N7894H

Substantial
None

Piper PA-12 S/N: 12-800

Accident Details

Date
Sunday, September 14, 1997
NTSB Number
ANC97LA137
Location
HEALY, AK
Event ID
20001208X08762
Coordinates
63.680572, -150.030670
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's inadequate preflight which failed to detect water contamination in the fuel tanks. Factors were the worn gaskets on the fuel tank caps, and the pilot's decision to abort the partial power precautionary landing.

Aircraft Information

Registration
N7894H
Make
PIPER
Serial Number
12-800
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
PA-12 PA12
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BURDEAUX JAMES III
Address
215 S LAUREL ST
Status
Deregistered
City
POST FALLS
State / Zip Code
ID 83854-9685
Country
United States

Analysis

On September 14, 1997, at 0830 Alaska daylight time, a Piper PA-12 airplane, N7894H, sustained substantial damage when it nosed over during a precautionary landing on an 800 foot long gravel strip on the Moody River, about 20 miles east of Healy, Alaska. The airline transport certificated pilot was uninjured. The flight was conducted under 14 CFR Part 91 as a personal, local flight, and departed the Healy River Airport, Healy, at 0800. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed.

The pilot stated in an interview with the NTSB investigator, that during climb to cruise, the engine rpm began to decrease. He said that application of carburetor heat, and switching magnetos did not correct the problem. The pilot indicated that he was making a precautionary landing at an 800 foot landing strip, and that horses were on the strip. After flying over the horses, the airplane landed on the remaining strip and bounced. The pilot attempted to abort the landing, the landing gear contacted a berm, and the airplane nosed over.

The NTSB investigator interviewed the persons who recovered the airplane. They reported an unknown quantity of water in the fuel, and worn fuel tank cap gaskets.

The engine was tested at an engine shop in Anchorage, Alaska, and witnessed by an FAA airworthiness inspector. The engine produced a static rpm of 1,900 rpm, which is the minimum required by the type certificate. The inspector stated that cylinder compression was low, and the engine was "tired."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC97LA137