No fatalities

Bell 206L-3 Forced Landing in Maize Field Near Three Rivers (ZS-HUP)

Farm near Three Rivers, ZA

On April 5, 2005, a Bell 206L-3 (registration ZS-HUP) was involved in an aviation accident near Farm near Three Rivers, ZA. No fatalities were reported. Investigators recorded the probable cause as: The pneumatic Pc tube located between the Power Turbine (PT) Governor and the Fuel Control Unit (FCU) fractured and separated at the FCU connection. 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

On 5 April 2005, a Bell 206L-3 helicopter (ZS-HUP) operated by Sapphire Air suffered an engine power loss during a hover near a power line tower. The pilot executed an autorotative landing in a maize field with no injuries.

Incident Overview and Operation Details On the morning of Tuesday, 5 April 2005, a Bell 206L-3 helicopter, registered ZS-HUP, was conducting commercial power line maintenance operations in the Three Rivers area. The aircraft was operating from a substation near Three Rivers to support maintenance on the Eskom Glockner Lethabo 2, 275-kilovolt line. The pilot-in-command held an Airline Transport Pilot licence and had a total of 7,200.0 flying hours, including 1,400.0 hours on the Bell 206L-3 type. The operator, Sapphire Air, held a valid Air Operating Certificate (No. N303D) at the time of the incident. ## Sequence of Events Prior to the first flight of the day, the pilot completed a pre-flight inspection and conducted a safety briefing with the live-line maintenance team. During the operation, maintenance personnel were being transferred from tower 43 to tower 44. After all workers had departed the helicopter, the pilot positioned the aircraft on the left-hand side of tower 43, facing in a north-westerly direction. While established in an out-of-ground effect hover at approximately 100 feet, the pilot reported that the engine suffered a power loss. Unable to maintain further flight, the pilot initiated a hovering autorotation from 100 feet and landed hard in a maize field adjacent to the power lines. The pilot, who was the sole occupant of the helicopter at the time, was not injured. ## Aircraft Maintenance and Meteorological Conditions The last Mandatory Periodic Inspection (MPI) for the aircraft was certified on 15 March 2005 at 9,361.0 airframe hours. Since that inspection, a further 55.6 hours had been flown. At the time of the accident, meteorological conditions included a surface wind from 090° at light strength, a temperature of 22°C, visibility greater than 10 km, and cloud cover of 1/8. The accident site was located on a farm near Three Rivers, with GPS coordinates of 26° 40.0’ South, 028° 01.0’ East, at an elevation of 4,500 feet AMSL.

Probable cause

The pneumatic Pc tube located between the Power Turbine (PT) Governor and the Fuel Control Unit (FCU) fractured and separated at the FCU connection. This caused the engine to spool down to ground idle (between 54-56% N1), resulting in a substantial engine power loss and the inability to maintain further flight, which led to a forced autorotative landing in a maize field.

Frequently asked questions

What happened in the 5 Apr 2005 Bell 206L-3 accident near Farm near Three Rivers, ZA?

On 5 April 2005, a Bell 206L-3 helicopter (ZS-HUP) operated by Sapphire Air suffered an engine power loss during a hover near a power line tower. The pilot executed an autorotative landing in a maize field with no injuries.

Were there any fatalities in the 5 Apr 2005 Bell 206L-3 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 5 Apr 2005 involved a Bell 206L-3, registration ZS-HUP, at Farm near Three Rivers, ZA.

What was the probable cause of the accident?

The pneumatic Pc tube located between the Power Turbine (PT) Governor and the Fuel Control Unit (FCU) fractured and separated at the FCU connection. This caused the engine to spool down to ground idle (between 54-56% N1), resulting in a substantial engine power loss and the inability to maintain further flight, which…