N8660K

Substantial
None

UNIVERSAL STINSON 108S/N: 108-1660

Accident Details

Date
Saturday, April 30, 2016
NTSB Number
ERA16LA173
Location
Calverton, NY
Event ID
20160501X01725
Coordinates
40.915000, -72.791946
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 maintain directional control during the landing roll.

Aircraft Information

Registration
N8660K
Make
UNIVERSAL STINSON
Serial Number
108-1660
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
108S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CHARNEWS DANIEL P
Address
1A BITTERSWEET CT
Status
Deregistered
City
CENTERPORT
State / Zip Code
NY 11721-1765
Country
United States

Analysis

On April 30, 2016, at 1000 eastern daylight time, a Universal Stinson 108, N8660K, was substantially damaged during a runway excursion while landing at the Calverton Executive Airpark (3C8), Calverton, New York. The private pilot was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight that that was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. The flight departed Lufker Airport (49N), East Moriches, New York at 0930, destined for Westmoreland Airport (49NY), Shelter Island, New York.The pilot stated that during climbout at an altitude of about 1,200 feet mean sea level, the engine began to "miss" as though it had a "partially fouled [spark] plug." He decided to perform a precautionary landing at 3C8 and attempt to remedy the problem on the ground. During the rollout after landing, a wind gust lifted the right wing and the airplane ground looped and came to rest in the grass on the left side of runway 32.

Brookhaven Airport (HWV), Shirley, New York, was located about 7 miles southwest of the accident site. At 0956 the reported weather at HWV included wind variable at 5 knots, clear skies, with 10 statute miles of visibility.

Runway 32 at 3C8 was constructed of asphalt and concrete and was 10,001 feet-long by 200 feet-wide.

An examination of the wreckage by a Federal Aviation Administration (FAA) inspector revealed that the left wing strut was bent, the left main landing gear was folded under the fuselage, the left wing tip was damaged, and the fuselage floor structure sustained substantial damage.

The pilot indicated that the engine had performed similarly on previous occasions, and he was able to correct it by performing an engine run-up. The airplane was fueled with automotive gasoline, for which it was approved; however, the applicable supplemental type certificate specifications did not permit the use of automotive fuel containing ethanol. The FAA inspector reported that the pilot had been purchasing automotive fuel that contained ethanol, and employed a "water shake" method in an attempt to remove the ethanol from the fuel before transferring it to the airplane fuel tanks.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA173