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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

September 30, 2007 · Fokker VI · UNREG

Morristown, TN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 30, 2007
Injury Outcomes
1 injury (1 serious injury)
Location
Morristown, TN
Aircraft
Fokker VI
Tail Number
UNREG
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
NYC07LA243

The pilot was conducting a test flight of the unregistered amateur-built Fokker VI airplane, prior to registering it. While on the downwind leg of the traffic pattern, the pilot noticed that the engine "was not making proper power" and he subsequently performed a forced landing, during which the airplane was substantially damaged. Examination of the engine revealed no evidence of any preimpact mechanical anomalies.

NTSB Probable Cause

A loss of engine power for undetermined reasons during approach.

Full Narrative

On September 30, 2007, at 1940 eastern daylight time, an unregistered amateur-built Fokker VI was substantially damaged during a forced landing in Morristown, Tennessee. The certificated private pilot was seriously injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local test flight conducted under 14 Code of Federal Regulations Part 91. According to the pilot, he was conducting a test flight of the experimental airplane, prior to registering it. While on the downwind leg of the traffic pattern, the engine "was not making proper power" and "did not sound right." The pilot realized he would not make it to the runway, and performed a forced landing to a field, during which the airplane was substantially damaged. The airplane was equipped with a Two Stroke International engine. Examination of the engine by a Federal Aviation Administration (FAA) inspector revealed continuity within the fuel system, and the fuel pump was tested with no anomalies noted. The carburetor was observed "loose from the engine;" however, the separation was consistent with impact damage. The carburetor was disassembled and no anomalies were noted with the butterfly valve. The engine crankshaft was rotated at the propeller flange, and valve train continuity and cylinder compression were confirmed. The weather reported at an airport 31 miles to the northwest, 5 minutes prior to the accident, included calm winds, clear skies, temperature 21 degrees Celsius, dew point 6 degrees Celsius, and an altimeter setting of 30.34 inches of mercury.

Flight

Event TypeAccident
Event Time19:40 EDT
Nearest AirportCoopers Field (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftFokker VI
Tail NumberUNREG
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsTwo Stroke International · Reciprocating · 50
Seats1

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 53 · Third Class · Serious

Conditions

ConditionsVMC
LightDusk
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point70 F / 43 C
Altimeter30.34 inHg
Observation Time23:35
Weather SourceWFAC

Appendix: Source Data