N554BGGoetz RAF 20002008-09-18 NTSB Accident Report

Substantial
None

Goetz RAF 2000S/N: H2-05-16-643

Summary

On September 18, 2008, a Goetz RAF 2000 (N554BG) was involved in an incident near Mulino, OR. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's failure to maintain directional control during landing.

The pilot submitted a written statement and reported that he was conducting flight tests on the gyrocopter. After performing a series of high-speed taxis and lift-offs, the pilot brought the gyrocopter around in the pattern. As the gyrocopter landed, it veered to the right and came to rest on its side. Post accident examination by the Federal Aviation Administration accident coordinator did not reveal any control anomalies. The gyrocopter had approximately 40 hours of flight time, and the pilot had 11 hours in make and model.

This incident is documented in NTSB report SEA08CA204. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N554BG.

Accident Details

Date
Thursday, September 18, 2008
NTSB Number
SEA08CA204
Location
Mulino, OR
Event ID
20081003X17552
Coordinates
45.216110, -122.589996
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 directional control during landing.

Aircraft Information

Registration
Make
GOETZ
Serial Number
H2-05-16-643
Year Built
2006
Model / ICAO
RAF 2000

Registered Owner (Historical)

Name
GOETZ BYRON P
Address
20435 S GREEN MOUNTAIN RD
Status
Deregistered
City
COLTON
State / Zip Code
OR 97017-9471
Country
United States

Analysis

The pilot submitted a written statement and reported that he was conducting flight tests on the gyrocopter. After performing a series of high-speed taxis and lift-offs, the pilot brought the gyrocopter around in the pattern. As the gyrocopter landed, it veered to the right and came to rest on its side. Post accident examination by the Federal Aviation Administration accident coordinator did not reveal any control anomalies. The gyrocopter had approximately 40 hours of flight time, and the pilot had 11 hours in make and model.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08CA204