SEA08CA204

NTSB accident investigation · Goetz RAF 2000 · Mulino, OR · September 18, 2008

Accident · No injuriesData collectionFinal report
Date
September 17, 2008, 17:00 local (Sep 18, 2008, 00:00 UTC)
Place
Mulino, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N554BGGoetz RAF 2000
Defining event
Landing-flare/touchdown: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report November 10, 2008
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20080917846529A
Case key
68949

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot's failure to maintain directional control during landing.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedGoetz Byron RAF 2000: 1 caseAll aircraft: 3,958 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported that he was conducting flight tests on the gyrocopter. After performing a series of high-speed taxi tests and takeoffs, the pilot brought the gyrocopter around in the pattern for a landing. 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.

Factual narrative

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.

Aircraft

Registration
N554BG
Reported as
Goetz RAF 2000
Category
Gyroplane, amateur-built
Serial number
H2-05-16-643
Engine
Subaru EJ22, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Departed
4S9 · Malino, OR
Destination
4S9 · Malino, OR
Flight plan
Unknown
Airport
4S9 · Portland-Mulino, runway 32, 3,425 × 100 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
58
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Flight hours
168 total · 11 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 52 °F
Altimeter
29.84 inHg
Observed at
USA

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.