N3710D

Substantial
None

CESSNA 182S/N: 34410

Accident Details

Date
Friday, February 20, 2009
NTSB Number
CEN09LA183
Location
Kelleys Island, OH
Event ID
20090302X10740
Coordinates
41.604721, -82.685279
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 aircraft control while landing in gusty winds due to inadequate aileron cable tension.

Aircraft Information

Registration
Make
CESSNA
Serial Number
34410
Engine Type
Reciprocating
Year Built
1957
Model / ICAO
182C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
182A

Registered Owner (Current)

Name
HILLER PAUL D
Address
14011 INDIAN HOLLOW RD
City
GRAFTON
State / Zip Code
OH 44044-9755
Country
United States

Analysis

On February 20, 2009, approximately 1100 eastern standard time, a Cessna 182A single-engine airplane, N3710D, sustained substantial damage during landing at Kelleys Island Land Field Airport, Kelleys Island, Ohio. The commercial pilot, who was the sole occupant, was not injured. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight departed Port Clinton, Ohio, at 1045.

The pilot executed a normal approach to runway 27 (2,270 feet by 35 feet, asphalt) in gusty wind conditions. During the landing flare, the airplane encountered a wind gust from the left, the airplane veered to the right, and the right wing tip struck the runway. While airborne, the pilot increased the engine throttle in an attempt to recover; however, the airplane then veered to the left. Subsequently, the airplane's nose landing gear impacted terrain adjacent to the runway and collapsed. The airplane skidded across the runway and came to rest upright. The pilot reported the wind was from 290 degrees at 15 to 20 knots, and gusting 25 to 30 knots.

Examination of the airplane by a Federal Aviation Administration inspector revealed the firewall was buckled, and the aileron control system had "slack" in the cables. The inspector reported that "not much pressure was required to move the ailerons to neutral while holding the control yoke." The inspector stated that the cable slack was not caused by damage during the accident sequence. Examination of the aileron control cables could not determine the reason for the lack of tension in the system.

The airplane underwent its most recent annual inspection on October 20, 2008. Between the time of the annual inspection and the accident, no additional maintenance to the aileron control system was noted in the maintenance records. At the time of the accident, the airplane had accumulated approximately 4 hours since the annual inspection.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA183