Summary
On May 31, 2009, a Piper PA-28-181 (N811SA) was involved in an incident near Caldwell, NJ. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot’s failure to maintain directional control of the airplane during landing. Contributing to the accident was the pilot’s failure to ensure that he could operate the rudder pedals without interference.
The pilot stated that during landing the airplane drifted to the left side of the runway prior to touchdown. He attempted to correct with right rudder application but was unable because his shoe was lodged between an object and the rudder pedal. Slight aileron input was ineffective and additional aileron correction was not applied in order to prevent the right wing from contacting the runway. As the pilot applied full power for a go-around, the left flap contacted a runway edge light. The go-around was routine and the pilot returned and executed a normal landing. The left flap and left portion of the stabilator incurred damage. The pilot stated that there were no mechanical abnormalities present with the airplane prior to the flight.
This incident is documented in NTSB report ERA09CA322. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N811SA.
Accident Details
Probable Cause and Findings
The pilot’s failure to maintain directional control of the airplane during landing. Contributing to the accident was the pilot’s failure to ensure that he could operate the rudder pedals without interference.
Aircraft Information
Registered Owner (Historical)
Analysis
The pilot stated that during landing the airplane drifted to the left side of the runway prior to touchdown. He attempted to correct with right rudder application but was unable because his shoe was lodged between an object and the rudder pedal. Slight aileron input was ineffective and additional aileron correction was not applied in order to prevent the right wing from contacting the runway. As the pilot applied full power for a go-around, the left flap contacted a runway edge light. The go-around was routine and the pilot returned and executed a normal landing. The left flap and left portion of the stabilator incurred damage. The pilot stated that there were no mechanical abnormalities present with the airplane prior to the flight.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA09CA322