Summary
On September 03, 2007, a Piper PA-34-200T (N251AS) was involved in an incident near Wilmington, DE. All 3 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 improper flare, which resulted in a hard landing. A factor to the accident was the wind gust.
The pilot of the PA-34-200T stated that the while on final approach for landing on runway 27 at his destination airport, he was advised by the control tower of "18 mph [wind] gusts out of 270" degrees. After touchdown the airplane rolled for "several yards," then "ballooned up and came down," at which time, the windshield broke. The airplane bounced once again, touched down, and rolled out, completing the landing. Post accident examination of the airplane by a Federal Aviation Administration inspector revealed that the nose landing gear "A-frame" assembly had impacted the base of the windshield after tearing through the fuselage structure located above the nose landing gear wheel well.
This incident is documented in NTSB report NYC07CA213. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N251AS.
Accident Details
Probable Cause and Findings
The pilot's improper flare, which resulted in a hard landing. A factor to the accident was the wind gust.
Aircraft Information
Registered Owner (Current)
Analysis
The pilot of the PA-34-200T stated that the while on final approach for landing on runway 27 at his destination airport, he was advised by the control tower of "18 mph [wind] gusts out of 270" degrees. After touchdown the airplane rolled for "several yards," then "ballooned up and came down," at which time, the windshield broke. The airplane bounced once again, touched down, and rolled out, completing the landing. Post accident examination of the airplane by a Federal Aviation Administration inspector revealed that the nose landing gear "A-frame" assembly had impacted the base of the windshield after tearing through the fuselage structure located above the nose landing gear wheel well. Further examination revealed that the right propeller was also damaged and the ends of the blades had been bent aft. No evidence of any preimpact malfunctions were discovered.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC07CA213