Summary
On July 23, 1995, a Bellanca 17-31ATC (N500BT) was involved in an incident near Hico, 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 ATTAIN THE PROPER TOUCHDOWN POINT AND THE DELAYED GO-AROUND.
On July 23, 1995, at 1000 central daylight time, a Bellanca 17-31ATC, N500BT, collided with a fence during an aborted landing near Hico, Texas. The airline transport rated pilot/operator and one passenger were not injured, and the airplane sustained substantial damage. Visual meteorological conditions prevailed and no flight plan was filed. The airplane departed Conroe, Texas, at 0850 for the Title 14 CFR Part 91 personal flight.
This incident is documented in NTSB report FTW95LA311. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N500BT.
Accident Details
Probable Cause and Findings
THE PILOT'S FAILURE TO ATTAIN THE PROPER TOUCHDOWN POINT AND THE DELAYED GO-AROUND.
Aircraft Information
Registered Owner (Historical)
Analysis
On July 23, 1995, at 1000 central daylight time, a Bellanca 17-31ATC, N500BT, collided with a fence during an aborted landing near Hico, Texas. The airline transport rated pilot/operator and one passenger were not injured, and the airplane sustained substantial damage. Visual meteorological conditions prevailed and no flight plan was filed. The airplane departed Conroe, Texas, at 0850 for the Title 14 CFR Part 91 personal flight.
The pilot reported his touchdown on the 2,300 foot grass strip "was long so I elected to go around," and "upon rapid application of power, engine hesitated." During a telephone interview, conducted by the investigator-in-charge, the pilot stated "the aircraft did not accelerate properly" and became airborne with the "stall warning horn going off." The pilot further stated he then turned left to "avoid trees" at the end of the runway and, subsequently, the airplane impacted a fence.
A Federal Aviation Administration inspector examined the airplane and reported the outboard section of the left wing was severed, the right wing spar was cracked, and the fuselage was deformed. All three propeller blades were bent toward the cambered side approximately 90 degrees and displayed chordwise scratching and gouging.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA311