Summary
On August 20, 2014, a Raytheon Aircraft Company G36 (N636TM) was involved in an accident near Milton, FL. The accident resulted in 2 minor injuries, with 3 people uninjured out of 5 aboard. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this accident to be: The pilot's inadequate preflight planning, which resulted in an attempted takeoff over the airplane's maximum gross weight and beyond its aft center of gravity limit. Contributing to the accident was the pilot's lack of total flight experience in the aircraft make and model.
The pilot attempted the takeoff with the airplane loaded 238 pounds over the maximum gross weight of 3,833 pounds, with the center of gravity (cg) 3.3 inches aft of the aft cg limit. During the takeoff roll, the nose of the airplane lifted 10 knots prior to the recommended rotation speed for a no-flap takeoff, and witnesses described the airplane in an unstable "pitch-up" attitude before it settled back on the runway and overran the departure end, struck a ditch, and came to rest with substantial damage to the left wing and horizontal stabilizer. The pilot reported he had 1.8 hours of flight experience in the accident airplane make and model, and that there were no mechanical malfunctions with the airplane that would have precluded normal operation.
This accident is documented in NTSB report ERA14CA397. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N636TM.
Accident Details
Probable Cause and Findings
The pilot's inadequate preflight planning, which resulted in an attempted takeoff over the airplane's maximum gross weight and beyond its aft center of gravity limit. Contributing to the accident was the pilot's lack of total flight experience in the aircraft make and model.
Aircraft Information
Registered Owner (Historical)
Analysis
The pilot attempted the takeoff with the airplane loaded 238 pounds over the maximum gross weight of 3,833 pounds, with the center of gravity (cg) 3.3 inches aft of the aft cg limit. During the takeoff roll, the nose of the airplane lifted 10 knots prior to the recommended rotation speed for a no-flap takeoff, and witnesses described the airplane in an unstable "pitch-up" attitude before it settled back on the runway and overran the departure end, struck a ditch, and came to rest with substantial damage to the left wing and horizontal stabilizer. The pilot reported he had 1.8 hours of flight experience in the accident airplane make and model, and that there were no mechanical malfunctions with the airplane that would have precluded normal operation.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA14CA397