WPR09CA186

NTSB accident investigation · Air Creation Clipper 58 · Anacortes, WA · April 9, 2009

Accident · Minor injuriesData collectionFinal report
Date
April 8, 2009, 19:00 local (Apr 9, 2009, 02:00 UTC)
Place
Anacortes, WA
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5138JAir Creation Clipper 58
Defining event
Initial climb: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report June 22, 2009
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20090408004099A
Case key
73621

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 partial loss of engine power due to the passenger's inadvertent movement of the engine throttle control.

Findings · 2

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.

Engine controls: power leverAircraft › Aircraft power plant · Unintentional use/operationAir Creation CLIPPER 582S: 1 caseAll aircraft: 95 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 the experimental weight-shift-control light sport aircraft (trike) experienced a partial loss of engine power during initial climb. The pilot noticed that the engine's throttle went to an idle setting upon climbing to a maximum height of 50 feet above the runway. The pilot made a forced landing on grass-covered terrain adjacent to the runway and the airplane collided with the airport's perimeter chain link fence. One of the trike's fabric wings was ripped over a foot-long span, and the cockpit enclosure was cracked. The pilot reported that no maintenance had been performed on the airplane since he purchased it about 2 months prior to the accident. According to the pilot, although the propeller continued rotating when the engine power loss occurred, insufficient power was produced to sustain flight. A Federal Aviation Administration inspector who examined the trike and interviewed the pilot reported that the trike's throttle is accessible to occupants located in both the front and rear seats. In his statement, the pilot opined that during takeoff the throttle was inadvertently retarded by the passenger in the front seat.

Factual narrative

The experimental weight-shift-control light sport aircraft (trike) experienced a partial loss of engine power during initial climb. The pilot reported that he noticed the engine's throttle went to an idle setting upon climbing to a maximum height of 50 feet above the runway. Thereafter the trike descended, and the pilot made a forced landing on grass-covered terrain adjacent to the runway. As the trike decelerated, it collided with the airport's perimeter chain link fence. The private pilot was not injured, and the passenger sustained a minor injury. One of the trike's fabric wings was ripped over a foot-long span, and the cockpit enclosure was cracked. The pilot reported to the National Transportation Safety Board investigator that no maintenance had been performed on the trike since he purchased it about 2 months prior to the accident. According to the pilot, although the propeller continued rotating when the engine power loss occurred, insufficient power was produced to sustain flight. The Federal Aviation Administration coordinator who examined the trike and interviewed the pilot reported that the trike's throttle is accessible to occupants located in both the front and rear seats. The pilot opined that during takeoff, he did not notice that the throttle was inadvertently retarded by the passenger in the front seat.

Aircraft

Registration
N5138J
Reported as
Air Creation Clipper 58
Category
Weight-shift
Serial number
T99045
Airframe hours
232
Engine
Rotax 582, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental light sport (Special)
Last inspection
Condition · September 10, 2007
Departed
74S · Anacortes, WA
Destination
74S · Anacortes, WA
Airport
74S · Anacortes, runway 36, 3,015 × 60 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
45
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Last flight review
July 17, 2007
Seat
Rear
Flight hours
134 total · 10 in this make and model · 120 as pilot in command · 10 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
20,000 ft overcast
Temperature
48 °F, dew point 45 °F
Altimeter
29.84 inHg

FAA reports on this event · 1

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