N538CJ

Destroyed
Fatal

ZENITH AIRCRAFT CO ZODIAC 601 XLS/N: 6-6528

Accident Details

Date
Friday, November 6, 2009
NTSB Number
CEN10FA042
Location
Agnos, AR
Event ID
20091107X34009
Coordinates
36.255279, -91.693054
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The in-flight separation of both wings due to aileron flutter. The aileron flutter was the result of inadequate wing stiffness and strength and the lack of aileron counterbalances.

Aircraft Information

Registration
N538CJ
Make
ZENITH AIRCRAFT CO
Serial Number
6-6528
Year Built
2007
Model / ICAO
ZODIAC 601 XL

Registered Owner (Historical)

Name
CUMMINGS CHARLES
Address
PO BOX 208
Status
Deregistered
City
NORTH AURORA
State / Zip Code
IL 60542-0208
Country
United States

Analysis

HISTORY OF FLIGHT

On November 6, 2009, at 1005 central standard time, a Zenith Aircraft Company Zodiac 601 XL, experimental light sport airplane, N538CJ, was destroyed when it impacted terrain, following an in-flight breakup near Agnos, Arkansas. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. The sport pilot was fatally injured. The cross country flight departed Sharp County Regional Airport (KCVK), Ash Flat, Arkansas, at 0848.

The property owner discovered the wreckage of the accident airplane in his field. There were no known or identified witnesses to the events that led up to the accident flight or impact sequence. Federal Aviation Administration (FAA) radar data was not available for the accident flight. The pilot was not in communications with other pilots or airport ground personnel in the area or air traffic control at the time of the accident.

The debris field was scattered over 600 feet on a magnetic bearing of 35 degrees initiating with the right wing assembly which came to rest in a pond. The left wing assembly came to rest forward of the right wing. The left wing spar, left wing fuel tank, various cockpit items, and personal effects were located in the debris field. The fuselage, empennage, engine, and propeller assembly came to rest, inverted, approximately 600 feet from the right wing. There were no ground scars identified between the right wing and the main wreckage that could be associated with the left or right wing, empennage, or fuselage.

The wreckage was recovered and relocated to a facility in Clinton, Arkansas, for further examination.

PERSONNEL INFORMATION

The pilot, age 71, held a sport pilot certificate issued on January 12, 2008. In addition, he held a repairman certificate for light sport aircraft – Zodiac 601 XL, N538CJ. He was issued a third class airman medical certificate/student pilot certificate on July 24, 2007. The medical certificate contained the limitations “holder must wear corrective lenses” and “not valid for any class after May 31, 2008.” The pilot held a valid driver’s license for the state of Illinois.

The pilot’s personal flight logbook was located in the vicinity of the main wreckage. The cover and first four pages of the logbook had torn and were not found within the main wreckage or debris field. A review of the logbook indicated that the pilot had logged 116 hours of flight time, of which 77 hours were in the accident airplane make and model. The pilot had logged two hours in the previous 90 days. According to the logbook, the pilot successfully demonstrated the skills required to be proficient for a sport pilot certificate on January 12, 2008.

AIRCRAFT INFORMATION

According to FAA records, the pilot/owner manufactured the 2007 experimental light sport airplane, a Zenith Zodiac 601 XL (serial number 6-6528). It was registered with an FAA special airworthiness certificate in the category of experimental for light sport operations. Block 8A “Existing Aircraft without an airworthiness certificate & do not meet 103.1” was checked. A Jabiru 3300 engine rated at 120 horsepower at 3,300 rpm powered the airplane. The engine was equipped with a two-blade Sensenich propeller.

The airplane registered to and operated by the pilot was maintained under an annual condition inspection program. The maintenance records were not with the airplane wreckage. Several requests were sent to the owner’s estate, requesting that the maintenance records and airplane information, or copies of those records and information be provided to the National Transportation Safety Board (NTSB) for their review. These records were not located by the bank handling the estate. Requests sent to family members were not responded to.

FAA records showed that Zenith Aircraft Company manufactured the accident airplane. However, the bill of sale for the airplane showed that it was a kit that had been sold from Zenith Aircraft Company, Mexico, Missouri, and the aircraft manufacturer was listed as “Charles Cummings,” with the Zodiac 601 XL designated as a kit.

Following the accident, a representative from Zenair in Canada (also a party to the accident investigation) informed the NTSB investigator-in-charge (IIC) that the accident pilot had previously experienced and reported an encounter with flutter in the accident airplane. The NTSB made contact with the owner of Flight Crafters who was identified as the source of this report. This individual clarified that the pilot had not reported this encounter to him, but rather he had heard of this encounter through other pilots in the area. Multiple attempts were made to locate the individual with whom the pilot had spoken with regarding the flutter event. This report could not be substantiated through first hand information, fact gathering, or interviews.

