N416TS

Substantial
Minor

PIPER PA-32R-301S/N: 3246100

Accident Details

Date
Thursday, June 9, 2022
NTSB Number
CEN22LA247
Location
Olla, LA
Event ID
20220614105260
Coordinates
31.533600, -92.660000
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
PIPER
Serial Number
3246100
Engine Type
Reciprocating
Year Built
1998
Model / ICAO
PA-32R-301P32R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
7
FAA Model
PA-32R-301

Registered Owner (Current)

Name
SUTTON NATHAN M
Address
345 KAROLINE ELIZABETH ST
City
HOUMA
State / Zip Code
LA 70360-6133
Country
United States

Analysis

On June 9, 2022, about 1545 central standard time, a Piper PA32R-301 airplane, N416TS, was substantially damaged when it was involved in an accident near Olla, Louisiana. The private pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot was flying under visual flight rules (VFR) from Union Parish Airport (F87), Farmerville, Louisiana, to Houma, Louisiana, with VFR flight following services provided by air traffic control. While enroute at 3,000 ft above mean sea level, an aural alarm sounded that indicated the oil pressure was low. He turned to the nearest airport for a precautionary landing and attempted to troubleshoot the issue, but the engine remained very “sluggish.” While maneuvering toward Olla Municipal Airport (L47), Olla, Louisiana, he could not maintain altitude and made an off-field landing into a field located about 7.5 miles east of L47. The airplane sustained damage to the right wing and forward section of the fuselage during the forced landing.

The airplane wreckage was transported to a secure facility in Baton Rouge, Louisiana, for further examination. Postaccident examination of the airframe and engine revealed no preimpact anomalies with the airframe, engine, or engine oil system. The engine controls were found connected and secured from the cockpit to the engine. The engine had continuity throughout its drive system; suction and compression were verified on all cylinders. The left and right magnetos were tested and produced spark to their respective spark plugs leads. The fuel servo fuel screen was clean and free of debris. The fuel injection distribution block was intact and had a small amount of fuel in it. The engine-driven fuel pump operated when tested. The oil and fuel lines were found connected and secured. Examination of the engine oil cooler and associated oil lines did not reveal any evidence of oil leakage. Oil was present in the oil lines, engine oil sump, and oil pump. The oil pump turned freely with no binding.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA247