N907W

Substantial
None

RHODES STEVEN D SR3500S/N: 173SR

Accident Details

Date
Sunday, September 17, 2023
NTSB Number
ANC23LA078
Location
NENANA, AK
Event ID
20230918193088
Coordinates
64.650753, -149.836910
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power due to fuel starvation. Contributing was the owner/builder’s inadequate maintenance.

Aircraft Information

Registration
Make
RHODES STEVEN D
Serial Number
173SR
Engine Type
Reciprocating
Year Built
2005
Model / ICAO
SR3500
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
SR3500

Registered Owner (Current)

Name
RHODES STEVEN D
Address
17500 MOUNTAINSIDE VILLAGE DR
City
ANCHORAGE
State / Zip Code
AK 99516-5733
Country
United States

Analysis

On September 16, 2023, about 1600 Alaska daylight time, an experimental amateur-built Murphy Moose SR 3500 airplane, N907W, sustained substantial damage when it was involved in an accident near Nenana, Alaska. The pilot was not injured. The airplane was operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight.

Pilot reported that, while en route in a float-equipped airplane, he noticed a slight rise in EGT with a slight decrease in fuel consumption. The engine was operating normally, but the pilot noted at a slight reduction in power output. Then the engine power began to surge followed by a rapid decrease in power. The pilot made a left turn into the wind and towards a large lake to perform an emergency landing. About 200 ft above ground level the engine lost total power. The pilot stated he did not have sufficient altitude to land on the lake; he elected to perform a forced landing to the tundra. After touchdown, the airplane slid for about 75 ft and then nosed over, sustaining substantial damage to the fuselage and wings.

Postaccident examination of the airplane revealed all the fuel lines from the gascolator to the engine fuel control unit contained fuel. The fuel inlet screen into the fuel control unit was clogged with fine nonmetallic debris which prevented fuel from entering the engine. The filter was installed about 12 to 13 years before the accident.

According to the service manual, the filter should be cleaned after a break-in period, and then after every 50 hours of operation. The manual also recommends removing and cleaning the fuel filters during condition and annual inspections. The pilot, who was also the owner/builder, was unaware of the requirements to inspect and clean the fuel control inlet filter.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC23LA078