ERA12CA096

NTSB accident investigation · Thompson Tommy W Loehle P5151 · Courtland, AL · December 4, 2011

Accident · Serious injuriesData collectionFinal report
Date
December 4, 2011, 10:50 local (16:50 UTC)
Place
Courtland, AL
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N212WEThompson Tommy W Loehle P5151
Defining event
Approach-VFR pattern downwind: Windshear or thunderstorm
Weather
Visual (VMC) · Day
Status
Completed · report February 16, 2012
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20111204028069A
Case key
82449

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 airplane's inadvertent encounter with excessive windshear while on the downwind traffic pattern leg at low altitude, which resulted in the pilot's inability to arrest the airplane’s descent. Contributing to the accident was the pilot's decision to fly the traffic pattern at a low altitude in gusty wind conditions.

Findings · 3

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.

Aircraft capability: climb capabilityAircraft › Aircraft oper/perf/capability · Attain/maintain not possibleThompson Tommy W LOEHLE P5151: 1 caseAll aircraft: 183 casesProbable cause
Wind: windshearEnvironmental issues › Conditions/weather/phenomena · Effect on operationThompson Tommy W LOEHLE P5151: 1 caseAll aircraft: 90 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

According to multiple statements, the seller of the single-seat, amateur-built airplane performed a preflight inspection with the buyer and an evaluation pilot, then he flew a demonstration flight around the traffic pattern at 300 to 400 feet above the ground and made a full-stop landing. The wind was straight down the runway at 10 knots and gusting. The evaluation pilot, who had not previously flown the airplane model, subsequently performed ground checks and taxi practice before taking off and climbing the airplane to about 400 feet. He then turned the airplane onto the crosswind leg and reduced power before turning it onto the downwind leg. After several seconds on the downwind leg, the airplane began to descend. The pilot added full power to arrest the descent; however, the airplane continued descending at full power, dropping almost vertically before impacting the ground in a level attitude, sustaining substantial damage to the wings and fuselage. Terrain elevation about 3 nautical miles upwind of the runway was about 150 feet higher. No preexisting mechanical anomalies were noted with the airplane, and all of the statements indicated that the engine was producing full power during the airplane's descent. A witness reported that possible low-level windshear was forecast for the region. Windshear, which is a difference in wind speed and direction over a relatively short distance, can result in a rapid loss of altitude, even with full engine power applied.

Factual narrative

According to multiple statements, the seller of the single-seat, amateur-built airplane first performed a preflight inspection, along with the buyer and an evaluation pilot, then flew a demonstration flight around the traffic pattern at 300 to 400 feet above the ground to a full stop landing. Winds were straight down the runway at 10 knots, but gusty. The evaluation pilot, who had not previously flown the model, subsequently performed ground checks and taxi practice before taking off and climbing the airplane to about 400 feet. He then turned the airplane onto the crosswind leg, and reduced power before turning it onto the downwind leg. After several seconds on the downwind leg, the airplane began to descend. The pilot added full power to arrest the descent; however, the airplane continued descending at full power, dropping almost vertically before impacting the ground in a level attitude and substantially damaging the wings and fuselage. Terrain elevation about 3 nautical miles upwind of the runway was approximately 150 feet higher. No preexisting mechanical anomalies were noted with the airplane, and all of the statements indicated that the engine was producing full power during the airplane's descent.

Aircraft

Registration
N212WE
Reported as
Thompson Tommy W Loehle P5151
Category
Airplane, amateur-built
Serial number
150968863P
Airframe hours
210
Engine
Rotax 582, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · June 7, 2009
Departed
9A4 · Courtland, AL
Destination
9A4 · Courtland, AL
Airport
9A4 · Courtland, runway 17

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
41
Injuries
Serious
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 3
Last flight review
June 30, 2011
Flight hours
5,700 total · 0 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 10 knots, gusting 10
Visibility
10 statute miles
Lowest ceiling
None
Observed at
9A4

Docket · 6

The files NTSB released with the investigation on December 28, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.5 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.