A review of the Experimental Aircraft Association (EAA) safety program records revealed that the owner/builder had not participated in either the EAA Flight Adviser or the EAA Technical Counselor Programs.

METEOROLOGICAL INFORMATION

The accident site was located between several official weather observation stations. The closest official weather observation station was Batesville Regional Airport (KBVX), Batesville, Arkansas, located 35 nautical miles (nm) south of the accident site. The elevation of the weather observation station was 465 feet mean sea level (msl).

The routine aviation weather report (METAR) for KBVX, issued at 1015, reported winds 170 degrees at 10 knots, gusting to 15 knots, visibility 10 statute miles, sky condition few clouds at 3,400 feet, temperature 17 degrees Celsius (C), dew point 04 degrees C, altimeter 30.25 inches of Mercury.

The METAR report for Walnut Ridge Regional Airport (KARG), Walnut Ridge, Arkansas, issued at 0955, (located 38 nm east-southeast of the accident site) reported winds 180 degrees at 8 knots, visibility 10 statute miles, sky condition clear, altimeter 30.27 inches of Mercury. Temperature and dew point were not reported.

The METAR report for Ozark Regional Airport (KBPK), Mountain Home, Arkansas, issued at 0953 (located 38 nm west of the accident site) reported winds 180 degrees at 8 knots, visibility 9 statute miles, sky condition clear, temperature 18 degrees C, dew point 10 degrees C, altimeter 30.19 inches of Mercury.

Two regional pilot reports (PIREPS) issued at 1153 and 1444 reported no turbulence. An Airmen’s Meteorological Information (AIRMET) for moderate turbulence below 8,000 feet was in effect for the accident airplane’s route of flight. There were no Significant Meteorological Information (SIGMETS) active for the area at the time of the accident.

In addition to the official weather observation stations, a Department of Interior weather station, designation ESDA4, was located 12 nm south-southwest of the accident site at an elevation of 538 feet. The station reported winds at 179 degrees at 4.33 knots with wind gusts to 10.44 knots.

FLIGHT RECORDERS

A Garmin GPSMap 296 handheld global positioning system (GPS) unit was located within the wreckage of the accident airplane. The unit was recovered and sent to the NTSB Vehicle Recorders Laboratory in Washington, D.C., for download. Upon arrival at the lab, power was applied to the unit and the recorded waypoint, route, and track log data were successfully downloaded from the unit via the USB port.

Eighty-six user defined waypoints, one user defined route, and 118 track logs were downloaded from the unit. This data included date, time, altitude, distance from previous update, time since previous update, average groundspeed since previous update, average course since previous update, and the latitude and longitude at the time of the update.

The track log data from the date of the accident started at 0848:06 and ended at 1004:56. The last position of the airplane was recorded at 36 degrees 15.061 minutes north latitude and 91 degrees 41.449 minutes west longitude. The last calculated groundspeed velocity of the airplane was 117 miles per hour. The last calculated course of the airplane was 081 degrees true.

The plotted data depicted the accident airplane depart KCVK and fly southwest towards Horseshoe Bend Airport (K6M2), Horseshoe Bend, Arkansas. The data was consistent with the performance of a touch and go landing at K6M2, and then a northeasterly departure from K6M2.

WRECKAGE AND IMPACT INFORMATION

The wreckage was located in a sparsely vegetated hilly field just south of Agnos, Arkansas. The right wing initiated the debris field, coming to rest inverted in a pond at a measured elevation of 820 feet. The wing included the right aileron and right flap; both remained attached to the wing assembly.

The left lower wing spar cap was located approximately 55 feet from the right wing. This spar separated from the left wing, and was bowed, forming a semi-circular shape.

The left wing was located approximately 190 feet from the right wing at a measured elevation of 838 feet. The left wing came to rest inverted. The left wing included the left aileron and left flap; both remained attached to the wing assembly. The leading edge of the left wing separated partially from the wing assembly along the lower rivet line from the wing root outboard to the landing light.

The left fuel tank came to rest 96 feet from the left wing. The fuel tank was bent and broken due to impact damage. Adjacent to the left fuel tank was a semi-circular ground scar, consistent in shape with the fuel tank. The ground scar contained a fluid consistent in color, smell, and texture with aviation fuel.

The main wreckage was located 295 feet from the fuel tank and came to rest inverted, directly beneath power lines and adjacent to a tree. The main wreckage consisted of the fuselage, empennage, and engine and propeller assembly. The empennage consisted of the horizontal a...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10FA042