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Aviation safety reports, made easier to study

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June 14, 2008 · Fetherolf CH-701 · N813DJ

Newton Falls, OH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 14, 2008
Injury Outcomes
No injuries (1 uninjured)
Location
Newton Falls, OH
Aircraft
Fetherolf CH-701
Tail Number
N813DJ
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI08CA165

The pilot reported he had been flying for approximately 15 minutes when he decided to land. The airplane was on downwind for the runway, abeam the threshold, when the engine "sputtered then quit." The pilot switched fuel tanks, and turned on the electric fuel boost pump; however, he was unsuccessful in restoring engine power. At that point, the airplane was outside of gliding distance to the runway, and the pilot made a forced landing to a wooded area short of the runway. A postaccident inspection revealed that the left fuel tank vent was obstructed. The obstruction appeared to be sealant used in the assembly of the tank. The pilot noted that the vent design will be changed to reduce the possibility of a blockage, and the preflight checklist will be revised to specifically verify that the vents are clear prior to flight.

NTSB Probable Cause

The loss of engine power during the landing approach due to fuel starvation resulting from an obstructed fuel tank vent. Factors contributing to the accident were the lack of suitable terrain for a forced landing, and the airplane's low altitude at the time of the power loss.

Full Narrative

The pilot reported he had been flying for approximately 15 minutes when he decided to land. The airplane was established on downwind for runway 1 (3,500 feet by 30 feet, asphalt), abeam the threshold, when the engine "sputtered then quit." The pilot switched fuel tanks and turned on the electric fuel boost pump; however, he was unsuccessful in restoring engine power. At that point, the airplane was outside of gliding distance to the runway. The pilot subsequently executed a forced landing to a wooded area short of the runway. A post accident inspection revealed that the left fuel tank vent was obstructed. The obstruction appeared to be sealant used in the assembly of the tank. The pilot noted that the vent design will be changed to reduce the possibility of a blockage, and the preflight checklist will be revised to specifically verify that the vents are clear prior to flight.

Flight

Event TypeAccident
Event Time15:30 EDT
Nearest AirportBraceville (0nm)
Runway1
Runway Length3000 ft
Runway Width30 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftFetherolf CH-701
Tail NumberN813DJ
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsSubaru · EA-81 · Reciprocating · 80
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 46 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind320° @ 6 kt
Visibility9 sm
CeilingBroken clouds 9000 ft
Temperature / Dew Point64 F
Altimeter29.97 inHg
Observation Time19:37
Weather SourceWFAC

Appendix: Source Data