LAX07CA262

NTSB accident investigation · Wessel Vortex · Mesa, AZ · September 1, 2007

Accident · No injuriesData collectionFinal report
Date
September 1, 2007, 15:46 local (22:46 UTC)
Place
Mesa, AZ
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N546SWWessel Vortex
Weather
Visual (VMC) · Day
Status
Completed · report November 29, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20070901021709A
Case key
66600

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

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.

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.

Airframe/component/system failure/malfunctionCruise - normal
Exhaust system,muffler - separationCause
Propeller system/accessories,blade - separationCause
Forced landingDescent - emergency
Autorotation - performedPilot in command
On ground/water collision with objectLanding - flare/touchdown
Terrain condition - ravineFactor
Terrain condition - high vegetationFactor

Analysis

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.

Factual 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.

Aircraft

Registration
N546SW
Reported as
Wessel Vortex
Category
Gyroplane, amateur-built
Serial number
MEW061
Engine
Rotax 618, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Marvin E. Wessel, Jr.
Airworthiness certificate
Special, Experimental (Special)
Departed
FFZ · Mesa, AZ
Destination
FFZ · Mesa, AZ
Airport
FFZ · Falcon Field

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
47
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Flight hours
757 total · 66 in this make and model · 36 in the last 90 days · 9 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.