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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 1, 2007 · Wessel Vortex · N546SW

Mesa, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 1, 2007
Injury Outcomes
No injuries (1 uninjured)
Location
Mesa, AZ
Aircraft
Wessel Vortex
Tail Number
N546SW
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX07CA262

The gyrocopter collided with high vegetation and rough terrain during a forced autorotation following the in-flight separation of a propeller blade. The pilot reported that the muffler's mounting strap broke during cruise flight, which caused one composite pusher propeller blade to separate. The pilot autorotated to a forced landing in a ravine. During touchdown the gyrocopter rolled over upon impacting 5-foot-high bushes.

NTSB Probable Cause

Failure of the muffler's mounting strap and subsequent loss of engine power due to propeller blade separation during cruise flight. A contributing factor was the unsuitable terrain for a forced landing.

Full Narrative

On September 1, 2007, about 1546 mountain standard time, an experimental Wessel Vortex, N546SW, made a forced landing in rough terrain about 4 miles north of the Falcon Field airport, Mesa, Arizona. The private pilot was the owner and operator of the homebuilt gyrocopter, and it was substantially damaged upon rolling over during impact with 5-foot-high brush in a ravine. The pilot was not injured. Visual meteorological conditions prevailed at the time, and no flight plan had been filed. The personal flight was performed under the provisions of 14 CFR Part 91, and it originated from Mesa about 1445. The pilot reported to the National Transportation Safety Board investigator that during cruise flight he heard a loud noise and felt a vibration. Thereafter, the rotorcraft lost power when one of the pusher propeller blades separated, and he autorotated. The pilot additionally reported an examination of the engine assembly revealed that the muffler's mounting strap had failed, and this event resulted in the subsequent separation of one composite propeller blade.

Flight

Event TypeAccident
Event Time15:46 MST
Nearest AirportFalcon Field (4nm)
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftWessel Vortex
Tail NumberN546SW
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 618 · Reciprocating

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 47 · Third Class

Conditions

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

Appendix: Source Data