CEN14LA079

NTSB accident investigation · Thompson William A Sparrow II · Jeromesville, OH · December 4, 2013

Accident · Serious injuriesLimited investigationFinal report
Date
December 4, 2013, 12:40 local (17:40 UTC)
Place
Jeromesville, OH
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5955YThompson William A Sparrow II
Defining event
Initial climb: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report December 19, 2014
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA -- Cleveland Flight Standards
FAA report
20131204024249A
Case key
88528

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 student pilot's in-flight loss of control while attempting to return to the runway following a loss of engine power. The cause of the loss of engine power could not be determined because the postaccident examination did not reveal any anomalies.

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · Student/instructed pilotThompson William A SPARROW II: 1 caseAll aircraft: 9,295 casesProbable cause
Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedThompson William A SPARROW II: 1 caseAll aircraft: 1,269 casesProbable cause
Not determinedNot determined › Not determined · Unknown/Not determinedThompson William A SPARROW II: 1 caseAll aircraft: 2,247 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 student pilot recalled taxi testing the airplane, which had a newly installed carburetor, before flying the airplane around his farm without incident. He believed that he took off again and that the engine lost power, but he was unsure at what point during the flight that might have occurred. He recalled that he might have been attempting to return to the runway at the time of the accident; however, he did not recall the accident. A postaccident examination of the airplane on scene did not reveal any anomalies attributable to a preimpact failure or malfunction. Although the airplane was operating in weather conditions with a chance of moderate carburetor icing at cruise power, the investigation could not determine whether the loss of power was caused by mechanical or environmental factors. The pilot received his student pilot certificate the year before the accident; however, he could not provide any record of an endorsement for solo flight, as required. Further, although he reported maintaining the airplane himself, there was no record of him holding a mechanic or repairman certificate.

Factual narrative

On December 4, 2013, about 1240 eastern standard time, an experimental, amateur-built Thompson Sparrow II, N5955Y, was substantially damaged when it impacted terrain near Jeromesville, Ohio. The pilot sustained serious injuries. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The flight originated from a private airstrip about 1230.The pilot informed Federal Aviation Administration (FAA) inspectors that he was in the process of testing a new carburetor that he recently installed. After conducting some taxi testing with the newly installed carburetor, he flew the airplane around his farm without incident. He did not recall the events after that point in time. The pilot believed that he took off again and that the engine lost power, but he was unsure at what point during the flight that might have occurred. He recalled that he might have been attempting to return to the runway at the time of the accident. The airplane came to rest upright. The propeller assembly and engine cowling had separated and were located in the debris path. The propeller blades remained attached to the hub and appeared undeformed. The nose landing gear had collapsed. The nose and center fuselage structure was deformed. Both wings were twisted and exhibited leading edge crush damage. The flight controls remained attached to the wing. The empennage appeared intact with the exception of the lower portion of the rudder, which was deformed. The fuel tanks appeared intact and contained fuel. A postaccident on-scene examination of the airplane did not reveal any anomalies attributable to a preimpact failure or malfunction. FAA records indicate that the pilot was issued a student pilot certificate on July 25, 2012; however, there was no record of the pilot having been issued an airman medical certificate. He could not provide any record of an endorsement for solo flight as required by the regulations. The pilot informed FAA inspectors that he did not maintain a flight time logbook. However, he reported accumulating about 300 hours total flight time, with about 30 hours in Sparrow II airplanes. The pilot also informed inspectors that he had been involved in previous accidents that had not been reported to the FAA or NTSB. The accident airplane was issued an experimental airworthiness certificate in October 1998. The pilot bought the airplane in April 2012. However, FAA records indicated that the pilot did not submit the required documentation to transfer the registration. The airplane registration was subsequently cancelled on September 3, 2014. The pilot informed FAA inspectors that he did not maintain any maintenance logbooks for the aircraft. Although the pilot reported maintaining the airplane himself, there was no record of the pilot holding a mechanic or repairman certificate.

Aircraft

Registration
N5955Y
Reported as
Thompson William A Sparrow II
Category
Airplane, amateur-built
Serial number
CA 306
Built
1998
Engine
Bombardier ROTAX 582UL, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Departed
PVT · Jeromesville, OH
Destination
PVT · Jeromesville, OH
Airport
PVT · Private

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
65
Injuries
Serious
Certificate
Student
Seat
Left
Flight hours
300 total · 30 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F, dew point 48 °F
Altimeter
29.84 inHg
Observed at
MFD, 14 nm away

Docket · 4

The files NTSB released with the investigation on November 12, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 867 KB 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.