Main Rotor Blade Strike Causes Severe Damage to Cabri G2 During Training

Casualties unknown • LKHK, CZ

A training helicopter sustained severe damage after the main rotor blades struck the tail boom during an autorotation maneuver at Hradec Králové Airport.

What happened

On March 10, 2018, a Cabri G2 helicopter, registration OK-CAB, was performing training maneuvers at Hradec Králové Airport (LKHK). The flight was part of a type conversion training program, with a student pilot and a flight instructor performing a series of autorotations. Following an initial unsuccessful attempt at a landing without engine power recovery, the crew proceeded with a second attempt targeting taxiway Charlie.

During the final phase of the landing maneuver, the pilot executed a flare at approximately 50 ft AGL, resulting in a significant nose-up attitude of over 30 degrees. As the pilot attempted to level the aircraft at 20 ft A/GL, they prematurely raised the collective lever. This action caused a loss of rotor RPM. The helicopter touched down on the edge of the runway with the rear skid first. The impact caused the aircraft to pitch, leading the pilot to react with an energetic cyclic input. This maneuver caused the main rotor disk to tilt, resulting in the main rotor blades striking the tail boom.

The investigation

The ÚZPLN investigation examined the aircraft, the flight crew's statements, and security camera footage from the airport. The investigation established that the aircraft was in a fully airworthy condition with no mechanical failures or control malfunctions. The crew's medical certificates and licenses were valid, and the pilot was performing the maneuvers under the instructor's supervision. Technical inspections of the wreckage confirmed that the damage to the tail boom, Fenestron, and main rotor blades was solely caused by the impact of the main rotor blades.

Findings

  • The pilot, while performing an autorotation without engine power recovery, executed an excessive flare that significantly increased the aircraft's pitch.
  • The pilot raised the collective lever prematurely before the aircraft had leveled out, leading to a critical loss of rotor RPM.
  • The pilot's instinctive and energetic cyclic input following the touchdown caused the rotor disk to tilt into the tail boom.
  • The instructor, although prepared to intervene, did not react quickly enough to prevent the improper control inputs during the critical phase of the flare.
  • The pilot's previous flight experience on Robinson R22 and R44 helicopters, which utilize different landing techniques, likely contributed to the improper handling of the Cabri G2 during the maneuver.

Probable cause

The accident was caused by the main rotor blades striking the tail boom due to improper control inputs by the pilot during an autorotative landing, specifically the premature application of collective pitch and an aggressive cyclic input following touchdown.

Frequently asked questions

What happened in the 2018-03-10 CABRI G2 accident near LKHK, CZ?

A training helicopter sustained severe damage after the main rotor blades struck the tail boom during an autorotation maneuver at Hradec Králové Airport.

What aircraft was involved and where did it happen?

The accident on 2018-03-10 involved a CABRI G2, at LKHK, CZ.

What was the probable cause of the accident?

The accident was caused by the main rotor blades striking the tail boom due to improper control inputs by the pilot during an autorotative landing, specifically the premature application of collective pitch and an aggressive cyclic input following touchdown.

Investigation report by the Czech Air Accidents Investigation Institute (UZPLN). Original record: https://uzpln.gov.cz/incident/532. This page is a structured re-presentation; facts and quotes are in the Ustav pro odborne zjistovani pricin leteckych nehod (UZPLN), Czech Republic.

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