No fatalities

Hard Landing on Runway Overrun Following Electrical and Landing Gear Difficulties (N43797)

Gainesville, FL, US

On May 16, 1989, a Piper PA-32R-300 (registration N43797) operated by Orthopaedics Associates, Inc. was involved in an aviation accident near Gainesville, FL. No fatalities were reported. Investigators recorded the probable cause as: PILOT'S INABILITY TO PROPERLY FLARE DUE TO A HIGH SINK RATE AS A RESULT OF INSUFFICIENT AIRSPEED WHICH RESULTED IN A HARD LANDING SHORT OF AND OFF OF THE RUNWAY. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A pilot lost radio contact during a VFR cruise, experienced landing gear extension problems due to electrical failure, and made a hard landing on the overrun. Two witnesses noted a nose-high attitude and high sink rate before impact.

Incident Details

The flight was operating under visual flight rules (VFR) when radio contact with air traffic control was lost. The pilot descended and returned to Gainesville Regional Airport (GNV). During the descent, the pilot attempted to lower the landing gear. He stated that he was unable to fully extend and lock the gear using both normal and emergency procedures due to a loss of electrical power. An approach was flown to the runway with the main landing gear extended and the nose gear in an undetermined position.

Final Approach and Impact

On short final approach, the pilot realized the aircraft would be short of the runway and attempted to add engine power, but the engine did not respond. The aircraft made a hard landing on the overrun section of the runway. The impact drove the main landing gear into the wing spar, causing a partial collapse of the landing gear and major structural damage to the aircraft.

Witness Observations

Two witnesses, both certified flight instructors (CFIs), reported that during the short final they heard two applications of power before impact. However, they observed that the aircraft had developed a nose-high attitude and a high sink rate, which was not arrested prior to ground contact.

Post-Accident Examination

Maintenance personnel examined the aircraft's alternator and found that the brushes were completely burned out. The engine was later test-run by Federal Aviation Administration (FAA) personnel and was found to operate normally.

Frequently asked questions

What happened in the 16 May 1989 Piper PA-32R-300 accident near Gainesville, FL?

A pilot lost radio contact during a VFR cruise, experienced landing gear extension problems due to electrical failure, and made a hard landing on the overrun. Two witnesses noted a nose-high attitude and high sink rate before impact.

Were there any fatalities in the 16 May 1989 Piper PA-32R-300 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 16 May 1989 involved a Piper PA-32R-300, registration N43797, operated by Orthopaedics Associates, Inc., at Gainesville, FL.

What was the probable cause of the accident?

PILOT'S INABILITY TO PROPERLY FLARE DUE TO A HIGH SINK RATE AS A RESULT OF INSUFFICIENT AIRSPEED WHICH RESULTED IN A HARD LANDING SHORT OF AND OFF OF THE RUNWAY.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X28378. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.