Mechanical & Engine Failure · NTSB WPR09LA202
ALEXANDER THOMAS P SPORTSMAN GS-2 — El Dorado HIlls, CA
| Date | April 18, 2009 |
| Location | El Dorado HIlls, CA |
| Aircraft | ALEXANDER THOMAS P SPORTSMAN GS-2 (amateur-built) |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Emergency descent Collision with terr/obj (non-CFIT) |
| Pilot age | 60 |
| Pilot total time | 1,626 hrs · Experienced |
| Time in type | 36 hrs |
| Fatalities | 1 |
Probable cause
NTSB findings
- Aircraft-Aircraft systems-Flight control system-Elevator control system-Failure - C
- Aircraft-Aircraft systems-Flight control system-Elevator control system-Incorrect service/maintenance - C
- Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Contributed to outcome
- Personnel issues-Task performance-Maintenance-(general)-Not specified - C
What happened
Witnesses monitoring the accident flight's departure airport common traffic advisory frequency reported that they heard a mayday radio transmission stating that "I've lost elevator control" and "I'm going down in some trees." Witnesses adjacent to the accident site reported hearing a loud whining noise followed by the sound of something impacting trees. One witness stated that the airplane was at a low altitude in an upright attitude when it struck trees. The airplane subsequently impacted terrain and came to rest near a residential structure where a post-crash fire consumed most of the fuselage. Post-accident examination of the wreckage revealed that the elevator torque tube was disconnected from the forward rod end bearing. The forward rod end bearing remained attached to the elevator bell crank assembly. No damage was observed on the forward torque tube rod end threads or forward rod end bearing threads. The forward torque tube rod end jam nut was observed threaded about one-half inch from the threaded rod end. The aft torque tube jam nut and torque tube rod end was observed against the aft rod end bearing. The aft torque tube rod end was slightly bent and did not allow movement. No evidence of "torque seal" was observed on the forward or aft jam nuts, rod end bearings, or torque tube assembly. No additional mechanical anomalies were noted with the recovered airframe.