WPR11LA180

NTSB accident investigation · William Wright Avid Flyer · Cedar City, UT · April 1, 2011

Accident · Minor injuriesLimited investigationFinal report
Date
April 1, 2011, 10:45 local (16:45 UTC)
Place
Cedar City, UT
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N613HHWilliam Wright Avid Flyer
Defining event
Initial climb: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report January 31, 2013
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
FAA FSDO
FAA report
20110401004379A
Case key
78733

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

A loss of engine power during initial climb for reasons that could not be determined because postaccident examination did not reveal a specific anomaly that would have precluded normal operation.

Findings · 4

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.

Not determinedNot determined › Not determined · Unknown/Not determinedWright William V AVID FLYER: 1 caseAll aircraft: 2,247 casesProbable cause
Object/animal/substance: tree(s)Environmental issues › Physical environment · Not specifiedWright William V AVID FLYER: 1 caseAll aircraft: 933 cases

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 was on a local test flight after restoring the airplane and flew for about 1 hour, performing maneuvers and touch-and-go landings. He then returned to the airport and picked up another pilot for a familiarization flight. About 1/2 hour into the second flight, the engine sputtered and lost power. The pilot subsequently made an emergency landing on an airstrip, and after performing some troubleshooting, he determined that fuel was not getting from the header tank to the engine. The pilot was able to eventually get the fuel flowing again and ran the engine for about 30 minutes on the ground, followed by accomplishing a successful run up. The pilot then departed the airstrip. He reported that the engine ran well until about 200 feet above ground level. The engine then lost all power, and the pilot glided the airplane into 15-foot-tall trees. Postaccident examination of the engine revealed modifications to the exhaust, intake, ignition, and fuel systems that were not approved by the manufacturer. At the conclusion of the examination, it could not be determined if there was a specific malfunction or a combination of the multiple modifications that led to the loss of engine power. According to FAA Advisory Circular AC 20-27F, Certification and Operation of Amateur-Built Aircraft, "Amateur builders are free to develop their own designs or build from existing designs.”

Factual narrative

HISTORY OF FLIGHT On April 1, 2011, about 1045 mountain daylight time, a William Wright Avid Flyer, N613HH, collided with trees during an off airport forced landing following a loss of engine power on takeoff from a strip near Cedar City, Utah. The pilot/owner was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The private pilot was not injured; the airplane sustained substantial damage to the wings from impact forces. The local personal flight was departing with a planned destination of Cedar City. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot stated that he departed Cedar City on a local test flight after restoring the airplane. He flew for approximately 1 hour, performing both maneuvers and touch-and-go takeoffs and landings. He returned to the airport, and picked up another pilot for a familiarization flight. About 1/2 hour into the second flight, the engine sputtered and lost power. The pilot made an emergency landing on a landing strip for radio remote controlled airplanes. He performed some troubleshooting, and determined that fuel was not getting from the header tank to the engine. He was successful in getting the fuel flowing again. He ran the engine for about 30 minutes on the ground, and performed a successful run up. The pilot decided to leave his passenger at the strip, and fly home alone. He planned to return by car to pick up the passenger. The pilot departed the strip, and reported that the engine ran well until about 200 feet above ground level (agl). The engine then lost all power, and he glided the airplane into 15-foot-tall trees. He was wearing a three-point harness; the full extent of his injuries included bruises along the strap lines. WRECKAGE EXAMINATION On April 19, 2011, inspectors from the Federal Aviation Administration (FAA) supervised examination of the airplane by personnel from Rotech Flight Safety, Inc., who were technical advisers to the Austrian accredited representative per International Civil Aviation Organization Annex 13. The complete Rotech report is part of the public docket; pertinent parts of the report follow. During the visual inspection, the investigators noted modifications to the exhaust system for incorporation of cabin heat by shrouding the exhaust muffler, and ducting into the cabin. They also observed that the exhaust gas temperature (EGT) probes had been relocated from the factory recommended positions, and the previous holes plugged with pop rivets. The installation manual noted that EGT would give the most rapid response in the event of improper mixture, pre-ignition, or detonation. The investigators observed an aftermarket mixture control installed on the engine, which also included modifications to the fuel and air intake systems. The Rotax installation manual stated that no modification should be made to the carburetor and air intake system without consulting Rotax. The system installed did not havetheir approval. The engine had dual carburetors installed. Both carburetors had jets that were different from the stock jets with leaner fuel to air ratios than the stock jets. Both jets were different from each other. According to the Rotech representative, in order for the engine to run properly, both carburetors must be synchronized to each other, and are required to have the exact same jetting. The fuel filters were installed in the incorrect location on the fuel system. The installation manual called for the filters to be between the fuel pump and the carburetors. On the accident engine, they were installed between the fuel pump and the fuel tank. The carburetor vent lines were improperly installed. The fuel pump was installed improperly to the top of the engine. The installation manual stated to mount it in a cool place, not on the engine itself. The spark plugs were nonstandard. The electrodes were excessively black and sooty, which the investigators noted was consistent with a rich fuel/air mixture. Examination of the ignition wires revealed that exposed bare wires had been spliced and soldered together, which had the potential of shorting. Solder was not an acceptable repair method, and the wire was in poor shape. Improper gear oil had been used to lubricate the Rotary and water pump drive shaft rather than 2-stroke injection oil as specified by the manufacturer. ADDITIONAL INFORMATION According to FAA Advisory Circular AC 20-27F, Certification and Operation of Amateur-Built Aircraft, "Amateur builders are free to develop their own designs or build from existing designs. We do not approve these designs and it would be impractical to develop design standards for the wide variety of design configurations, created by designers, kit manufacturers, and amateur builders."

Aircraft

Registration
N613HH
Reported as
William Wright Avid Flyer
Category
Airplane, amateur-built
Serial number
613
Engine
Rotax 582UL, 66 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Color Country Electronics
Registered owner
Color Country Electronics
Airworthiness certificate
Special, Experimental (Special)
Departed
Cedar City, UT
Destination
CDC · Cedar City, UT

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
63
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Seat
Left
Flight hours
285 total · 6 in this make and model · 215 as pilot in command · 5 in the last 90 days · 2 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
59 °F, dew point 30 °F
Altimeter
30.13 inHg
Observed at
KCDC, 5 nm away

Docket · 2

The files NTSB released with the investigation on November 29, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 6.8 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.