N3957X

Substantial
None

Piper PA32S/N: 32-7640003

Accident Details

Date
Monday, September 3, 2018
NTSB Number
ANC18LA069
Location
Wrangell, AK
Event ID
20180906X05209
Coordinates
55.968887, -132.423049
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The total loss of engine power due to oil starvation after an interruption of oil circulation for reasons that could not be determined based on the available evidence.

Aircraft Information

Registration
N3957X
Make
PIPER
Serial Number
32-7640003
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA32P32R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MORRIS ALLYN D
Address
24324 CRYSTAL LAKE RD
Status
Deregistered
City
WOODINVILLE
State / Zip Code
WA 98077
Country
United States

Analysis

On September 3, 2018, about 1353 Alaska daylight time, a Piper PA-32 airplane, N3957X, sustained substantial damage when it was involved in an accident near Wrangell, Alaska. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, while in level cruise flight, the engine rpm increased from a cruise power setting of 2,300 to 3,100, and he reduced the manifold pressure to correct for the high rpm. Shortly thereafter, he noticed the engine oil pressure drop and oil visible on the airplane’s windscreen, followed by a total loss of engine power. He performed an emergency landing near the high tide line in an area of seagrass. During the emergency landing, the airplane sustained substantial damage to the fuselage and left wing.

The airplane was equipped with a Lycoming IO-540-K1G5 engine. Examination of the engine revealed a large fracture hole near the Nos. 4- and 5-cylinder pads. The Nos. 4 and 5 connecting rods were fragmented, and pieces of the connecting rods and a large amount of metal debris were located within the engine and oil suction screen. The Nos. 4 and 5 connecting rods and rod bearing journals exhibited extensive mechanical damage and signatures consistent with extreme high heat.

The engine oil pump was intact with no evidence of thermal damage. The engine case halves displayed mechanical damage with multiple protrusions from the inside out. When the oil sump was removed, damaged connecting rod ends and a large amount of metal debris were discovered.

The pilot reported that the oil filter element had not been cut and examined at the last oil change, contrary to Lycoming Mandatory Service Bulletin No. 480F.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC18LA069