N916SR

Substantial
None

EVEKTOR AEROTECHNIK EV97S/N: 20242249

Accident Details

Date
Monday, July 29, 2024
NTSB Number
CEN24LA289
Location
Midland, TX
Event ID
20240729194799
Coordinates
31.942528, -102.201910
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot’s failure to maintain directional control during taxi due to strong wind gusts.

Aircraft Information

Registration
Make
EVEKTOR AEROTECHNIK
Serial Number
20242249
Engine Type
4-cycle
Year Built
2024
Model / ICAO
EV97EV97
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
HARMONY LSA

Registered Owner (Current)

Name
ERDMAN AVIATION LLC
Address
10510 SUPERFORTRESS AVE STE B
City
MATHER
State / Zip Code
CA 95655-4155
Country
United States

Analysis

On July 29, 2024, about 1330 central daylight time, an Evektor Aerotechnik EV97 Harmony, N916SR, was substantially damaged when it was involved in an accident near Midland, Texas. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 business flight.

The airplane was on a multi-day cross-country flight at the time of the accident. The pilot made a fuel stop at Austin Executive Airport (EDC) in Austin, Texas, two days before the accident and had the main landing gear brakes serviced because she said the brakes were sticking while taxiing. Hydraulic fluid was added to the brake system and the pilot stated that the brakes worked following the maintenance.

The airplane departed EDC on the day of the accident and landed without incident at Midland International Air and Space Port (MAF) in Midland, Texas, to refuel. The pilot reported that while taxiing from the fuel area to the runway for takeoff, the right brake became inoperative, and the airplane veered into the grass. The right main landing gear strut broke, and the right wing struck the ground, which resulted in substantial damage to the right wing.

The brake system for the main landing gear was examined and no anomalies were noted. Additionally, the steering linkages for the nose landing gear assembly were inspected and full travel was achieved.

At the time of the accident the wind was 140° at 11 knots gusting to 19 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA289