N1025Y

Substantial
Minor

WATERS VORTEX S/N: 022

Accident Details

Date
Wednesday, May 27, 1998
NTSB Number
CHI98LA176
Location
MONROE, WI
Event ID
20001211X10028
Coordinates
42.589763, -89.639015
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

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

Aircraft Information

Registration
N1025Y
Make
WATERS
Serial Number
022
Engine Type
Reciprocating
Year Built
1997
Model / ICAO
VORTEX BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RHEINHARDT WAYNE
Address
4670 BREEZE RD
Status
Deregistered
City
MOUNT VERNON
State / Zip Code
IN 47620-7136
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA176