Summary
On May 31, 2012, a Schweizer 269C-1 (N1803R) was involved in an incident near Titusville, FL. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The flight instructor’s inadequate supervision and delayed remedial action during a simulated engine-out procedure, which resulted in a hard landing.
According to the certificated flight instructor (CFI), during the helicopter instructional flight, a simulated engine failure maneuver was being performed. During the descent, the engine rpm began to decrease. The anticipated approach path to the landing area required the helicopter to overfly trees. As the helicopter approached the intended landing area, the student pilot raised the collective, which further decreased the rotor rpm. The CFI lowered the collective and increased the throttle; the helicopter landed hard, bounced, landed a second time, and rolled onto its left side, which resulted in substantial damage to the tailboom. A postaccident investigation revealed no preexisting mechanical anomalies that would have precluded normal operation.
This incident is documented in NTSB report ERA12CA375. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1803R.
Accident Details
Probable Cause and Findings
The flight instructor’s inadequate supervision and delayed remedial action during a simulated engine-out procedure, which resulted in a hard landing.
Aircraft Information
Registered Owner (Historical)
Analysis
According to the certificated flight instructor (CFI), during the helicopter instructional flight, a simulated engine failure maneuver was being performed. During the descent, the engine rpm began to decrease. The anticipated approach path to the landing area required the helicopter to overfly trees. As the helicopter approached the intended landing area, the student pilot raised the collective, which further decreased the rotor rpm. The CFI lowered the collective and increased the throttle; the helicopter landed hard, bounced, landed a second time, and rolled onto its left side, which resulted in substantial damage to the tailboom. A postaccident investigation revealed no preexisting mechanical anomalies that would have precluded normal operation. Additionally, neither pilot reported any mechanical malfunctions with the helicopter.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA12CA375