Casualties unknown

2002-02-12: HS-125-400B (ZS-JBA) — North-East of the dispersal ramp at Lanseria, ZA

North-East of the dispersal ramp at Lanseria, ZA

On February 12, 2002, a HS-125-400B (registration ZS-JBA) was involved in an aviation accident near North-East of the dispersal ramp at Lanseria, ZA. Investigators recorded the probable cause as: The hydraulic system was not pressurised during the pre-flight inspection of the aircraft. The chocks were therefore removed without adequate hydraulic system pressure available. 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

An HS-125-400B, ZS-JBA, rolled forward at Lanseria after the pilot assumed the hydraulic accumulator was pressurized, leading to removal of chocks without sufficient brake pressure. No injuries or fatalities occurred.

Accident Details

On 12 February 2002 at 0600 Z, an HS-125-400B aircraft registered as ZS-JBA was involved in a ground incident at Lanseria Airport (FALA). The aircraft, operating a commercial flight, was parked on the international departures apron, ready for a flight to Blantyre, Malawi. There were four people on board (2 crew and 2 passengers). No injuries or fatalities were reported.

Sequence of Events

According to the investigation report, the pilot assumed that the engineer had pressurised the hydraulic accumulator and therefore did not inspect it personally. When the passengers arrived, the pilot entered the aircraft and began internal pre-start checks. The co-pilot removed the chocks after boarding the passengers, closed the door, and then started to brief the passengers. At that moment, the pilot noticed that the aircraft was rolling forward. Attempts to stop the aircraft were unsuccessful. The aircraft rolled forward, narrowly missed a hangar and a parked Bell Long-ranger helicopter next to the hangar, crossed the taxiway, and finally stopped after entering a ditch between the taxiway and the runway.

Hydraulic System Inspection

Subsequent testing found that the operation of the hydraulic system was satisfactory. The hand pump was used to pressurise the system, after which the brakes could be applied successfully. This indicated that the lack of hydraulic pressure at the time of the incident was due to the system not being pressurised during the pre-flight inspection.

Probable Cause

The probable cause, as stated in the report, was that "the hydraulic system was not pressurised during the pre-flight inspection of the aircraft. The chocks were therefore removed without adequate hydraulic system pressure available."