DFW07LA102

NTSB accident investigation · Walker Zenith Zodiac 601 XL · Canadian, TX · May 2, 2007

Accident · FatalLimited investigationFinal report
Date
May 2, 2007, 13:00 local (18:00 UTC)
Place
Canadian, TX
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N10028Walker Zenith Zodiac 601 XL
Weather
Instrument (IMC) · Day
Status
Completed · report May 28, 2008
Report
Approved by Office Director
Parties
Zenair, FAA/FSDO
FAA report
20070502832439A
Case key
65683

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 NTSB’s determination of the probable cause, and any contributing factors.

The pilot's improper pre-flight planning and decision to depart into deteriorating weather conditions, which resulted in a loss of control and subsequent in-flight break up.

Analysis

The single engine experimental light sport airplane was observed departing from the airport in deteriorating weather conditions that consisted of low ceilings, reduced visibility, heavy rain, and lightning southwest of the airport. The pilot, who held an FAA Sport Pilot certificate, did not file a flight plan and there was no record that he obtained a weather briefing from an automated flight service station prior to departure. The purpose of the flight could not be determined; however, witnesses heard and/or observed the airplane depart and then fly in the vicinity of the airport for approximately 15 minutes before it was reported to police that the airplane had crashed approximately 2.3 miles northwest of the airport.about 16 minutes later. There were no known voice communications from the pilot prior to the accident. A review of the wreckage revealed that the airplane came apart in flight before it impacted terrain. The debris was scattered along a heading of 030 degrees for approximately 1.3 miles. Examination of the fractured wing spars and elevator rear attachment points revealed signatures consistent with overload stresses. In addition, examination of the two seatbelt assemblies revealed that they remained securely attached to their respective airframe attachment points, but were not buckled. The seatbelt material was clean, not stretched, and the metal buckles (male and female) did not exhibit any damage. The canopy's locking mechanism was found in the unlocked position. A toxicological exam revealed positive results for the following drugs; bupropion, an antidepressant medication, was detected in the kidney, bupropion metabolite was detected in the kidney and present in the liver; chloroquine, a medication used for the treatment or prevention of malaria, was detected in the liver; and, diphenhydramine, an antihistamine with sedative effects, was detected in the kidney and liver. No blood, urine, or vitreous was available for analysis.

Factual narrative

The factual narrative1,311 words

History of flight

On May 2, 2007, approximately 1245 central daylight time, an experimental Walker Zodiac 601 XL single-engine light sport airplane, N10028, sustained substantial damage following an in-flight break up and collision with terrain west of the Hemphill County Airport (HHF), near Canadian, Texas. The certificated sport pilot, sole occupant of the airplane, was fatally injured. The airplane was operated by and registered to the pilot. No flight plan was filed for the flight that departed Hemphill County Airport approximately 1230. The purpose or destination of the flight could not be determined. Instrument meteorological conditions prevailed for the flight conducted under 14 Code of Federal Regulations Part 91.

A witness was dropping people off at a facility located near the airport around 1230, when he observed a "dingy tan color" airplane parked at the south end of the main runway with its engine running. He said, "The plane just looked odd to me. The plane took off the ground right in front of the Exhibition Center [where he was standing]. When the plane got up he immediately went to banking the plane back toward the Red Deer Bridge area. The plane was climbing and banking to the south at the same time. I thought to myself at the time that it was silly to take off in the rain the way the rain was coming in." The witness then drove his truck to the local nursing home. When he got out of the truck he could hear the airplane. He said it sounded "o.k" and thought that maybe the pilot was practicing take offs and landings. The witness turned his attention away from the airplane and heard about the accident later on that afternoon.

In a telephone interview, the airport manager, who was also a pilot, stated that he was walking into his home located about 1 mile from the airport around 1230, when he heard the sound of an airplane equipped with a 4-cylinder engine departing. Based on his location, he was unable to see the airplane. Approximately 15 minutes later, as the airport manager was walking from his home to his driveway, he again heard the sound of the airplane and thought that maybe it was making an approach to the airport. He described the weather as "heavy rain," but did not recall seeing any lightning or hearing thunder. The airport manager then got into his car and started driving. He noted that while driving in the heavy rain, his forward visibility was approximately 500 feet and the rain was bouncing back up off the road.

Another witness, who was also a pilot and former federal agent, was in his office at the local Courthouse, about 4 miles from the accident site around 1240, when he received a call that his daughter was in the emergency room at a hospital in Dallas, Texas. This prompted him to check the weather and determine if it was suitable for him to fly his own airplane to go see her. When he looked out the window he observed heavy rain, low clouds and reduced visibility. Even though his Cessna 210 was equipped for instrument flight, he told himself, "no way!" The witness later heard the police dispatch call that announced that an airplane had crashed northwest of the airport. He said the time was around 1300.

A gentleman, who was driving along a road that intersected the wreckage path, called 911 when he observed airplane debris in the road. According to the Hemphill County Sheriff's report, this call was made at 1250.

A review of Automated Flight Service Station (AFSS) records revealed that the pilot did not receive a weather briefing prior to the flight. Hemphill County Airport is an uncontrolled airport and does not have an air traffic control tower. There was no recorded voice communications or radar information for this flight.

