N201MM

Substantial
Minor

MOONEY M-18C 55S/N: 357

Accident Details

Date
Friday, May 26, 2023
NTSB Number
WPR23LA202
Location
Napa, CA
Event ID
20230530192263
Coordinates
38.297833, -122.255480
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s failure to use carburetor heat, which resulted in a loss of engine power due to carburetor icing and a subsequent impact with terrain during a forced landing.

Aircraft Information

Registration
Make
MOONEY
Serial Number
357
Engine Type
Reciprocating
Year Built
1955
Model / ICAO
M-18C 55
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
M-18C 55

Registered Owner (Current)

Name
HARMS KAREN
Address
2401 BEACH ST
City
NAPA
State / Zip Code
CA 94558-3625
Country
United States

Analysis

On May 25, 2023, about 1846 Pacific daylight time, a Mooney M-18C, N201MM, was substantially damaged when it was involved in an accident near Napa, California. The sole occupant on board sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he departed Ed Carlson Memorial Field - South Lewis County Airport (KTDO), Toledo, Washington, for a multi-leg cross-country flight destined for Napa County Airport (KAPC). During the approach to land at KAPC, about 8 miles north of the airport and 3,000 ft agl, the engine lost all power. The pilot cycled the throttle control to full, but the engine did not restart and the propeller continued to windmill. He then declared an emergency and initiated a forced landing onto an open field about 5 miles north of runway 19R. During the landing roll on unimproved terrain, the left wing struck a large rock and came to rest nose down. Subsequently, the left wing sustained substantial damage. Recovery of the airplane revealed that the airplane had about 13 gallons of fuel in its main tank and 7 gallons in its auxiliary tank.

A postaccident examination of the airplane and engine did not reveal any preimpact mechanical anomalies. The fuel system was traced from each wing tank to the carburetor at the engine through the fuel selector, which rotated normally and was unobstructed. The fuel lines that had not been damaged from impact or removed to transport the airplane were secure.

Mechanical continuity of the engine was established throughout the rotating group, valvetrain, and accessory section as the crankshaft was manually rotated at the propeller by hand. Thumb compression was achieved at all four cylinders and the valves displayed normal lift when the crankshaft was rotated. Examination of the cylinders’ combustion chamber interior components using a lighted borescope revealed normal piston face and valve signatures, and no indications of catastrophic engine failure.

At 1754, the weather reported at KAPC, about 6 miles south of the accident site, included a temperature of 63°F and a dew point 52°F; the calculated relative humidity was about 67%. Review of the icing probability chart contained within FAA Special Airworthiness Information Bulletin CE-09-35 revealed that the atmospheric conditions at the time of the accident were "conducive to serious icing at glide [idle] power." The pilot added that he did not use carburetor heat during the descent and approach into KAPC and that he should have used a prelanding checklist.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR23LA202