DFW08LA220

NTSB accident investigation · Schleicher ASW-20B · Cleburne, TX · August 31, 2008

Accident · FatalLimited investigationFinal report
Date
August 31, 2008, 14:18 local (19:18 UTC)
Place
Cleburne, TX
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N30WKSchleicher ASW-20B
Defining event
Approach: Unknown or undetermined
Weather
Visual (VMC) · Day
Status
Completed · report January 29, 2009
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20080831844919A
Case key
68849

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

Loss of control inflight for undetermined reason.

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.

Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedSchleicher ASW-20B: 1 caseAll aircraft: 1,269 cases
Not determinedNot determined › Not determined · Unknown/Not determinedSchleicher ASW-20B: 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

While performing a landing into an open field, the glider pilot experienced a loss of control and impacted terrain. An examination of the wreckage did not reveal any pre-impact anolmalies. A review of the Cambridge Aero Instrument data recording device displayed that after failing to acquire thermal lift, the pilot manuevered for a left base pattern to a grass field. A low level of diphenhydramine, an over the counter sedating antihistamine often known by the trade name Benadryl, was found in the pilot's blood, well below the concentrations normally associated with impairment.

Factual narrative

On August 31, 2008, at approximately 1418 central daylight time, a Schleicher. ASW-20B glider, N30WK, was substantially damaged upon impact with terrain near Cleburne, Texas. The commercial pilot, the sole occupant, was fatally injured. The glider was owned and operated by a private individual. Visual meteorological conditions prevailed and no flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight originated from TSA Gliderport (TA11), Midlothian, Texas as a local flight at approximately 1326. A local resident contacted emergency services to inform them that a glider had crashed. An inspector from the Federal Aviation Administration (FAA) also responded and documented the crash site. The glider impacted an open field near a residence. The flaps were set to "2" corresponding with -6 degrees of flaps (flaps up 6 degrees). The wreckage was recovered to a secure location for examination. An examination was conducted by the NTSB Investigator-in-Charge. Flight control continuity was established to the rudder, elevator, and ailerons. Continuity to the airbrakes and flaps was also established. No pre-impact anomalies were discovered with the airframe. The accident flight was recorded by an Cambridge Aero Instruments data recording device. An examination of the data revealed that the glider was towed from TA11 and began a flight to the southwest of the airport. The device recorded several successful attempts to thermal the glider. At approximately 1355 the glider began maneuvering to obtain thermal lift, but continued to descend. The flight continued over a field and the glider appeared to enter a normal left traffic pattern. The last recorded point was at 1417 with the glider at 895 feet mean sea level (about 150 feet above ground level), traveling 29 miles per hour, in a descent of approximately 390 feet per minute on "final approach" leg. The glider pilot had logged over 5,279 hours in various military and civilian aircraft. The pilot had logged approximately 399 hours in gliders with at least 7.5 hours in the accident glider. An autopsy was performed on the pilot by the Tarrant County Medical Examiner's Office, Fort Worth, Texas. The medical examiner ruled the manner of death as a result of multiple blunt force trauma. Forensic toxicology was performed on specimens from the pilot by the FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma. The toxicology report stated the presence of carbon monoxide, cyanide, was ethanol was not detected. The report notes: DIPHENHYDRAMINE detected in Blood DIPHENHYDRAMINE detected in Liver IBUPROFEN detected in Blood According to the Chief of the FAA Forensic Toxicology Research Team, diphenhydramine was not quantified in the pilot's blood because the level was below the laboratory's calibration curve. At 1425, an automated weather reporting station located at Cleburne Municipal Airport (CPT), located approximately 9 miles northwest of the accident sitereported winds from 120 degrees at 4 knots, visibility 10 miles, skies clear, temperature 90 degrees Fahrenheit, dew point 72 degrees Fahrenheit and a barometric pressure of 29.96 inches of Mercury.

Aircraft

Registration
N30WK
Reported as
Schleicher ASW-20B
Category
Glider
Serial number
20641
Airframe hours
1,513
Damage
Substantial damage
Flight
Personal · Part 91
Operator
James Rider
Registered owner
James Rider
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 30, 2008
Departed
TA11 · Midlothian, TX

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
71
Injuries
Fatal
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Last flight review
August 22, 2007
Seat
Single
Toxicology
Performed
Flight hours
5,279 total · 8 in this make and model · 1 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 72 °F
Altimeter
29.95 inHg
Observed at
CPT, 9 nm away

FAA reports on this event · 1

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