N5520P

Substantial
Fatal

PIPER PA-24S/N: 24-583

Accident Details

Date
Wednesday, January 31, 2024
NTSB Number
ERA24FA102
Location
Eufaula, AL
Event ID
20240201193731
Coordinates
31.000000, -85.000000
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Aircraft Information

Registration
Make
PIPER
Serial Number
24-583
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
PA-24PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-24-180

Registered Owner (Current)

Name
ODONNELL NATHAN RAY
Address
806 E LEE ST APT 9
City
ENTERPRISE
State / Zip Code
AL 36330-2078
Country
United States

Analysis

On January 31, 2024, about 1325 central standard time, a Piper PA-24-180, N5520P, was substantially damaged when it was involved in an accident at Weedon Field Airport (EUF), Eufaula, Alabama. The commercial pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the airport manager, she saw the pilot on the day of the accident on the ramp and they spoke briefly. She subsequently observed the airplane taxiing for departure but did not observe it takeoff. On February 1, 2024, a pilot who was taxiing for departure reported that he observed a crashed airplane at the end of runway 36. The wreckage was located about 300 feet from the departure end of runway.

Initial review of automatic dependent surveillance-broadcast (ADS-B) data revealed that the airplane departed from runway 36, and subsequently began a turn back toward the runway. The tracking data ended during the 180° turn.

The airplane came to rest oriented on a magnetic heading of about 70°. All primary flight control surfaces remained attached to the airplane. The nose of the airplane was crushed aft to the cockpit and partially separated from the fuselage. Flight control continuity was established for all primary flight control surfaces. The engine and avionics instruments were destroyed by impact. The empennage displayed crush damage and remained partially attached. The horizontal and vertical primary control surfaces remained connected to the empennage and were unremarkable. The wings remained attached to the fuselage and exhibited impact damage.

The airplane was recovered for further examination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA24FA102