Summary
On May 06, 1993, a Zeigler MONI (N10GZ) was involved in an incident near Seymour, IN. 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: An inadvertent stall. Factors relating to the accident are the major alteration of the airframe, and failure of the pilot-in- command to obtain new performance data.
On May 6, 1993, at 0945, eastern standard time, a Zeigler Moni homebuilt airplane, N10GZ, sustained substantial damage when the pilot lost control and crashed on takeoff at the Freeman Municipal Airport, Seymour, Indiana. The private pilot, and sole occupant of the airplane, received minor injuries. No flight plan was filed for the local flight, and visual meteorological conditions prevailed at the time.
The pilot stated the airplane stalled after takeoff at an altitude of about 50 feet, and contacted the ground in a nose- down attitude.
The airplane had been modified by the pilot, who was also the builder. Each wing had been shortened by 3 feet, and a heavier landing gear had been installed.
This incident is documented in NTSB report CHI93DEX01. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N10GZ.
Accident Details
Probable Cause and Findings
an inadvertent stall. Factors relating to the accident are the major alteration of the airframe, and failure of the pilot-in- command to obtain new performance data.
Aircraft Information
Registered Owner (Historical)
Analysis
On May 6, 1993, at 0945, eastern standard time, a Zeigler Moni homebuilt airplane, N10GZ, sustained substantial damage when the pilot lost control and crashed on takeoff at the Freeman Municipal Airport, Seymour, Indiana. The private pilot, and sole occupant of the airplane, received minor injuries. No flight plan was filed for the local flight, and visual meteorological conditions prevailed at the time.
The pilot stated the airplane stalled after takeoff at an altitude of about 50 feet, and contacted the ground in a nose- down attitude.
The airplane had been modified by the pilot, who was also the builder. Each wing had been shortened by 3 feet, and a heavier landing gear had been installed. No adjustment had been made to the performance data for the airplane to compensate for the increased weight or shortened wings. The airplane had not been recertificated in this configuration.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI93DEX01