Engine power loss leads to tail rotor strike during autorotation in Palermo

Casualties unknown • Aeroporto di Palermo Boccadifalco, IT

A Schweizer S 269C helicopter experienced a sudden engine power loss during takeoff, forcing the pilot into an emergency autorotation that resulted in a tail rotor impact.

What happened

On July 31, 2002, at approximately 14:58 UTC, a Schweizer S 26 and C helicopter, registration I-LIAO, was conducting an aerial reconnaissance mission for wildfire detection near the Boccadifalco airport in Luparello, Palermo. Shortly after takeoff, while maintaining an altitude of approximately 50 to 60 meters, the pilot heard an unidentified noise followed by a left yaw. Fearing a total engine failure, the pilot initiated an autorotative descent. During the landing, the aircraft maintained an excessive pitch attitude, causing the tail rotor to strike the ground.

The investigation

The investigation focused on the mechanical condition of the engine following the incident. Technical inspections of the engine revealed that cylinder number 2 lacked compression, with a noticeable leak occurring through the exhaust. A borescope examination identified an impact mark on the piston head. Upon further disassembly of the engine, investigators discovered that a buildup of carbon deposits on the exhaust valve stem had caused the valve to stick. This malfunction led to the valve striking the piston head, resulting in a deformation that left the valve stuck in the open position, which caused a significant loss of engine power.

Findings

  • The primary cause of the incident was a loss of engine power during takeoff.
  • Carbon deposits on the exhaust valve stem caused the valve to seize.
  • The resulting impact between the valve and the piston head deformed the valve, leaving it open and preventing proper compression.
  • The pilot's execution of the autorotative landing was improper, characterized by an excessive pitch attitude that led to the tail rotor strike.
  • The pilot sustained no injuries during the event.

Probable cause

The engine suffered a significant power loss during takeoff because carbon deposits caused the exhaust valve to stick in the open position, which subsequently induced an improperly managed autorotative landing.

Frequently asked questions

What happened in the 2002-07-31 S 269C , accident near Aeroporto di Palermo Boccadifalco, IT?

A Schweizer S 269C helicopter experienced a sudden engine power loss during takeoff, forcing the pilot into an emergency autorotation that resulted in a tail rotor impact.

What aircraft was involved and where did it happen?

The accident on 2002-07-31 involved a S 269C ,, registration I-LIAO, at Aeroporto di Palermo Boccadifalco, IT.

What was the probable cause of the accident?

The engine suffered a significant power loss during takeoff because carbon deposits caused the exhaust valve to stick in the open position, which subsequently induced an improperly managed autorotative landing.

Loading the flight search…