N8023Y

Substantial
None

Mayfield SparrowhawkS/N: 2003003

Accident Details

Date
Saturday, May 14, 2005
NTSB Number
DFW05CA120
Location
Hondo, TX
Event ID
20050622X00834
Coordinates
29.356666, -99.326667
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain control of the gyrocraft during takeoff. A contributing factor was the failure of the pre-rotator cable.

Aircraft Information

Registration
Make
MAYFIELD
Serial Number
2003003
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
SparrowhawkSBM3
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
SPARROWHAWK

Registered Owner (Current)

Name
REEVE GILBERT
Address
PO BOX 275
City
PANGUITCH
State / Zip Code
UT 84759-0275
Country
United States

Analysis

On May 14, 2005, approximately 1400 central daylight time, a Mayfield Sparrowhawk single-engine gyrocraft, N8023Y, sustained substantial damage when it impacted the ground following a loss of control during takeoff from runway 08 at the Hondo Municipal Airport (HDO), near Hondo, Texas. The commercial pilot, sole occupant of the gyrocraft, was not injured. The gyrocraft was registered and operated by GBA Gyros of Phoenix, of Paradise Valley, Arizona. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight was originating at the time of the accident.

The 5,600-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that the accident flight was the first flight after he had adjusted the pre-rotator gear. During takeoff, the gyrocraft yawed to the right and the pilot attempted to land. As the gyrocraft landed, it rolled over onto its left side.

Examination of the Subaru powered gyrocraft by an Federal Aviation Administration (FAA) inspector, who responded to the accident site, revealed that the tubular structure fuselage was bent and separated in various areas. The main rotor blade was also damaged. Examination of the pre-rotator cable revealed that a worn internal bolt appeared jammed in the engaged position.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA120