N6571J

Destroyed
Serious

PIPER PA-28-180S/N: 28-5024

Accident Details

Date
Wednesday, May 15, 2024
NTSB Number
CEN24LA189
Location
Hot Springs, AR
Event ID
20240516194267
Coordinates
34.478028, -93.096222
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The student pilot’s selection of an improper fuel tank selector position, which resulted in fuel starvation and a total loss of engine power. Contributing to the accident was the instructor’s inadequate oversight.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-5024
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-180P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-180

Registered Owner (Current)

Name
LIMA ALPHA LLC
Address
3307 AMITY RD
City
PEARCY
State / Zip Code
AR 71964-9689
Country
United States

Analysis

On May 15, 2024, at 1450 central daylight time, a Piper PA-28-180, N6571J, was destroyed when it was involved in an accident near Hot Springs, Arkansas. The flight instructor sustained serious injuries, and the student pilot sustained minor injuries. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 instructional flight.

The flight instructor and student pilot had completed flight maneuvers as part of the instructional flight before returning from the practice area to the departure airport for a visual approach and landing. The flight instructor said that the student pilot made a fuel tank selection change while they performed the descent checklist. The student pilot was flying the approach when the flight instructor told the student pilot to add engine power, but the engine exhibited a total loss of engine power. The flight instructor took over the flight controls, and the airplane impacted a vacant area in a residential neighborhood. The airplane was destroyed by impact forces and postcrash fire.

Postaccident examination of the airplane revealed that the fuel selector valve did not intersect any of the valve body ports. With the fuel selector valve between port positions, fuel was unable to flow downstream to the engine. There were no other preacccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA189