N352Y

Substantial
Minor

BUHL LA 1S/N: 141

Accident Details

Date
Sunday, May 3, 2015
NTSB Number
WPR15LA156
Location
Cottage Grove, OR
Event ID
20150503X95142
Coordinates
43.804164, -123.031944
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A loss of engine power on downwind for landing due to carburetor icing, which resulted in a forced landing.

Aircraft Information

Registration
Make
BUHL
Serial Number
141
Engine Type
Reciprocating
Year Built
1931
Model / ICAO
LA 1FK12
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
LA-1

Registered Owner (Current)

Name
EVERS MELVIN D
Address
PO BOX 158
City
ELMIRA
State / Zip Code
OR 97437-0158
Country
United States

Analysis

On May 3, 2015, about 1100 Pacific daylight time, a Buhl LA 1, N352Y, collided with trees during a forced landing at Cottage Grove State Airport (61S) Cottage Grove, Oregon. The pilot/owner was operating the airplane under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91. The commercial pilot sustained minor injuries; the airplane sustained substantial damage to the wings. The local personal flight was in the traffic pattern. Visual meteorological conditions (VMC) prevailed, and no flight plan had been filed.The pilot stated that he did not intend to fly. He made several low speed taxi tests, and then began a high speed run. It was windy; after encountering a gust, the airplane unexpectedly became airborne. There was not enough room to abort the takeoff, so the pilot decided to fly the traffic pattern, and return to land. On downwind, the engine lost power; he continued straight ahead toward an open area; the right wing impacted a tree during the forced landing.

The pilot reported that the airplane was not equipped with carburetor heat, and suspected that carburetor ice could have caused the loss of power.

A Federal Aviation Administration (FAA) inspector oversaw an examination of the engine. The examination revealed no anomalies that would have precluded normal operation. A complete report is part of the public docket.

The FAA published Special Airworthiness Information Bulletin (SAIB) CE-09-35 on June 30, 2009, regarding carburetor ice prevention. The conditions encountered in this accident (ambient temperature 71 degrees F, dew point 40 degrees F, and 32 percent relative humidity) were in the area of icing at glide and cruise power, and in the area of serious icing at glide power.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR15LA156