N14NP

Substantial
None

VANS RV14S/N: 140143

Accident Details

Date
Monday, September 4, 2023
NTSB Number
CEN23LA402
Location
Orchard, TX
Event ID
20230906193019
Coordinates
29.614326, -95.969194
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of an alternator belt and the builder/previous owner’s incorrect electrical wiring of the airplane’s other alternator, which resulted in a total loss of electrical and engine power.

Aircraft Information

Registration
Make
VANS
Serial Number
140143
Engine Type
Reciprocating
Year Built
2017
Model / ICAO
RV14RV14
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
RV-14A

Registered Owner (Current)

Country
United States

Analysis

On September 4, 2023, about 1100 central daylight time, an RV-14A airplane, N14NP, was substantially damaged when it was involved in an accident near Orchard, Texas. The pilot and pilot-rated passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot had purchased the airplane from its builder about one month before the accident. According to the pilot, about 10 minutes into the accident flight from Fair Weather Field (TX42), Monaville, Texas, to Texas Gulf Coast Regional Airport (LBX), Angleton/Lake Jackson, Texas, he noticed the left and right battery indications on the instrument panel turned on and off several times. About 8 minutes later, he noticed a loss of electrical power to the secondary EFIS and several other avionics, but the primary EFIS was still powered, and the engine continued to operate normally. The pilot turned back toward TX42 and flew for another 10 minutes until the airplane lost all electrical and engine power. The pilot made a forced landing to a field and the airplane came to rest upright.

Postaccident examination revealed that the airplane sustained substantial damage to the fuselage. The No. 2 alternator belt was broken. It was found inside the engine cowling, and the cowling had black rubber marks on its inside surface. The No. 1 alternator belt remained intact.

During a subsequent examination, the two batteries did not show any voltage when tested with a multimeter. The two alternators were wired such that the No. 2 alternator was the only alternator charging the batteries. When tested, the No. 2 alternator worked as expected with no issues. The examination revealed no other mechanical malfunctions or anomalies that would have resulted in a loss of electrical or engine power. The airplane was equipped with an electronic ignition and injection system.

The pilot stated that the alternator indication lights were not wired to turn on when the alternators are offline. The airplane builder told the pilot that he relied on the ammeters, which are displayed digitally on the EFIS, to show alternator functionality. The builder also told the pilot that the only indication that an alternator was working was when the needle pointed up on the corresponding ammeter.

The pilot provided accident flight data to the NTSB that he said was recorded by the airplane’s EFIS. These data showed that a battery alert was first generated about 1031, when the airplane was traveling at a ground speed of about 3 knots. The recorded data showed an increase in ground speed about 20 seconds later, followed by an increase in altitude consistent with takeoff. Intermittent battery alerts continued until about 1048. The data also showed intermittent battery alerts during a 2-minute portion of an earlier flight on the same day.

The airplane maintenance logbooks revealed that the airplane was equipped with two EarthX ETX900 13.2-volt lithium batteries, which had been installed by the airplane builder. On April 18, 2018, at airframe total time of 201.1 hours, he replaced the No. 2 alternator belt. The builder performed the airplane’s most recent annual condition inspection on February 1, 2023, about seven months before the accident, at airframe total time of 523.7 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA402