N270JS

Substantial
None

Piper J5AS/N: 5-18

Accident Details

Date
Sunday, December 1, 2002
NTSB Number
ANC03LA016
Location
Soldotna, AK
Event ID
20021212X05600
Coordinates
60.476112, -151.032501
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 failure to remove all water from the airplane's fuel supply during the preflight inspection, which resulted in a loss of engine power and subsequent hard landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
5-18
Engine Type
Reciprocating
Year Built
1940
Model / ICAO
J5AJ5
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
J5A

Registered Owner (Current)

Name
AUBIN CAROL
Address
5995 COUNTY RD 210
City
BANGS
State / Zip Code
TX 76823
Country
United States

Analysis

On December 1, 2002, about 1200 Alaska standard time, a Piper J5A airplane, N270JS, sustained substantial damage when the main landing gear collapsed during an emergency landing following a loss of engine power at the Soldotna Airport, Soldotna, Alaska. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, at the time of the accident. The solo commercial pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on December 9, the pilot said he had taken off on runway 07, and started a right climbing turn, when the engine lost power. The pilot said he applied carburetor heat, and checked the position of the fuel tank selector, but he could not restart the engine. He said he was about 200 feet above ground level, and turned toward the runway. He said the airplane landed hard on the runway, the left main landing gear collapsed, and the left wing struck the runway. The pilot said there were no known mechanical anomalies with the airplane prior to the accident, however, he said the mechanic who recovered the airplane removed more than a pint of water from the right wing fuel sump. The pilot said he fueled the airplane with 87-octane auto gas from 5-gallon cans prior to the flight, and stated he should have strained the fuel through a water trap 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# ANC03LA016