No fatalities

Bell 206L Accident at Rand Airport (ZS-HIB)

Rand Airport next to runway 17, ZA

On October 16, 2001, a Bell 206L (registration ZS-HIB) was involved in an aviation accident near Rand Airport next to runway 17, ZA. No fatalities were reported. Investigators recorded the probable cause as: The fuel control unit to the governor tee pneumatic tube 'B' nut was not properly tightened after work was performed on the fuel control unit and vibrated loose during flight. This summary draws on records from the South African Civil Aviation Authority (SACAA) Accident and Incident Investigations Division; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe South African Civil Aviation Authority (SACAA) Accident and Incident Investigations DivisionPrimary reportUpdated 2026-10-18Data APIEditorial standards

A Bell 206L (ZS-HIB) suffered a power loss during a test flight at Rand Airport on 16 October 2001. The pilot executed an autorotation, but the helicopter bounced on landing, causing rotor-blade contact with the tail boom. No injuries were reported.

Overview and Operation Details On 16 October 2001, a Bell 206L helicopter registered ZS-HIB was conducting a test flight at Rand Airport. The aircraft had recently undergone maintenance to its gearbox and fuel control unit. The pilot-in-command, a 55-year-old private licence holder, had 21,100 total flying hours and 8,163 hours on type. Two ground engineers were also on board. ## Accident Sequence After approximately 45 minutes of satisfactory flight, the pilot began a turn to land on the helipad near the tower when a sudden loss of power occurred. The pilot performed an autorotation and selected a grass area on the eastern side of Runway 17 for landing. Upon touchdown, the right main skid contacted a rainwater furrow beside the runway, causing the helicopter to bounce. During the bounce, the main rotor blades struck the tail boom. ## Damage and Investigation Findings The accident resulted in substantial damage to the main rotor blades, tail rotor, tail boom, tail rotor drive shaft, and horizontal and vertical stabilizers. No injuries were reported. An on-site investigation revealed that the fuel control to governor tee pneumatic tube 'B' nut assembly (Part number 6893073) was completely loose, a condition that could lead to minimum fuel flow or a fuel flow shutdown. The last mandatory periodic inspection had been completed on 22 August 2001 at 7,044.40 airframe hours; the accident occurred at 7,081.00 airframe hours.

Probable cause

The fuel control unit to the governor tee pneumatic tube 'B' nut was not properly tightened after work was performed on the fuel control unit and vibrated loose during flight.

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Frequently asked questions

What happened in the 16 Oct 2001 Bell 206L accident near Rand Airport next to runway 17, ZA?

A Bell 206L (ZS-HIB) suffered a power loss during a test flight at Rand Airport on 16 October 2001. The pilot executed an autorotation, but the helicopter bounced on landing, causing rotor-blade contact with the tail boom. No injuries were reported.

Were there any fatalities in the 16 Oct 2001 Bell 206L accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 16 Oct 2001 involved a Bell 206L, registration ZS-HIB, at Rand Airport next to runway 17, ZA.

What was the probable cause of the accident?

The fuel control unit to the governor tee pneumatic tube 'B' nut was not properly tightened after work was performed on the fuel control unit and vibrated loose during flight.