Casualties unknown

2001-01-27: Robinson R-22 Beta (ZS-RBM) — Farm near Bethlehem, ZA

Farm near Bethlehem, ZA

On January 27, 2001, a Robinson R-22 Beta (registration ZS-RBM) was involved in an aviation accident near Farm near Bethlehem, ZA. Investigators recorded the probable cause as: The accident was caused by the pilot's improper response to a reduction in main rotor RPM, which triggered a hard landing and a subsequent rollover. This was compounded by the pilot's lack of experience operating in high density altitude environments. This summary draws on records from the South African Civil Aviation Authority (SACAA) Accident and Incident Investigations Division.

Sourcesthe South African Civil Aviation Authority (SACAA) Accident and Incident Investigations DivisionPrimary reportUpdated 1785104676Data APIEditorial standards

A private helicopter flight ended in a rollover on a farm near Bethlehem after the pilot attempted to reposition the aircraft for hangarage.

What happened

On January 27, 2001, a Robinson R-22 Beta, registration ZS-RBM, was engaged in a private flight originating from Durban. After a refueling stop in Harrismith, the pilot proceeded to a farm near Bethlehem. Following a visit to family, the pilot decided to remain at the location overnight due to deteriorating weather conditions, which included thunderstorm activity and the potential for hail.

To protect the aircraft from the weather, the pilot intended to move the helicopter into a nearby hangar. This required repositioning the aircraft closer to the hangar structure via a low hover. During this maneuver, the pilot encountered a decay in the main rotor RPM. In response, the pilot overreacted by dumping the collective, resulting in a hard landing. The impact caused the helicopter to bounce back into the air; upon the second touchdown, the left front skid assembly failed, causing the aircraft to roll over to the left. No injuries were reported.

The investigation

The investigation focused on the sequence of events during the low hover maneuver and the environmental conditions at the time of the accident. Investigators examined the aircraft's performance during the repositioning attempt and the pilot's reaction to the loss of rotor RPM. The investigation also looked into the pilot's familiarity with high-altitude operations, noting that the density altitude at the time was approximately 8,600 feet amsl.

Findings

  • The primary cause of the accident was the pilot's overreaction to a sudden decay in main rotor RPM, which led to the hard landing and subsequent rollover.
  • A significant contributing factor was the high density altitude of 8,600 feet amsl.
  • The pilot's flying experience was primarily based in coastal regions, and they lacked sufficient familiarity with how high density altitude affects aircraft performance.

Probable cause

The accident was caused by the pilot's improper response to a reduction in main rotor RPM, which triggered a hard landing and a subsequent rollover. This was compounded by the pilot's lack of experience operating in high density altitude environments.