Probable cause
The pilot's excessive pitch attitude, which resulted in an aerodynamic stall during the takeoff initial climb. Contributing to the accident was the pilot’s failure to comply with weight and balance limitations.
NTSB analysis
Several witnesses reported observing the airplane become airborne about two-thirds of the way down the departure runway. It then pitched up to a nose-high attitude of at least 20 degrees, leveled off about 40 feet above ground level, pitched up again to about the same pitch attitude, and subsequently descended behind a tree line with a high sink rate. Another witness reported seeing the airplane come over the tree line behind his residence and impact the ground in a nose-low attitude. A postaccident examination of the airplane and engine revealed no mechanical malfunctions or failures that would have precluded normal operation. The witness observations are consistent with the pilot attempting to climb at too steep a pitch angle, which resulted in an aerodynamic stall. According to calculations, the airplane’s weight was about 110 pounds over the maximum allowable takeoff weight, which would have resulted in reduced climb performance.
Text from the NTSB. Open the NTSB docket for ERA11FA348 for the full record.
Event
- Date
- Jun 18, 2011
- Type
- Accident
- Place
- Guntersville, Alabama
- Nearest airport
- Guntersville Municipal Airport (8A1)
- Highest injury
- Fatal
- Fatal injuries
- 3
- Serious injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Piper PA-28-140
- N-number
- N1803T
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.