- Date
- December 22, 2010, 14:30 local (22:30 UTC)
- Place
- Newberg, OR
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N7008ZMoyes Bailey Microlite
- Defining event
- Maneuvering: Loss of control in flight
- Weather
- Visual (VMC) · Day
- Status
- Completed · report May 16, 2011
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- FAA FSDO
- FAA report
- 20101222053679A
- Case key
- 78052
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 improper recovery from a dive, which resulted in a loss of control.
Findings · 5
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.
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
According to the pilot, he leveled the experimental, amateur-built airplane in cruise flight and gripped the control stick with his legs in order to free his hands to perform some aerial photography. The pilot had done the same thing on previous flights, and he was aware that the airplane had a tendency to pitch down and accelerate when not monitored and controlled continuously. After he took some photographs, he grasped the stick with one hand and applied back pressure to reduce the airspeed. While attempting to stow the camera, he inadvertently let go of the control stick, and the airplane descended and accelerated again. Although the control stick was free to move, the pilot was unable to correct the flight path with the elevator, and he deployed the ballistic recovery parachute, and retarded the engine to idle. The airplane impacted terrain nose-first and sustained substantial damage. Postaccident examination of the airplane by a Federal Aviation Administration inspector did not reveal any preimpact anomalies or failures. The pilot reported that after the accident, he learned it was necessary to retard the throttle in order to successfully recover from a dive.
Factual narrative
The experimental, amateur-built airplane was a high-wing pusher-propeller configuration, with the engine mounted above the wing. The private pilot reported that he had a total flight experience of about 154 hours, including about 36 hours in the accident airplane. The preflight inspection, engine run-up, and takeoff were normal. After the pilot leveled the airplane in cruise flight at an altitude of about 1,300 feet above the ground, he gripped the control stick with his legs in order to free his hands to access and use a camera for some aerial photography. The pilot had done the same thing on previous flights, and he was aware that the airplane had a tendency to pitch down and accelerate when not monitored and controlled continuously. After he took some photographs, he grasped the stick with one hand and applied back pressure to reduce the airspeed. He tried to stow the camera with one hand, but let go of the stick to complete that task. The airplane descended and accelerated again, but to a higher airspeed than the previous time. Although the control stick was free to move, the pilot was unable to correct the flight path with the elevator, and stated that within "a few seconds the aircraft was pointing near[ly] straight down." He deployed the ballistic recovery parachute, and then retarded the engine to idle. The airplane impacted terrain nose-first and sustained substantial damage. The still-inflated parachute dragged the airplane across the ground until the pilot egressed the airplane and collapsed the parachute. Post accident examination of the airplane by a Federal Aviation Administration inspector did not reveal any pre-impact anomalies or failures. The pilot reported that after the accident, he learned from other pilots of the accident airplane make and model that it was necessary to retard the throttle in order to successfully recover from a dive.
Aircraft
- Registration
- N7008Z
- Reported as
- Moyes Bailey Microlite (Dragonfly)
- Category
- Airplane
- Serial number
- 046
- Airframe hours
- 300
- Engine
- Rotax 582, 65 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Special, Experimental light sport (Special)
- Last inspection
- Condition · October 3, 2009
- Departed
- 2S6 · Newberg, OR
- Destination
- 7S9 · Hubbard, OR
- Airport
- 2S6 · Sportsman Airpark
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
- 46
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, With waivers/limitations
- Last flight review
- September 25, 2009
- Seat
- Front
- Flight hours
- 154 total · 36 in this make and model · 154 as pilot in command · 5 in the last 90 days · 2 in the last 30 days · 0 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 200° at 6 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 48 °F, dew point 37 °F
- Altimeter
- 29.84 inHg
- Observed at
- UAO, 6 nm away
Docket · 4
The files NTSB released with the investigation on January 25, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.2 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N7008Z · 2
Matched to the same aircraft by N-number and date.