Rotor Vortex Ring State leads to Robinson R22 crash in Brazil

Casualties unknown • MOGI DAS CRUZES, SP, BR

A flight training maneuver involving a Robinson R22 BETA resulted in a loss of control and ground impact due to vortex ring state during a tailwind approach.

What happened

On April 16, 2003, an R22 BETA helicopter, registration PT-YBF, was conducting a local flight training mission near Mogi das Cruzes, Brazil. The flight was intended to assist a private pilot in transitioning back to active flying in preparation for a commercial pilot checkride.

During the second approach to a landing area, the pilot attempted to reduce the rate of descent by increasing collective pitch. This action triggered significant vibrations and an abnormal rate of sink. The crew attempted to regain control, but the aircraft entered a state of uncontrolled descent, performing a 1/2 turn before the left skid struck the ground. Both occupants survived the impact without injuries, but the aircraft sustained severe damage and was determined to be a total loss.

The investigation

CENIPA investigators examined the flight profiles, maintenance records, and crew qualifications. The investigation focused on the aerodynamic conditions during the approach and the crew's response to the onset of instability. Investigators analyzed the impact site, a golf course near a reservoir, and reviewed the aircraft's engine and rotor performance. While investigators considered the possibility of carburetor icing due to the proximity to a body of water, environmental data ruled this out. The investigation also looked into the training school's procedures and the instructor's management of the student during the maneuver.

Findings

  • The aircraft entered a vortex ring state during a high-angle approach.
  • The approach was conducted with a tailwind component, which delayed the movement of the turbulent wake and exacerbated the loss of lift.
  • The crew failed to account for the degradation of engine performance caused by high density altitude and high temperatures.
  • The instructor demonstrated poor judgment and delayed intervention, failing to take control effectively when the student's inputs led to an unrecoverable situation.
  • There was a lack of coordination and assertiveness between the instructor and the student during the emergency.
  • The flight training school's procedures deviated from the manufacturer's manual, specifically regarding approach angles and tailwind operations.

Probable cause

The accident was caused by the aircraft entering a vortex ring state during a steep, high-angle approach with a tailwind, compounded by the crew's failure to recognize the phenomenon and the instructor's delayed corrective actions.

Frequently asked questions

What happened in the 2003-04-16 aircraft accident near MOGI DAS CRUZES, SP, BR?

A flight training maneuver involving a Robinson R22 BETA resulted in a loss of control and ground impact due to vortex ring state during a tailwind approach.

What aircraft was involved and where did it happen?

The accident on 2003-04-16 involved a aircraft, registration PTYBF, at MOGI DAS CRUZES, SP, BR.

What was the probable cause of the accident?

The accident was caused by the aircraft entering a vortex ring state during a steep, high-angle approach with a tailwind, compounded by the crew's failure to recognize the phenomenon and the instructor's delayed corrective actions.

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