N447PMMICHAEL A HOWARD DOMINATOR2012-06-28 NTSB Accident Report

Substantial
Minor

MICHAEL A HOWARD DOMINATORS/N: 4

Summary

On June 28, 2012, a Michael A Howard DOMINATOR (N447PM) was involved in an accident near Omaha, NE. The accident resulted in 1 minor injury. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this accident to be: A nosewheel shimmy on takeoff, which resulted in the failure of the nosewheel landing gear and a loss of control.

The pilot, who was also the builder, was conducting testing on the newly built gyrocopter. He reported that he spun the rotor up to approximately 110 rpm and was attempting to accelerate the rotor to flight rpm, by going down the runway. The pilot added that he was going about 25 mph when the nosewheel hit a bump in the runway and started to shimmy. He immediately reduced the throttle to slow down; however, the nosewheel strut failed, the craft turned left, and came to rest on its right side. During the rollover, the rotor and fuselage sustained substantial damage.

This accident is documented in NTSB report CEN12CA416. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N447PM.

Accident Details

Date
Thursday, June 28, 2012
NTSB Number
CEN12CA416
Location
Omaha, NE
Event ID
20120703X93512
Coordinates
41.195835, -96.112220
Nearest Airport
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A nosewheel shimmy on takeoff, which resulted in the failure of the nosewheel landing gear and a loss of control.

Aircraft Information

Registration
Make
MICHAEL A HOWARD
Serial Number
4
Engine Type
Reciprocating
Year Built
2011
Model / ICAO
DOMINATORLW20
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HOWARD MICHAEL A
Address
104 S 127 PLAZA
Status
Deregistered
City
OMAHA
State / Zip Code
NE 68154
Country
United States

Analysis

The pilot, who was also the builder, was conducting testing on the newly built gyrocopter. He reported that he spun the rotor up to approximately 110 rpm and was attempting to accelerate the rotor to flight rpm, by going down the runway. The pilot added that he was going about 25 mph when the nosewheel hit a bump in the runway and started to shimmy. He immediately reduced the throttle to slow down; however, the nosewheel strut failed, the craft turned left, and came to rest on its right side. During the rollover, the rotor and fuselage sustained substantial damage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12CA416