N16253

Substantial
Minor

PIPER PA32S/N: 32-7340080

Accident Details

Date
Friday, November 17, 2023
NTSB Number
CEN24LA039
Location
Ozark, MO
Event ID
20231120193403
Coordinates
36.996031, -93.248258
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A reported total loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
PIPER
Serial Number
32-7340080
Engine Type
Reciprocating
Model / ICAO
PA32P32R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
PA-32-300

Registered Owner (Current)

Name
QUINCY AIRCRAFT LLC
Address
1030 SPRING LAKE CT
City
QUINCY
State / Zip Code
IL 62305-6094
Country
United States

Analysis

On November 17, 2023, about 1524 central standard time, a Piper PA32-300 airplane, N16253, was substantially damaged when it was involved in an accident near Ozark, Missouri. The pilot received minor injuries. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot reported the airplane’s four fuel tanks were full after refueling before departing the Quincy Regional Airport–Baldwin Field (UIN), Quincy, Illinois. The airplane departed and flew a total of 30 minutes on the left tank, 30 minutes on the left tip tank, and about 20 to 25 minutes on the right tip tank, when the engine sustained a total loss of power. The pilot switched to the right main tank and attempted to restart the engine. Unable to restore engine power, the pilot performed a forced landing to a field. During the approach to landing, the airplane collided with a power line, and the airplane subsequently impacted terrain and came to rest inverted.

The airplane sustained substantial damage to the fuselage and wings. The responding Federal Aviation Administration inspector confirmed that adequate fuel was found in all the fuel lines and fuel tanks except for the left tip tank, which was breached. The fuel selector operated normally, and the selector tank position detents were identified while rotating the selector.

A postaccident examination of the engine did not find any mechanical anomalies. Residual fuel found in the fuel servo tested negative for water. When functionally tested, the magnetos would not produce spark, as water was noted in the magnetos. Since the accident occurred, the wreckage had been stored outside.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA039