N750GZ

Substantial
None

ZENITH CH750S/N: 75-10231

Accident Details

Date
Thursday, May 16, 2019
NTSB Number
ERA19LA177
Location
Savannah, TN
Event ID
20190519X90420
Coordinates
35.151111, -88.212219
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

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.

Aircraft Information

Registration
Make
ZENITH
Serial Number
75-10231
Engine Type
Reciprocating
Year Built
2017
Model / ICAO
CH750
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
ZENITH CH 750 STOL

Registered Owner (Current)

Name
ZIEBELL GRANT G
Address
208 PLACID COVE LN
City
MC CORMICK
State / Zip Code
SC 29835-4043
Country
United States

Analysis

On May 16, 2019, about 1435 central daylight time, an experimental amateur-built Zenith CH750 STOL, N750GZ, was substantially damaged when it was involved in an accident near Savannah-Hardin County Airport (SNH), Savannah, Tennessee. The pilot and passenger were not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91.

According to the pilot, he performed a preflight inspection of the airplane with no anomalies noted. He stated that he checked the battery voltage after engine start-up, then departed SNH. While in flight, he 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 and about 2 minutes later, the DC bus voltage dropped to 0 vdc and the engine stopped producing power. The pilot selected an open field and preformed a forced landing. After the accident, the pilot noted that the alternator in-line circuit breaker located under the instrument panel, was tripped.

Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed substantial damage to the firewall and additional damage to the nosewheel and rudder pedals. An inspection of the alternator circuit breaker revealed that its location underneath the instrument panel was not visible or accessible to reset during flight.

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

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA19LA177