 1130
Departure Time Zone PDT
Destination Same as Local Flt --
Destination Airport Code CXP
Destination City CARSON CITY
Destination State NV
Destination Country USA
Specific Phase of Flight Cruise
Report sent to ICAO? No
Evacuation occurred No
Date of most recent change to record Dec 31 2005 1:26PM
User who most recently changed record COOS
Since inspection or accident --
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --