FTW98FA203
1998-05-05 · OLUSTEE, Oklahoma, United States · Fatal · 1 aircraft · Status: Completed
Airport F09
Aircraft involved
Probable cause & findings
The student pilot's improper decision to attempt an 180 degree turn to return to the takeoff runway.
Factual narrative
HISTORY OF FLIGHT
On May 5, 1998, approximately 2035 central daylight time, an Engineering & Research 415-C (Ercoupe) airplane, N87125, owned and operated by a private individual, was substantially damaged when it impacted the ground in an uncontrolled descent at the Olustee Municipal Airport near Olustee, Oklahoma. Visual meteorological conditions prevailed, and a flight plan was not filed for the Title 14 CFR Part 91 local personal flight. The student pilot sustained serious injuries, and his passenger was fatally injured. The flight had originated from the Olustee Municipal Airport, about 5 minutes before the accident. During a personal interview conducted by the NTSB investigator-in-charge (IIC) and on the enclosed statements, the student pilot reported that he had completed 2 or 3 touch and go landings to runway 35. During the following takeoff, while turning left crosswind, the aircraft "shuddered" and entered what he believed was a "slip stall." He "vaguely" remembered struggling to recover the aircraft from the stall and seeing the end of the runway over his left shoulder and thinking "we have got to get back over there." Subsequently, the aircraft impacted the ground. The pilot reported that at 1700, he left work and proceeded directly home, which is approximately 0.9 mile from his office. When he arrived home, his brother, who is an electrician, was waiting for him, along with one of his brother's employees. They were there to correct an electrical problem with the house's electrical system. At this time his brother offered him a beer, which he accepted and drank. After correcting the electrical problem, they proceeded to the local convenience store. While en route back to his residence, a decision was made to go flying. Upon arrival at his residence a friend was waiting, and the friend agreed to go flying with them. They proceeded to the Olustee Municipal Airport, which is about a 16 mile drive. They arrived at the airport approximately 1800-1815, and after rolling the aircraft out of its hangar, a preflight inspection was completed. The student pilot and his friend flew to the Altus Municipal Airport, Altus, Oklahoma, for fuel. According to Altus Airport records, the aircraft arrived at 1840. The aircraft was fueled with 21 gallons of 100 octane low lead aviation fuel and departed at 1915. The student pilot reported that after flying back to Olustee, he flew around the area for about 5-10 minutes showing his friend "the river and other spectacular sites." They then flew to the airport and landed. At this time the owner of the airplane got in, and they did touch and go landings for about 10-15 minutes. Next he took his brother's employee for a short flight. He then flew his brother around the area showing him the local sights. Then "after gaining some altitude we made some turns as well as a few stalls." They then returned to the airport and landed. He then got out of the airplane for the first time since getting fuel at Altus. The student pilot further reported that his friend asked to go up a second time. "As he was my best friend, I agreed to take him up one more time. We both climbed back into the cockpit and took off." Witnesses reported observing the pilot "practicing stalls, steep turns and approaches."
PERSONNEL INFORMATION
A review of the student pilot's flight logbook revealed that his first instructional flight was on October 17, 1997. There was an endorsement for VFR solo flight for the Olustee Municipal Airport, dated January 2, 1998, and an endorsement for solo cross-country flight dated April 1, 1998. The last entry in his logbook was dated April 29, 1998, for 0.9 hour dual instruction. He had accumulated a total of 34.7 flight hours, of which 10 hours were dual, and all was in the Ercoupe.
AIRCRAFT INFORMATION
The 1946 Engineering & Research 415-C (Ercoupe) is a low wing, single engine, two-place airplane, which has fixed tricycle landing gear. The registered owner purchased the airplane at an auction in Plainview, Texas, on August 30, 1997. According to the owner, he had an agreement with the student pilot, allowing him to fly the airplane whenever he wanted. Part of this agreement was that the student pilot would pay half of the maintenance costs, which included the annual inspection. A review of the airframe and engine records did not reveal evidence of any anomalies or uncorrected maintenance defects. The aircraft's last annual inspection was completed on October 12, 1997, at an aircraft total time of 1,267.9 hours.
