1 fatality

27 Jan 2008: Free Bird Sportlite (N75474) — Christopher M. Vanree — McCullough, AL

McCullough, AL, United States

On 27 Jan 2008, a Free Bird Sportlite (registration N75474) operated by Christopher M. Vanree was involved in an aviation accident near McCullough, AL. One person was killed. Investigators recorded the probable cause as: The non-certificated pilot's failure to maintain aircraft control while maneuvering. Contributing to the accident was the non-certificated pilot's improper decision to conduct a flight prior to the airplane being properly inspected and certified. This summary draws on records from NTSB; 1 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On January 27, 2008, an amateur-built Free Bird Sportlite 103 (N75474) was destroyed after impacting terrain near McCullough, Alabama, killing the non-certificated pilot. The aircraft was being registered as an experimental light-sport airplane but had not yet been inspected or certificated.

Accident Overview

On January 27, 2008, about 1630 central standard time, an amateur-built Free Bird Sportlite 103, registration N75474, was destroyed during impact with terrain near McCullough, Alabama. The non-certificated pilot was killed. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 Code of Federal Regulations Part 91.

Aircraft Information

According to a Federal Aviation Administration Designated Airworthiness Representative (DAR), the pilot owned the accident airplane but had not yet obtained an FAA sport pilot certificate. The pilot purchased the airplane from a private individual through the Internet, and it did not come with any manuals. The airplane was a two-seat tandem design with the engine mounted on the rear of the high wing. It had a basic empty weight of approximately 500 pounds and a maximum gross weight of 900 pounds. The airplane was equipped with a Two Stroke International model 690L-70 engine, a 70-horsepower engine described as the heaviest available for the airplane. The DAR suggested that due to the engine's weight, it may have created an aft center of gravity condition, which would require modification to move the CG forward prior to certification.

The DAR added that the pilot was in the process of registering and certifying the airplane as an experimental light-sport airplane under FAR 21.191, with a deadline of January 31, 2008. Beyond that date, the airplane would no longer be eligible for ultralight exemptions under FAR 103. The airplane was registered, but due to the DAR's backlog, it had not yet been inspected and certified. Because the airplane was registered before the deadline, certification could be completed after the deadline. The DAR stated that since he had not inspected and certified the airplane, he did not know its actual center of gravity or airworthiness.

Pilot Information

The DAR also owned the flight school where the pilot received instruction. The DAR reported that the minimum flight time requirement for an FAA sport pilot certificate under FAR 61 was 20 hours, and the pilot had accumulated 25 hours of flight instruction, 38 hours of ground instruction, had soloed, and had passed an FAA written examination. The pilot needed to complete a long cross-country flight and then prepare for and pass a practical test with a designated pilot examiner.

The DAR further stated that several months before the accident, the pilot was involved in a prior accident in the same airplane. That accident occurred during a high-speed taxi, in which the airplane accidentally became airborne. The pilot was subsequently advised by the DAR and his flight instructor not to fly the airplane until it was certificated and the pilot received a sport pilot certificate. The DAR stated that all of the pilot's training was conducted in the DAR's flight school airplanes.

Investigation

An FAA inspector reported that according to a witness, the accident airplane departed a private turf airstrip near McCullough and flew around the local area. About 1630, the airplane was in the vicinity of a right downwind leg for the east runway when it impacted a field nose down and left wing low. The witness did not see the impact but heard the engine noise increase, decrease, then increase again, followed by the sound of impact. Most of the airplane was consumed by a postcrash fire; however, the FAA inspector was able to confirm flight control continuity.

Weather and Aftermath

The reported weather at an airport located approximately 20 miles northeast of the accident site, at 1653, was: wind from 330 degrees at 5 knots; visibility 10 miles; sky clear; temperature 13 degrees Celsius; dew point 1 degree Celsius; altimeter 30.25 inches of mercury. An autopsy was performed on the pilot by the Office of the Medical Examiner, District 1, Pensacola, Florida. According to the autopsy report, the cause of death was multiple blunt force injuries. The FAA did not perform toxicological testing on the pilot; however, toxicological testing ordered by the Office of the Medical Examiner was negative for drugs and alcohol.

Contributing factors

Pilot