LAX93FA042

NTSB accident investigation · Cessna TU-206F · Clearlake, CA · November 16, 1992

Accident · FatalField investigationFinal report
Date
November 15, 1992, 16:51 local (Nov 16, 1992, 00:51 UTC)
Place
Clearlake, CA
Injuries
2 fatal, 1 serious
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N51198Cessna TU-206F
Weather
Visual (VMC) · Dusk
Status
Completed · report September 28, 1993
Report
Approved by Office Director
FAA report
19921115046569A
Case key
27810

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The exhaust valve failing due to a complete fracture which resulted in the total lose of engine power. Factors in this accident were: 1) the terrain not being suitable for a forced landing, and 2) low ambient light which hampered the pilot's ability to see the terrain.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise - normal
Engine assembly,valve,exhaust - fracturedCause
Engine assembly,valve,exhaust - failure,totalCause
Forced landingDescent - emergency
In flight collision with terrain/waterDescent - emergency
Light condition - duskFactor
Terrain condition - none suitableFactor
Terrain condition - mountainous/hillyFactor

Analysis

The pilot and his two passengers were in cruise flight on a VFR cross country when the airplane's engine suddenly began to run rough. The pilot, who was being flight followed by an FAA center, declared an emergency and requested vectors to a nearby airport. Within about 2 minutes the pilot reported that the engine completely quit. The pilot entered a power off forced landing and collided with hilly terrain. No suitable terrain was available for the forced landing and the lighting conditions were reported as 'dusk to dark.' The pilot and one of his passengers received fatal injuries. An off site examination and teardown of the engine revealed that the number 5 cylinder exhaust valve stem broke just above the valve head. The valve head fell into the cylinder and the action of the piston caused a hole to be broken through the piston center crown structure. The valve head was found wedged between the crankcase structure and the crankshaft, preventing crankshaft rotation.

Aircraft

Registration
N51198
Reported as
Cessna TU-206F
Category
Airplane
Serial number
U20601977
Airframe hours
5,746
Engine
Continental TSIO-520-C, 285 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Falcon Aerial
Registered owner
Falcon Aerial
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 16, 1992 · 60 hours before
Departed
STS · Santa Rosa, CA
Destination
CIC · Chico, CA

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
1,920 total

Weather

Conditions
Visual (VMC) · Dusk
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N51198 · 1

Matched to the same aircraft by N-number and date.