N751DW

Substantial
None

CESSNA 172RGS/N: 172RG1002

Accident Details

Date
Wednesday, May 22, 2024
NTSB Number
CEN24LA211
Location
Chandeleur Island, LA
Event ID
20240606194406
Coordinates
29.836600, -88.839000
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A fatigue failure of the engine oil pressure line, which resulted in the loss of engine oil during the flight and subsequent damage to the nose landing gear support structure during the precautionary landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
172RG1002
Engine Type
Reciprocating
Year Built
1981
Model / ICAO
172RGC72R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172RG

Registered Owner (Current)

Name
GASKINS FRANK E
Address
225 SECRETARIAT CT
City
ASHLAND
State / Zip Code
VA 23005-2434
Country
United States

Analysis

On May 22, 2024, about 0653 central daylight time, a Cessna 172RG airplane, N751DW, was substantially damaged when it was involved in an accident near Chandeleur Island, Louisiana. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 aerial observation flight.

The pilot reported that about an hour and twenty minutes into the flight he smelled smoke and noticed that the oil pressure was decreasing. He diverted to Chandeleur Island for a precautionary landing. By that time, the oil pressure had dropped to zero and the cabin was filling with smoke. He landed on a beach, and the nose landing gear dug into the sand and collapsed. The landing gear well structure sustained substantial damage during the precautionary landing.

A postaccident examination determined that the oil pressure line from the engine to the firewall fitting had fractured. The line was bent about 360° near mid-span, and the line was fractured within the bent segment. Metallurgical examination revealed that the fracture surface exhibited features consistent with fatigue. The origin was located at the exterior surface of the tube at the outside of the 360°bend. The crack progressed through the thickness of the tube wall and then circumferentially to final fracture at the opposite side of the tube.

Airplane maintenance records revealed that the engine had been overhauled and was reinstalled on the airframe about one month before the accident. The mechanic noted that the oil line was visually inspected for condition, and there was no corrosion, worn areas, dents, or nicks on the line. As a result, the oil line was reinstalled on the airplane after the overhaul. The airplane had accumulated 119 hours since the engine overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA211