N218DH

Substantial
None

David G. Holmes Bensen Gyrocopter

Accident Details

Date
Sunday, April 22, 2001
NTSB Number
MIA01LA134
Location
Troy, AL
Event ID
20010503X00866
Coordinates
31.759885, -85.999122
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the pilot to maintain airspeed during the approach resulting in a hard landing. A contributing factor in the accident was the loss of engine power during final approach due to undetermined reasons.

Aircraft Information

Registration
N218DH
Make
DAVID G. HOLMES
Engine Type
Reciprocating
Year Built
2000
Model / ICAO
Bensen GyrocopterAVAM
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HOLMES DAVID G
Address
3176 CONNELL RD
Status
Deregistered
City
TROY
State / Zip Code
AL 36079-5583
Country
United States

Analysis

On April 21, 2001, about 1900 central daylight time, a Bensen gyrocopter, N218DH, registered to a private individual, landed hard, bounced then rolled over after touchdown on a golf fairway at the Troy County Club, Troy, Alabama. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The gyrocopter was substantially damaged and the airline transport-rated pilot, the sole occupant, was not injured. The flight originated about 10 minutes earlier from the Brundidge Municipal Airport, Brundidge, Alabama.

The pilot stated that he performed a power-off approach to the 10th fairway, but just before touchdown he elected to fly closer to the club house and pitched the nose up then added power, but the engine did not respond. A high sink rate developed resulting in a hard landing. The gyrocopter then began to wobble, resulting in main rotor blade contact with the grass fairway. The gyrocopter then rolled over and a postcrash fire damaged one of the main rotor blades, the main rotor pitch change assembly, and the carburetor. He further stated that there was no flight control preimpact failure or malfunction and he believes the engine quit during the approach due to "flooding", as it had happened before. He also stated that he should have added power before pitching up to air taxi.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA01LA134