N7755H

Substantial
Serious

PIPER PA-12 S/N: 12-653

Accident Details

Date
Friday, July 21, 1995
NTSB Number
ANC95LA111
Location
ANCHORAGE, AK
Event ID
20001207X03842
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

THE PILOT'S IMPROPER USE OF CARBURETOR HEAT WHICH LED TO CARBURETOR ICING AND A PARTIAL LOSS OF ENGINE POWER. FACTORS CONTRIBUTING TO THE ACCIDENT ARE PREVAILING CARBURETOR ICING CONDITIONS, AND THE PILOT'S FAILURE TO PROPERLY JUDGE THE AIRPLANE'S DISTANCE AND SPEED DURING THE FORCED LANDING.

Aircraft Information

Registration
Make
PIPER
Serial Number
12-653
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
PA-12 PA12
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
PA-12

Registered Owner (Current)

Name
GOOS LYNN
Address
47911 518 AVE #351
City
AGUILA
State / Zip Code
AZ 85320
Country
United States

Analysis

On July 21, 1995, about 1555 Alaska daylight time, N7755H, a Piper PA-12, collided with terrain during a forced landing in Anchorage and was substantially damaged. The forced landing was precipitated by a partial loss of engine power while the airplane was maneuvering. The private pilot received minor injuries and the sole passenger received serious injuries. Visual meteorological conditions prevailed and no flight plan had been filed. The personal flight was conducted under 14 CFR 91.

The pilot stated that the accident flight was the first flight since the engine was rebuilt. After a preflight inspection and successful engine run-up, the airplane departed from a private airstrip and maneuvered about 700 feet above the airstrip. The pilot reported that the "engine lost power," but did not stop. The pilot immediately descended and maneuvered to approach the airstrip and land to the north. He overshot the landing strip and purposely stalled the airplane in an effort to avoid colliding with obstructions. The airplane impacted terrain about 200 feet beyond the end of the runway and was substantially damaged.

An examination of the engine and fuel system did not reveal evidence of any mechanical deficiencies. The reported temperature and dew point near the time and place of the accident were 59 degrees F and 57 degrees F respectively. According to the Carburetor Icing Probability Chart published by the FAA (attached), the prevailing weather conditions could produce "serious icing at cruise power" in light aircraft piston engines.

The pilot stated that he had applied full carburetor heat immediately upon sensing the power loss, with no effect noted. He said the airplane could not maintain altitude, but the engine continued to run.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC95LA111