WPR11CA079

NTSB accident investigation · Moyes Bailey Microlite · Newberg, OR · December 22, 2010

Accident · No injuriesData collectionFinal report
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.