Summary
On November 03, 2014, a Piper PA 22-150 (N7102D) was involved in an incident near Old Bridge, 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 loss of control while landing the tailwheel-equipped airplane in gusting wind conditions, which resulted in a ground loop.
According to the pilot, while in the landing flare, the tailwheel-equipped airplane began to roll to the left. He applied right aileron to counteract the roll and provide wind correction; however, as the airplane decelerated during the landing roll, it lacked rudder authority to counteract a gust of wind from the right. The airplane ground looped 180 degrees to the right, and the left main landing gear collapsed, resulting in substantial damage to the outboard portion of the left wing and left horizontal stabilizer. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Recorded wind velocity at a nearby airport about the time of the accident was 15 knots, with gusts to 25 knots.
This incident is documented in NTSB report ERA15CA043. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N7102D.
Accident Details
Probable Cause and Findings
The pilot's loss of control while landing the tailwheel-equipped airplane in gusting wind conditions, which resulted in a ground loop.
Aircraft Information
Registered Owner (Historical)
Analysis
According to the pilot, while in the landing flare, the tailwheel-equipped airplane began to roll to the left. He applied right aileron to counteract the roll and provide wind correction; however, as the airplane decelerated during the landing roll, it lacked rudder authority to counteract a gust of wind from the right. The airplane ground looped 180 degrees to the right, and the left main landing gear collapsed, resulting in substantial damage to the outboard portion of the left wing and left horizontal stabilizer. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Recorded wind velocity at a nearby airport about the time of the accident was 15 knots, with gusts to 25 knots.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA15CA043