No fatalities

Main Rotor Blade Deformation on Robinson R44 at Grand Central (ZS-RAX)

Grand Central Aerodrome (FAGC), ZA

On October 2, 2006, a Robinson R44 Raven II (registration ZS-RAX) was involved in an aviation accident near Grand Central Aerodrome (FAGC), ZA. No fatalities were reported. Investigators recorded the probable cause as: It is believed that the main rotor blade Serial # 2981C was subjected to a downwards load at a place and time that could not be determined. This resulted in the stretching of the blade upper skin. 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 2026-10-18Data APIEditorial standards
Aircraft registered ZS-RAX
Aircraft registered ZS-RAX. Photo: Bob Adams from Amanzimtoti, South Africa / CC BY-SA 2.0, via Wikimedia Commons

A Robinson R44 Raven II experienced severe main rotor blade deformation after the pilot noted a low-frequency vibration. Inspection revealed bending and wrinkling of blade serial #2981C and damage to the teeter stop. The manufacturer attributed the damage to mishandling.

Incident Overview

On 2 October 2006, at approximately 1200Z, a Robinson R44 Raven II helicopter (registration ZS-RAX) operated by a private pilot departed from Cullinan for a return flight to Grand Central Aerodrome (FAGC). The pilot, who was also the owner of the helicopter, had flown from Grand Central to Cullinan earlier that morning. During the morning flight, he noticed a low-frequency vibration but attributed it to turbulence. On the return flight later in the afternoon, the vibration persisted and, according to the pilot, increased in amplitude.

Landing and Inspection

After an uneventful landing at Grand Central, the pilot requested a maintenance engineer to inspect the helicopter and described the vibration concern. During the inspection of the main rotor blades, one blade (serial number 2981C) exhibited severe deformation, including bending of the blade and wrinkling on the upper skin surface. Damage was also found on the teeter stop of the main rotor assembly associated with that blade. The other main rotor blade showed no signs of damage or deformation.

Manufacturer Evaluation

The helicopter manufacturer was consulted, and the evidence was forwarded for evaluation. According to the manufacturer, this was not an isolated case. They stated that the damage could be attributed to mishandling or manhandling of the blade by a person who did not comply with the placard warning located on the underside of each main rotor blade tip, which reads: "Never Pull Down/Push Up Opposite Blade" (Pilot’s Operating Handbook, Section 2, Page 2-11).

Pilot and Aircraft Information

The pilot held a valid private pilot’s license with the aircraft type endorsed. He had 88.0 total flying hours, all on the Robinson R44 type, and was 37 years old. The aircraft had accumulated 20.0 hours since new at the time of the event and held a valid Certificate of Airworthiness. No injuries or fatalities occurred; there was one person on board (the pilot) and none were injured or killed.

Weather Conditions

Surface wind was 350° at 11 knots, temperature 25°C, visibility greater than 10 kilometers, and conditions were CAVOK (clear and visibility OK).

Probable cause

It is believed that the main rotor blade Serial # 2981C was subjected to a downwards load at a place and time that could not be determined. This resulted in the stretching of the blade upper skin. Subsequently the in-flight lifting loads bowed the main rotor blade upward, wrinkling the upper skin and caused a condition of severe low frequency vibration in-flight.

Frequently asked questions

What happened in the 2 Oct 2006 Robinson R44 Raven II accident near Grand Central Aerodrome (FAGC), ZA?

A Robinson R44 Raven II experienced severe main rotor blade deformation after the pilot noted a low-frequency vibration. Inspection revealed bending and wrinkling of blade serial #2981C and damage to the teeter stop. The manufacturer attributed the damage to mishandling.

Were there any fatalities in the 2 Oct 2006 Robinson R44 Raven II accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 2 Oct 2006 involved a Robinson R44 Raven II, registration ZS-RAX, at Grand Central Aerodrome (FAGC), ZA.

What was the probable cause of the accident?

It is believed that the main rotor blade Serial # 2981C was subjected to a downwards load at a place and time that could not be determined. This resulted in the stretching of the blade upper skin. Subsequently the in-flight lifting loads bowed the main rotor blade upward, wrinkling the upper skin and caused a…