WRECKAGE IMPACT INFORMATION
The wreckage distribution, including ground scars, encompassed an area approximately 96 feet long. The centerline of the energy path was oriented on a heading of 130 degrees magnetic, and the aircraft came to rest upright on a heading of 170 degrees magnetic, about 320 feet from the departure end of runway 35. Examination of the aircraft revealed the forward portion of the fuselage was displaced to the left. The left wing had leading edge damage and the leading edge was twisted downward. The nose and right main landing gear were separated. The engine was found attached to its mounts. The crankshaft was rotated and continuity was confirmed to all cylinders and to the rear of the engine. Thumb compression was noted on all cylinders, and both magnetos sparked at all terminals when the crankshaft was rotated by hand. The propeller remained attached to the engine. One blade exhibited "S" type bending and chordwise scratching. The other blade was twisted toward the direction of rotation, and it had chordwise scratching. Examination of the airplane wreckage did not disclose evidence of any pre-impact structural or mechanical anomalies. Continuity was established to all flight control surfaces.
MEDICAL AND PATHOLOGICAL INFORMATION
The toxicology report from the Jackson County Memorial Hospital Laboratory, Altus, Oklahoma, revealed that 44 MG/DL (0.044%) alcohol was detected in the pilot's blood. The specimen was drawn at 2130, on May 5, 1998, the day of the accident, and analyzed at 1130, on May 6, 1998. A specimen of the pilot's blood was sent to the Civil Aeromedical Institute (CAMI), Oklahoma City, Oklahoma for testing. CAMI measured a blood alcohol concentration of 29 mg/dl (0.029%). According to Dr. Salazar, FAA Southwest Region Flight Surgeon, the blood alcohol concentration of 0.044% detected at the hospital and the 0.029% detected at CAMI "may have affected the pilot's performance, but he would not have been impaired." As a point of reference, under the provisions of the Department of Transportation/Federal Aviation Administration Aviation Alcohol Misuse Prevention Program, this level would have placed a commercial pilot in a "not ready for duty status." Relating this value to automobile "driving while impaired" levels, most states use either 0.08% or 0.1%.
SURVIVAL ASPECTS
The airplane was not equipped with shoulder harnesses for either occupant.
ADDITIONAL DATA
The aircraft wreckage was released to the owner on May 6, 1998. The student pilot with a passenger onboard, had completed 2 or 3 touch and go landings to runway 35. During the following takeoff, while turning left crosswind, the aircraft 'shuddered' and entered what the pilot believed was a 'slip stall.' He 'vaguely' remembered struggling to recover the aircraft from the stall and seeing the end of the runway over his left shoulder and thinking 'we have got to get back over there.' Subsequently, the aircraft impacted the ground. The wreckage path was oriented on a magnetic heading of 130 degrees, and the airplane came to rest approximately 320 feet from the departure end of runway 35. No structural or mechanical anomalies were observed during an examination of the airplane. According to the FAA Southwest Region Flight Surgeon, the blood alcohol concentration of 0.044% detected at the hospital and the 0.029% detected at the Civil Aeromedical Institute (CAMI) 'may have affected the pilot's performance, but he would not have been impaired.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_FTW98FA203.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing, stall, maintenance). All research papers
- Embry-Riddle Scholarly Commons 2023 · Faculty research project Reconfigurable Guidance and Control Systems for Emerging On-Orbit Servicing, Assembly, and Manufacturing (OSAM) Space Vehicles
Dynamic response to emergent situations is a necessity in the on-orbit servicing, assembly, and manufacturing (OSAM) field, because traditional on-orbit guidance and control (G&C) cannot respond effic…
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- Embry-Riddle Scholarly Commons 2023 · Conference paper The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR) An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP) NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …