2 fatalities

23 Feb 2022: PIPER PA-32-260 (N3952W) — Fostoria, OH

Fostoria, OH, United States

On 23 Feb 2022, a PIPER PA-32-260 (registration N3952W) was involved in an aviation accident near Fostoria, OH. 2 people were killed. Investigators recorded the probable cause as: The pilot’s loss of airplane control in night instrument meteorological conditions during the procedure turn of an instrument approach due to spatial disorientation, which resulted in a collision with terrain. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On February 22, 2022, a Piper PA32 airplane (N3952W) was destroyed and both occupants fatally injured when it crashed near Fostoria, Ohio, during an RNAV instrument approach.

History of Flight

On February 22, 2022, about 2241 eastern standard time, a Piper PA32 airplane, registration N3952W, was destroyed when it was involved in an accident near Fostoria, Ohio. The pilot and passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 business flight.

The flight was conducted as an instrument flight rules (IFR) flight from Effingham County Memorial Airport (1H2), Effingham, Illinois, to Findlay Airport (FDY), Findlay, Ohio. The filed IFR flight plan stipulated a cruise altitude of 9,000 ft mean sea level (msl), an estimated time en route of 1 hour 28 minutes with 4 hours of fuel on board.

A review of archived Federal Aviation Administration (FAA) automatic dependent surveillance broadcast data revealed that the airplane departed 1H2 about 1956 central standard time, climbed to about 7,000 ft msl, and proceeded on a relatively direct track toward DOYET, the initial approach fix for the RNAV/GPS runway 25 instrument approach.

After passing DOYET, the airplane made about a 30° left turn, consistent with a teardrop entry into the procedure turn. The airplane aligned with the outbound side of the holding pattern for about a mile before turning left again. As the airplane flew north of the published holding pattern in its final minute of flight, its altitude decreased from about 3,000 ft to about 2,600 ft before climbing back to about 3,000 ft. About 4 nm from the IAF, the airplane turned right and descended rapidly in a spiral, impacting terrain on a heading of 340°.

A review of commercially available communications data revealed that the last confirmed communication between the accident airplane and air traffic control (ATC) took place when ATC instructed the pilot to cross DOYET at or above 3,000 ft and cleared them for the RNAV runway 25 approach, to which the pilot read back the clearance and altitude restriction. Shortly thereafter, ATC attempted to contact the pilot and subsequently issued a low altitude alert, but no reply or acknowledgement was received.

A witness inside their residence described hearing an airplane low near their house. They described the noise as a loud engine or high rpm engine followed by silence. Another nearby witness saw the lights of the airplane but did not hear anything because they were in a car with the radio on. They said that at first sight, the airplane was estimated between 300 and 500 ft above ground level (agl). When they lost sight of the airplane as it descended behind houses, they estimated the altitude between 150 and 250 ft agl.

Wreckage and Impact Information

The airplane impacted a field in a relatively flat attitude and continued on a 340° track into a forest, where it collided with multiple trees and became highly fragmented. Flight control continuity could not be established due to the highly fragmented nature of the wreckage, but all lengths of control cables were accounted for at the accident location. All major pieces of the airplane were observed at the accident location.

A postaccident examination of the engine revealed no mechanical malfunctions or anomalies that would have precluded normal operation.

Additional Information

The Federal Aviation Administration’s (FAA) Airplane Flying Handbook (FAA-H-8083-3B) described some hazards associated with flying when the ground or horizon are obscured. The handbook states, in part, the following:

The vestibular sense (motion sensing by the inner ear) in particular can and will confuse the pilot. Because of inertia, the sensory areas of the inner ear cannot detect slight changes in airplane attitude, nor can they accurately sense attitude changes that occur at a uniform rate over a period of time. On the other hand, false sensations are often generated, leading the pilot to believe the attitude of the airplane has changed when, in fact, it has not. These false sensations result in the pilot experiencing spatial disorientation.

Medical and Pathological Information

The FAA Forensic Sciences laboratory performed toxicological testing of postmortem specimens from the pilot. Diphenhydramine was detected in liver and muscle, and Doxylamine was detected in muscle; the liver specimen was unsuitable for reporting a doxylamine result. Dextromethorphan was detected in liver and muscle, and the dextromethorphan metabolite dextrorphan was detected in liver (not in muscle).

Contributing factors

PilotAltitude — Not attained/maintainedHeading/course — Not attained/maintainedContributed to outcome