Summary
On February 25, 1995, a Cessna 180J (N9900N) was involved in an incident near El Paso, TX. All 2 people 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 DURING THE LANDING ROLL.
On February 25, 1995, at 1224 mountain standard time, a Cessna 180J, N9900N, was substantially damaged during landing at West Texas Airport, El Paso, Texas. The airline transport rated pilot and his pilot rated passenger were not injured. Visual meteorological conditions prevailed for the local personal flight.
The pilot reported in his written report and during an interview conducted by a Federal Aviation Administration inspector that during his second landing on runway 08 the aircraft began to "veer to the right despite rudder corrections." In an attempt to abort the landing he "added full power;" however, he "pulled the power off when it veered off the runway." Both main landing gears were separated, the fire wall buckled, and the fuselage damaged.
This incident is documented in NTSB report FTW95LA123. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N9900N.
Accident Details
Probable Cause and Findings
THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DURING THE LANDING ROLL.
Aircraft Information
Registered Owner (Current)
Analysis
On February 25, 1995, at 1224 mountain standard time, a Cessna 180J, N9900N, was substantially damaged during landing at West Texas Airport, El Paso, Texas. The airline transport rated pilot and his pilot rated passenger were not injured. Visual meteorological conditions prevailed for the local personal flight.
The pilot reported in his written report and during an interview conducted by a Federal Aviation Administration inspector that during his second landing on runway 08 the aircraft began to "veer to the right despite rudder corrections." In an attempt to abort the landing he "added full power;" however, he "pulled the power off when it veered off the runway." Both main landing gears were separated, the fire wall buckled, and the fuselage damaged. The wind was from 140 degrees at 5 knots.
An examination of the aircraft revealed no anomalies that could have contributed to the accident sequence.
During the interview the pilot revealed that he was demonstrating the aircraft to another pilot, for the owners, and that he was landing for the second time in a "normal no flap condition."
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA123