Runway excursion during night landing

No fatalities • Summerville, United States of America • Landing (descent or approach)

An aircraft overran a wet runway at night after the pilot landed at a speed exceeding the calculated requirements, resulting in a post-impact fire.

What happened

During a night landing on a 5,000-foot asphalt runway, the pilot attempted to land the aircraft on a wet surface under calm wind conditions. The pilot reported touching down before the 1,000-foot markers and immediately applied maximum braking pressure. While the anti-skid system began cycling, the pilot noted the response felt slower than usual. During the landing roll, the left brake suddenly grabbed, causing the aircraft to yaw left and enter a series of lateral skids. The aircraft eventually exited the runway, traveled down an embankment, and struck a rocky berm approximately 360 feet beyond the runway end. All occupants, including the pilot and passengers, exited the aircraft without injury, though a fire broke out following the impact and destroyed the cockpit, the right wing, and the center fuselage.

Findings

Investigation into the flight data was limited because thermal damage from the fire destroyed the avionics. However, ADS-B data confirmed the aircraft was on final approach at a ground speed of 120 knots, which matched the pilot's report. While the pilot used the cockpit display unit (CDU) to calculate a landing reference speed (Vref) of 120 knots, simulations using the actual environmental conditions showed that the correct Vref should have been 112 knots. Furthermore, calculations indicated that a landing at 120 knots on the wet runway would require a distance exceeding the available 5,000 feet. Specifically, a speed of 117 knots would have required 5,311 feet, and 122 knots would have required 5,794 feet. The CDU had been programmed with the runway length and would have displayed a warning that the landing field length was insufficient for those speeds.

Regarding the braking system, no mechanical failures were found that would have prevented normal operation. Although a testing anomaly involving hysteresis was noted in the power brake and anti-skid valve, the manufacturer stated this would not prevent braking or pressure release. Ultimately, the investigation concluded that the pilot landed the aircraft at a speed higher than required for the available runway length.

Probable cause

The pilot performed a landing at a speed exceeding the calculated requirements for the available wet runway length.

Frequently asked questions

What happened in the 2023-05-18 Honda HA-420 HondaJet accident near Summerville, United States of America?

An aircraft overran a wet runway at night after the pilot landed at a speed exceeding the calculated requirements, resulting in a post-impact fire.

Were there any fatalities in the 2023-05-18 Honda HA-420 HondaJet accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 2023-05-18 involved a Honda HA-420 HondaJet, registration N255HJ, operated by Upfrunt Services, at Summerville, United States of America.

What was the probable cause of the accident?

The pilot performed a landing at a speed exceeding the calculated requirements for the available wet runway length.

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