SEA98LA091

NTSB accident investigation · Stephens Vortex · Chinook, MT · June 9, 1998

Accident · FatalLimited investigationFinal report
Date
June 9, 1998, 05:45 local (11:45 UTC)
Place
Chinook, MT
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N9261NStephens Vortex
Weather
Visual (VMC) · Day
Status
Completed · report February 11, 2000
Report
Approved by Office Director
FAA report
19980609025689A
Case key
42794

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

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Probable cause

The pilot's failure to maintain aircraft control for an undetermined reason.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightClimb
Aircraft control - not maintainedPilot in commandCause
Reason for occurrence undeterminedCause
Altitude deviation,uncontrolledDescent - uncontrolled
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The private pilot, who was the builder of the gyroplane, had logged about 21 hours of flight time in gyroplanes, but did not have a gyroplane rating. A witness observed the gyroplane's departure and climb-out from the airport. When the gyroplane was approximately 400-500 feet AGL, the witness observed the nose pitch down slightly, then rapidly upward about 40 degrees, then down rapidly about 40 degrees below horizontal then back up as before. The witness said the gyroplane then seemed to fall nearly vertically downward to the ground, and speculated that there was some sort of catastrophic failure to the aircraft. FAA inspectors, however, found no evidence of inflight breakup, or a main rotor blade strike of the empennage.

Factual narrative

On June 9, 1998, approximately 0545 mountain daylight time, an amateur-built Stephens Vortex gyroplane, N9261N, was destroyed when it collided with terrain in an uncontrolled descent shortly after departure from the Chinook, Montana, airport. The private pilot, who was the owner and the sole occupant of the aircraft, was fatally injured. Visual meteorological conditions prevailed at the time of the accident. The aircraft burned after impact. There was no ELT on board the aircraft.

The gyroplane had recently been issued a special airworthiness certificate. The private pilot, who was the builder of the gyroplane, had logged about 21 hours of flight time in gyroplanes, but did not have a gyroplane rating.

A witness, who was flying in an airplane at the time of the accident, observed the gyroplane's departure from the airport, taking off from runway 08. He stated that the gyroplane "climbed on the runway heading to about 300 feet and made a left 90 degree turn. He flew about 1/2 mile to the north then made a 90 degree turn to the right and flew east about 1/2 mile. At that point, he was approximately 400-500 feet AGL [above ground level]. Suddenly the nose pitched down slightly, then rapidly upward about 40 degrees, then down rapidly about 40 degrees below horizontal then back up as before. He then seemed to fall nearly vertically downward to the ground. The aircraft looked as if it was being jerked around, falling like a leaf. Due to the fact I was in my aircraft at the time, I could not hear the engine. Having been around aviation all of my life, it appeared there was some sort of catastrophic failure to the aircraft."

Statements were provided to the Safety Board concerning a main rotor blade repair that had been completed prior to this flight. FAA inspectors found no evidence of inflight breakup, or a main rotor blade strike of the empennage, and no evidence of a failed main rotor blade repair.

Aircraft

Registration
N9261N
Reported as
Stephens Vortex
Category
Gyroplane, amateur-built
Serial number
001
Engine
Rotax 582, 65 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Registered owner
Howard J. Stephens
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 5, 1998
Departed
S71

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
70
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Toxicology
Performed
Flight hours
2,322 total · 21 in this make and model · 7 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
36 °F, dew point 34 °F
Altimeter
29.00 inHg
Observed at
KHV

FAA reports on this event · 1

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