CHI98LA176

NTSB accident investigation · Waters Vortex · Monroe, WI · May 27, 1998

Accident · Minor injuriesLimited investigationFinal report
Date
May 27, 1998, 11:35 local (16:35 UTC)
Place
Monroe, WI
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1025YWaters Vortex
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 2001
Report
Approved by Office Director
FAA report
19980527011029A
Case key
10893

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

the pilot's failure to maintain rotor RPM. A factor associated with the accident was the soft terrain on which the gyrocopter touched down.

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.

Miscellaneous/otherCruise - normal
Rotor rpm - not maintainedPilot in commandCause
Forced landingEmergency descent/landing
Roll overLanding - flare/touchdown
Terrain condition - softFactor

Analysis

The pilot stated that shortly after departure while at about 1,200 feet above ground level, he felt the gyroplane slowing down and he noticed a loss of rotor RPM. He initiated an emergency descent and elected to land straight ahead in a cultivated field. The pilot initiated a 180 degree turn to avoid tree and the gyroplane descended to impact with the terrain. The left landing gear dug into the soft plowed field and the gyroplane rolled over onto its left side. Post accident inspection of the gyroplane failed to reveal any mechanical failure and/or malfunction which would have prevented normal operation. The pilot installed a pre-rotor system on the gyroplane the weekend before the accident.

Factual narrative

On May 27, 1998, at 1135 central daylight time (cdt), a Waters Vortex gyroplane, N1025Y, impacted the terrain during a forced landing after losing rotor rpm while en route to a private landing strip in Davis, Illinois. The pilot received minor injuries and the aircraft sustained substantial damage. The aircraft was being operated as a personal flight under 14 CFR Part 91 when the accident occurred. The flight originated in Monroe, Wisconsin, at 1125 cdt. Visual meteorological conditions prevailed at the time and no flight plan was filed.

The pilot stated that shortly after departure from Monroe Municipal Airport while at about 1,200 feet above ground level, he felt the gyroplane slowing down and he noticed a loss of rotor RPM. He initiated an emergency descent and elected to land straight ahead in a cultivated field. The pilot said he realized he was not going to clear the trees. He initiated a left 180 degree turn and continued his descent to where the gyroplane impacted the terrain.

The pilot reported that the left landing gear dug into the soft plowed field and the aircraft rolled over onto its left side.

Post accident inspection of the gyroplane by Inspectors from the Federal Aviation Administration's Milwaukee Flight Standards District Office failed to reveal any mechanical failure and/or malfunction of the gyroplane or the engine which would have prevented normal operation. The pilot installed a pre-rotor system on the gyroplane the weekend before the accident. Post accident inspection of the pre-rotor system failed to reveal any anomalies.

Aircraft

Registration
N1025Y
Reported as
Waters Vortex
Category
Gyroplane, amateur-built
Serial number
022
Airframe hours
10
Engine
Rotax 582, 67 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Clyde E. Waters
Airworthiness certificate
Special, Experimental (Special)
Departed
EFT

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
70
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
2,360 total

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 5 knots
Visibility
10 statute miles
Lowest ceiling
10,000 ft broken
Temperature
72 °F, dew point 55 °F
Altimeter
30.00 inHg
Observed at
EFT, 4 nm away

FAA reports on this event · 1

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