N29HTHUNT SPARROWHAWK2011-10-15 NTSB Accident Report

Substantial
Minor

HUNT SPARROWHAWKS/N: HA1

Summary

On October 15, 2011, a Hunt SPARROWHAWK (N29HT) was involved in an accident near Blair, 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: The pilot/builder’s inadequate installation of a nosewheel steering component, which resulted in a shimmy and a loss of directional control during the takeoff roll.

The pilot/builder was planning a short flight above the runway for the purpose of testing the newly built gyrocopter. During the takeoff roll, the nose wheel experienced a shimmy and the pilot was unable to maintain directional control. The gyrocopter rolled onto its left side and exited the side of the runway before coming to rest in the grass. During the rollover, the main rotor mast was substantially damaged. A postaccident examination of the gyrocopter revealed a loose bolt in the nose gear steering linkage which allowed the nose wheel to shimmy.

This accident is documented in NTSB report CEN12CA029. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N29HT.

Accident Details

Date
Saturday, October 15, 2011
NTSB Number
CEN12CA029
Location
Blair, NE
Event ID
20111019X01446
Coordinates
41.408889, -96.105278
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/builder’s inadequate installation of a nosewheel steering component, which resulted in a shimmy and a loss of directional control during the takeoff roll.

Aircraft Information

Registration
Make
HUNT
Serial Number
HA1
Model / ICAO
SPARROWHAWK

Registered Owner (Historical)

Name
HUNT DANIEL E
Address
1395 COREY DR
Status
Deregistered
City
BLAIR
State / Zip Code
NE 68008-2762
Country
United States

Analysis

The pilot/builder was planning a short flight above the runway for the purpose of testing the newly built gyrocopter. During the takeoff roll, the nose wheel experienced a shimmy and the pilot was unable to maintain directional control. The gyrocopter rolled onto its left side and exited the side of the runway before coming to rest in the grass. During the rollover, the main rotor mast was substantially damaged. A postaccident examination of the gyrocopter revealed a loose bolt in the nose gear steering linkage which allowed the nose wheel to shimmy.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12CA029