NTSB Prelim: Piper PA-24 | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.10.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-Unlimited-11.06.25

AirborneUnlimited-11.07.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Wed, Feb 21, 2024

NTSB Prelim: Piper PA-24

Airplane Departed From Runway 36, And Subsequently Began A Turn Back Toward The Runway

Location: Eufaula, AL Accident Number: ERA24FA102
Date & Time: January 31, 2024, 13:25 Local Registration: N5520P
Aircraft: Piper PA-24 Injuries: 1 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

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.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (11.14.25): Marker Beacon

Marker Beacon An electronic navigation facility transmitting a 75 MHz vertical fan or boneshaped radiation pattern. Marker beacons are identified by their modulation frequency and >[...]

Aero-News: Quote of the Day (11.14.25)

“Aviation is an incredible tool for Samaritan’s Purse. After a disaster strikes, we want people to know why we are bringing life-saving supplies. We want them to know t>[...]

Classic Aero-TV: CiES All-Digital Fuel Senders

From 2024 (YouTube Edition): New Capabilities For Business Aviation CiES Corporation President Scott Philiben walked Aero-News Editor in Chief Jim Campbell through some of what set>[...]

Airborne 11.10.25: Affordable Expo Succeeds, Citation Ascend, Kenai Shuts Down

Also: Duffy Predicts ‘Mass Chaos’, Modern Skies Coalition, More Impacts, Archer Buys Hawthorne With only a few months of preparation—and minimal outside media sup>[...]

NTSB Final Report: Lancair 320

The Experienced Pilot Chose To Operate In Instrument Meteorological Conditions Without An Instrument Flight Rules Clearance Analysis: The airplane was operated on a personal cross->[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC