20000428017999I

Incident · Minor damage

FAA incident report · Cessna T210L · Oakland, CA · April 28, 2000

Date
April 28, 2000 · 15:36 local
Place
Oakland, CA
Airport
Metropolitan Oakland International
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2109S
Reported as
Cessna T210L
Reported engine
Continental TSIO520H
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,500 total1,000 in this make and model3 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)Acft had taken off from petaluma, was in cruise configuration and noticed deteriorating power and manifold pressure. Reported rough running engine, prior to landing safely at oak. Turbo-charger failed, and the number 1 cylinder exhibited classic indications of extreme, detonation, causing engien failure. Further engine teardown inspection are scheduled for further determination of cause. Partial engine teardown and investigation has been on-going, in addition to reviewing fuel contamination possibilities, operator error possibilities, individual component adjustments, settings, and function, etc. Incident report will be amended as necessary to indicate further findings.

As the FAA filed it

(-23)ACFT HAD TAKEN OFF FROM PETALUMA, WAS IN CRUISE CONFIGURATION AND NOTICED DETERIORATING POWER AND MANIFOLD PRESSURE. REPORTED ROUGH RUNNING ENGINE, PRIOR TO LANDING SAFELY AT OAK. TURBO-CHARGER FAILED, AND THE NUMBER 1 CYLINDER EXHIBITED CLASSIC INDICATIONS OF EXTREME, DETONATION, CAUSING ENGIEN FAILURE. FURTHER ENGINE TEARDOWN INSPECTION ARE SCHEDULED FOR FURTHER DETERMINATION OF CAUSE. PARTIAL ENGINE TEARDOWN AND INVESTIGATION HAS BEEN ON-GOING, IN ADDITION TO REVIEWING FUEL CONTAMINATION POSSIBILITIES, OPERATOR ERROR POSSIBILITIES, INDIVIDUAL COMPONENT ADJUSTMENTS, SETTINGS, AND FUNCTION, ETC. INCIDENT REPORT WILL BE AMENDED AS NECESSARY TO INDICATE FURTHER FINDINGS.