ANC92LA152

NTSB accident investigation · Cessna 206 · Fort Yukon, AK · September 2, 1992

Accident · Serious injuriesLimited investigationFinal report
Date
September 1, 1992, 17:42 local (Sep 2, 1992, 01:42 UTC)
Place
Fort Yukon, AK
Injuries
1 serious, 1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8070ZCessna 206
Weather
Visual (VMC) · Day
Status
Completed · report December 16, 1993
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19920901035009A
Case key
5796

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

Fatigue failure of an engine cylinder precipitated by the pilot-in-command intentionally exceeding the engine performance ratings in order to sustain flight in the grossly overweight condition. A factor contributing to the accident was the high grass. A factor contributing to the severity of the passenger's injury was the unsecured cargo.

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(partial) - mech failure/malfCruise - normal
Aircraft weight and balance - exceededPilot in commandCause
Engine assembly,cylinder - overtemperatureCause
Powerplant controls - improper use ofPilot in commandCause
Engine assembly,cylinder - fatigueCause
Forced landingLanding - flare/touchdown
Nose overLanding - roll
Terrain condition - high vegetationFactor
Tie down - not performedPilot in commandFactor

Analysis

The pilot loaded the 2 passengers and gear in the airplane to the extent that it took successive attempts to close the door due to the gear which 'filled up the airplane to the roof.' The rear pax had to lay on top of meat and camp supplies with 2 dogs in his lap. The airplane was estimated to be 772 lbs over max gross weight at takeoff. After takeoff the airplane climbed slowly for aprx 55 min at takeoff power. A 'sledgehammer' sound preceded the appearance of oil flowing into the cabin area. No reduction of power was observed. The oil pressure began dropping rapidly, and the pilot made a precautionary landing on a beach. The airplane nosed over in grass. Engine teardown examination revealed that the #6 cylinder had failed through the head-to-barrel threaded joint. Metallurgical examination revealed that the failure was the result of fatigue cracking in the cylinder head casting. This type of failure occurs when the cylinder is operated at elevated temperatures (above maximum allowable) for a considerable period of time.

Aircraft

Registration
N8070Z
Reported as
Cessna 206
Category
Airplane
Serial number
U206-0470
Engine
Continental IO-520A, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Operator
Larry R. Rivers
Registered owner
Larry R. Rivers
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 2, 2000 · 35 hours before
Departed
Red Sheep Creek, AK

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
44
Certificate
Private
Airplane ratings
Single-engine sea, Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Flight hours
4,900 total · 720 in this make and model · 4,830 as pilot in command · 155 in the last 90 days · 148 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
50 statute miles
Lowest ceiling
7,000 ft overcast
Temperature
50 °F, dew point -0 °F

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 N8070Z · 1

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