No fatalities

Cessna 182Q Overruns Runway After Aborted Takeoff Near Elba, Alabama (N20BK)

Elba, AL, United States

On October 28, 2018, a Cessna 182 Q (registration N20BK) was involved in an aviation accident near Elba, AL. No fatalities were reported. Investigators recorded the probable cause as: A leak in the pitot-static system for reasons that could not be determined based on the available information, which resulted in an airspeed indication error, an aborted takeoff, and a subsequent runway overrun. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On October 28, 2018, a Cessna 182Q (N20BK) overran the runway and struck a berm after an aborted takeoff near Elba, Alabama. No injuries occurred. Postaccident testing revealed a pitot-static system leak.

Accident Overview

On October 28, 2018, at about 1500 central daylight time, a Cessna 182Q, registration N20BK, sustained substantial damage during an accident near Elba, Alabama. The flight instructor, the commercial pilot receiving instruction, and a passenger were not injured. The airplane was being operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

Sequence of Events

According to the flight instructor, all three occupants boarded the airplane after completing a preflight inspection. An engine run-up revealed no anomalies. As the airplane neared the midpoint of the 3,050-foot-long runway, the instructor noticed that the airspeed was 50 knots and was not increasing. He immediately reduced engine power to idle, aborted the takeoff, and applied the brakes. The airplane overran the runway and collided with a berm about 1,000 feet past the runway end.

Damage and Examination

An examination by a Federal Aviation Administration (FAA) inspector revealed that the nose landing gear had broken away from the strut and that the engine firewall was buckled. The airplane’s maintenance logs were not made available for review.

Postaccident Testing

A postaccident test of the pitot-static system found a leak within the system. During testing, the airspeed indicator read 40 knots when tested at 70 knots, and 60 knots when tested at 100 knots.

Contributing factors

MalfunctionContributed to outcome