Personnel information

The FAA issued the 63-year old pilot a Sport Pilot certificate on July 12, 2006. According to the pilot's son, the pilot had accrued a total of 176 hours; 43 hours in make and model, of which 29 hours were in the accident airplane. In addition, the pilot had logged a total of 30 hours in the 90 days preceding the accident. The pilot was not required to have an FAA medical and he used the airplane to commute back and forth from his home in Oklahoma for business purposes.

Meteorological information

Weather reported at Hemphill County Airport at 1230 was wind from 020 degrees at 4 knots, visibility 10 statute miles, scattered clouds 1,200 feet, broken clouds 2,000 feet, overcast clouds 2,600 feet, temperature 63 degrees, dew point 61 degrees, and a barometric pressure setting of 29.94 inches of Mercury.

Weather reported at 1245 was wind from 100 degrees at 7 knots, visibility 3 statute miles, heavy rain, scattered clouds 500 feet, broken clouds 2,000 feet, overcast clouds 2,900 feet, temperature 61 degrees, dew point 61 degrees, a barometric pressure setting of 29.94 inches of Mercury, and lightning southwest of the airport.

Weather reported at 1305, was wind from 360 degrees at 5 knots, visibility 2 statute miles, heavy rain, scattered clouds 200 feet, broken clouds 800 feet, overcast clouds 2,000 feet, temperature 59 degrees, dew point 59 degrees, and a barometric pressure setting of 29.93 inches of Mercury.

Wreckage and impact information

A Federal Aviation Administration (FAA) safety inspector performed an on-scene examination of the wreckage and was assisted by the Hemphill County Sheriff's Department. According to the inspector, airplane debris was found dispersed over an area that was 1.3-miles-long on an approximate heading of 030 degrees about 2.3 miles northwest of the airport. The beginning of the wreckage path was identified by pieces of paper and a section of the airplane's checklist followed by two sections of the left wing, then the right wing, the main wreckage, and the engine, which was found at the furthest end of the debris field. The main wreckage, which consisted of part of the fuselage, empennage and tail control surfaces, came to rest several hundred feet beyond where the wings came to rest. The pilot's body came to rest on the ground several feet away from the main wreckage. Also found scattered along the 1.3-mile-long debris path were pieces of Plexiglas, fiberglass, aeronautical charts, and the pilot's personal belongings.

The airplane wreckage was examined on May 31, 2007, under the supervision of the Safety Board. Examination of the left wing revealed that it was torn into two sections and exhibited impact damage. The rear attachment bolt had ripped through the rear spar fuselage attachment. The forward and rear spars also exhibited angular fracture features indicative of overload. The right wing was in one section and exhibited some impact damage. The forward and rear spars were bent aft and exhibited angular fracture features indicative of overload.

The tail section, including the elevator, vertical stabilizer and rudder, remained attached to the airframe by the forward attachment bolts, but the elevator was no longer attached to the rear attachment points. The tail section was removed and sent to the Safety Board's Materials Laboratory in Washington DC, where it was examined on April 16, 2008. According to the Materials laboratory Factual Report,"... the airplane's engineering drawings indicated that the horizontal stabilizer was attached to the fuselage at the right rear and left rear locations through a sheet metal bracket (rear attachment plate) with two lobes that extend down and are bolted to fuselage structure. Examination of the horizontal stabilizer’s rear attachment locations on the fuselage revealed that lower lobe portions of the rear attachment plate were fractured from the remainder of the plate and remained bolted to the stabilizer attachment bracket on the fuselage. Examination of the fracture faces revealed a clean, slightly grainy surface that was inclined on a slant plane of approximately 45 degrees, consistent with an overload event.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

In flight encounter with weatherManeuvering
Weather condition - low ceilingFactor
Preflight planning/preparation - poorPilot in commandCause
Weather condition - rainFactor
Airframe/component/system failure/malfunctionManeuvering
Wing - separationCause
Design stress limits of aircraft - exceededPilot in commandCause
Loss of control - in flightDescent - uncontrolled
In flight collision with terrain/waterDescent - uncontrolled

Aircraft

Registration
N10028
Reported as
Walker Zenith Zodiac 601 XL
Category
Airplane
Serial number
6-5123
Airframe hours
3,542.11
Engine
Teledyne Continental O-200-A`, 100 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
McMurphy Consulting
Airworthiness certificate
Special, Special light-sport (Special); Special, Experimental (Special)
Last inspection
Continuous airworthiness · March 1, 2007
Departed
HHF · Canadian, TN
Destination
HHF · Canadian, TN
Airport
HHF · Hemphill County Airport

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
Fatal
Certificate
Sport Pilot
Airplane ratings
Single-engine land
Last flight review
July 1, 2006
Seat
Left
Toxicology
Performed
Flight hours
176 total · 43 in this make and model · 30 in the last 90 days

Weather

Conditions
Instrument (IMC) · Day
Wind
360° at 5 knots
Visibility
2 statute miles
Lowest ceiling
800 ft broken
Temperature
59 °F, dew point 59 °F
Altimeter
29.93 inHg
Observed at
HHF, 2 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.