No fatalities

16 May 2019: ZENITH CH750 STOL (N750GZ) — Savannah, TN

Savannah, TN, United States

On 16 May 2019, a ZENITH CH750 STOL (registration N750GZ) was involved in an aviation accident near Savannah, TN. No fatalities were reported. Investigators recorded the probable cause as: The total loss of engine power due to a loss of all electrical power. Contributing to the accident was the inaccessible placement of the alternator circuit breaker and the construction of the airplane without a backup electrical source. This summary draws on records from NTSB; 8 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On May 16, 2019, an experimental amateur-built Zenith CH750 STOL (N750GZ) experienced an electrical failure near Savannah, Tennessee, resulting in a forced landing and substantial damage. The pilot and passenger were uninjured.

Incident Overview

On May 16, 2019, at approximately 1435 central daylight time, an experimental amateur-built Zenith CH750 STOL, registered as N750GZ, sustained substantial damage during a forced landing near Savannah-Hardin County Airport (SNH) in Savannah, Tennessee. The pilot and passenger were not injured. The flight was conducted under Title 14 Code of Federal Regulations Part 91.

Pilot's Account

According to the pilot, the preflight inspection revealed no anomalies. After engine start, the battery voltage was checked. During flight, the pilot observed a drop in the direct current (DC) electrical bus voltage from a normal value of about 13.6 volts direct current (vdc) to about 12.5 vdc. He initiated a turn back to SNH. Approximately two minutes later, the DC bus voltage dropped to 0 vdc and the engine stopped producing power. The pilot selected an open field and performed a forced landing.

Post-Accident Observations

After the accident, the pilot noted that the alternator in-line circuit breaker, located under the instrument panel, was tripped. An examination by a Federal Aviation Administration (FAA) inspector revealed substantial damage to the firewall, as well as additional damage to the nosewheel and rudder pedals. Inspection of the alternator circuit breaker indicated that its location underneath the instrument panel was not visible or accessible for reset during flight.

Electrical System Configuration

The airplane was constructed with an engine electrically dependent on a single alternator and a single battery to provide required electrical power for the fuel pump and engine ignition systems. Following the accident, the pilot installed a backup battery in the airplane.

Contributing factors

MalfunctionDesign