Casualties unknown

Aircraft Electrical Power Loss and Landing Gear Collapse During Flight Review (N6017P)

Hillsboro, OR, US

On May 23, 1999, a Piper PA-24-180 (registration N6017P) was involved in an aviation accident near Hillsboro, OR. Investigators recorded the probable cause as: A loose alternator drive belt, and the flight crew's decision to continue flight with a known electrical system deficiency, resulting in disabling of the aircraft electrical system and landing with the gear not down-and-locked. 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 2026-06-10Data APIEditorial standards

During a flight review, the flight instructor observed an ammeter discharge indication. Despite inability to restore charge, the crew continued. Electrical power was lost on approach, and the landing gear collapsed on landing. Post-accident examination revealed a loose alternator drive belt.

Event Summary

A flight instructor reported observing a discharge indication on the aircraft's ammeter during a flight. The crew, which consisted of a pilot undergoing a flight review and her flight instructor, were unable to restore a positive charge indication. Despite this, they elected to continue the flight.

Loss of Electrical Power

As the aircraft approached the airport, it experienced a complete loss of electrical power. The landing gear, which is electrically actuated and retractable, subsequently collapsed upon landing.

Landing Gear Indications

The crew reported that they had observed a gear-down indication prior to the loss of electrical power. However, a witness who observed the aircraft from a vantage point near the approach end of the runway reported that the landing gear was not fully extended during the final approach.

Post-Accident Examination

A post-accident inspection of the aircraft's electrical system revealed a normally functioning alternator. However, when the aircraft battery (nominally 12 volts) was used to energize the system, the bus voltage measured 11.35 volts. Additionally, the alternator drive belt was found to be loose.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18894. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.