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August 21, 2010 · Hummel / Finberg Ultra Cruiser · N524DF

Canby, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 21, 2010
Injury Outcomes
No injuries (1 uninjured)
Location
Canby, OR
Aircraft
Hummel / Finberg Ultra Cruiser
Tail Number
N524DF
Operator
Finberg Kenneth Dale
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR10LA419

The pilot reported that he was in cruise flight when the engine began to run rough and lose power. Shortly thereafter, the engine lost total power and the pilot maneuvered the airplane to a nearby field to perform a forced landing. Just before touchdown, the airplane collided with a barbed wire fence and subsequently landed hard. Examination and disassembly of the 2-cylinder engine revealed that the right and left cylinder intake valves were not properly seating with the cylinder heads when the valves were in the closed position. The pilot reported this condition would likely cause low cylinder compression and a loss of engine power. No other anomalies were noted with the engine.

NTSB Probable Cause

Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng cyl section-Failure - C

Full Narrative

On August 21, 2010, about 1145 Pacific daylight time, an experimental amateur-built Hummel/Finberg Ultra Cruiser airplane, N524DF, sustained substantial damage following a loss of engine power and subsequent forced landing near Canby, Oregon. The sport pilot, the sole occupant of the airplane, was not injured. The airplane was registered to the pilot and operated as a personal flight under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Mulino State Airport, Mulino, Oregon, at 1140, and was en route to Lenhardt Airpark, Hubbard, Oregon. During a telephone conversation with the National Transportation Safety Board investigator-in-charge, the pilot reported that about 10 minutes after takeoff the engine began to run rough, and lose power. He said he was unable to correct the situation and initiated an off-airport landing to a nearby field. Just before touchdown in the field, the airplane collided with a barbed wire fence and landed hard. The experimental single-seat airplane was powered by a four stoke Globe 2-cylinder horizontally opposed air cooled piston engine, rated at 35 horsepower. Postaccident examination and disassembly of the engine revealed that right and left cylinder intake valves were not properly seating with the cylinder heads when the valves were in the closed position. The pilot reported that this condition would likely cause low cylinder compression and a loss of engine power. No other anomalies were noted with the engine.

Flight

Event TypeAccident
Event Time11:45 PDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHummel / Finberg Ultra Cruiser
Tail NumberN524DF
Aircraft CategoryAir
DamageSubstantial
OperatorFinberg Kenneth Dale
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsGlobe · Reciprocating · 35
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 74 · Sprt · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data