# Accident 20001116025349A: Cessna 210K, Oxnard, CA, November 16, 2000 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: November 16, 2000, 15:40 local time - Place: Oxnard, CA - Airport: Oxnard Airport - Damage: Substantial damage - Phase of flight: Fcd/Prec Ldg From Cruise - Operating rules: General operating rules (Part 91) - Location: 34.1905° N, 119.1705° W: From the FAA, an estimate near the named town, within about 3 miles - Nearby events: https://openairdocs.org/map.md?lat=34.1905&lon=-119.1705&mi=10 - Aircraft: N8118G (not matched to a registry record) - Reported make and model: CESSNA 210K - Reported engine: CONT IO550* - People aboard: 2 - Fatal injuries: 0 - Pilot flight hours: 600 total, 300 in this make and model - NTSB investigation: [NTSB LAX01LA043](https://openairdocs.org/ntsb/LAX01LA043) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/20001116025349A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (-23) ON NOVEMBER 16, 2000, AT ABOUT 1830 I VISITED VENTURA FAIR GROUNDS, CA. TO INVESTIGATE THE ACCIDENT OF A CESSNA 210K, N8118G, THAT LOST ENGINE POWER AND MADE A FORCED LANDING. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE, HOWEVER, THE CERTIFIED PRIVATE PILOT, HIS PASSENGER, AND TWO DOGS WERE NOT INJURED. NO ONE ON THE GROUND RECEIVED ANY INJURIES. APART FROM THE AIRPLANE, ONLY THE FENCE WAS DAMAGED. THE PLANE WAS OPERATED BY THE PILOT/OWNER AS A PERSONAL FLIGHT UNDER TITLE 14 CFR PART 91 WHEN THE ACCIDENT OCCURRED. THE FLIGHT ORIGINATED FROM CHINO, CA. AIRPORT AT 1505. VMC PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED. AS THE AIRPLANE TOUCHDOWN, THE PILOT APPLIED BRAKES. THE AIRPLANE SKIDDED BEFORE STRIKING THE FENCE AND CAME TO A STOP. THE FAILED ENGINE WAS CONTINENTAL REMANUFACTURED IO-550. IT HAD ABOUT 57 HOURS SINCE REMANUFACTURED BY CONTINENTAL. IT REPLACED THE ORIGINAL ENGINE IO-520 AND ITS INSTALLATION WAS AUTHORIZED BY STC. THE ENGINE WAS SENT TO CONTINENTAL ALABAMA FOR INVESTIGATION BY THE NTSB & CONTINENTAL REPRESENTATIVE. (.4) ON NOVEMBER 16, 2000, AT 1540 HOURS PACIFIC STANDARD TIME, A CESSNA 210K, N8118G, LOST ENGINE POWER AND MADE A FORCED LANDING NEAR OXNARD, CALIFORNIA. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE; HOWEVER, THE CERTIFICATED PRIVATE PILOT, HIS PASSENGER, AND TWO DOGS WERE NOT INJURED. THE AIRPLANE WAS BEING OPERATED BY THE PILOT/OWNER AS A PERSONAL FLIGHT UNDER 14 CFR PART 91 WHEN THE ACCIDENT OCCURRED. THE FLIGHT ORIGINATED FROM THE CHINO, CALIFORNIA, AIRPORT AT 1505. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED THAT HE HAD BEGUN HIS DESCENT FROM HIS EN ROUTE CRUISE ALTITUDE OF 10,500 FEET MEAN SEA LEVEL (MSL) WHEN, AFTER DESCENDING ABOUT 400 TO 500 FEET, HE FELT A MINOR CONCENTRIC VIBRATION. HE IMMEDIATELY CHECKED ENGINE OIL PRESSURE AND FUEL MIXTURE, AND DETERMINED THAT BOTH WERE WITHIN LIMITS. SHORTLY THEREAFTER, THE VIBRATION INCREASED IN MAGNITUDE AND HE REDUCED THE THROTTLE. AT THIS TIME HE ALSO RICHENED THE MIXTURE, SWITCHED FUEL TANKS, AND TRIED TO ADJUST THE PROPELLER PITCH IN HOPES OF SOMEHOW REDUCING THE VIBRATION. THE PILOT DECLARED AN EMERGENCY TO LOS ANGELES CENTER AND WAS GIVEN A HEADING OF 140 DEGREES TO THE NEAREST AIRPORT, WHICH WAS AT OXNARD. AFTER TURNING TO THE NEW HEADING, THE ENGINE QUIT. HE INFORMED CENTER THAT HE WOULD NOT BE ABLE TO REACH OXNARD. ABOUT 5,200 FEET MSL, THE PILOT SAW AN OPEN AREA AND SET UP A NORMAL TRAFFIC PATTERN APPROACH. WHEN HE WAS SURE THAT LANDING WAS ASSURED, HE ATTEMPTED TO LOWER HIS LANDING GEAR AND APPLIED FULL FLAPS. HE ESTIMATED HIS FINAL APPROACH WAS A LITTLE FAST, ABOUT 90 TO 100 KNOTS. HE ATTRIBUTED THE HIGHER SPEED TO THE FACT THAT HE DOVE THE AIRPLANE SLIGHTLY SINCE IT WAS STILL TOO HIGH DURING THE TURN TO FINAL. AS THE AIRPLANE TOUCHED DOWN, THE PILOT APPLIED THE BRAKES. THE AIRPLANE SKIDDED ABOUT 300 TO 400 FEET BEFORE STRIKING A PERIMETER FENCE AND A TREE. AS THE AIRPLANE STRUCK THE TREE, IT YAWED ABOUT 90 DEGREES TO THE RIGHT AND CAME TO A STOP. THE AIRPLANE HAD ITS ENGINE REPLACED THE PREVIOUS MAY. THE NEW ENGINE WAS A FACTORY REMANUFACTURED CONTINENTAL IO-550. IT REPLACED THE ORIGINAL CONTINENTAL IO-520, AND ITS INSTALLATION WAS AUTHORIZED UNDER A SUPPLEMENTAL TYPE CERTIFICATE (STC). THE ENGINE WAS TAKEN TO TELEDYNE CONTINENTAL MOTORS, THE MANUFACTURER, IN MOBILE, ALABAMA, FOR DISASSEMBLY AND INSPECTION. THE ENGINE WAS FOUND TO HAVE A BROKEN CAM GEAR. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX01LA043](https://openairdocs.org/ntsb/LAX01LA043), Nov 16, 2000: Cessna 210K (N8118G), Oxnard, CA, substantial damage. Probable cause: Failure of the internal cam gear in the remanufactured engine. A factor was the congested obstacles in the forced landing area. From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.