Jandakot - Jandakot

On August 11, 2003 at 03:37 PM, Jandakot - Jandakot experienced a crash involving Cessna 404 Titan, operated by Fugro Spatial Solutions, with the event recorded near Jandakot Western Australia.

The flight was categorized as survey / patrol / reconnaissance and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

6 people were known to be on board, 2 fatalities were recorded, 4 survivors were identified or estimated. This corresponds to an estimated fatality rate of 33.3%.

Crew on board: 1, crew fatalities: 0, passengers on board: 5, passenger fatalities: 2, other fatalities: 0.

The listed crash cause is technical failure. The aircraft took off from runway 24 right (24R) at Jandakot Airport, WA. One pilot and five passengers were on board the aircraft. The flight was being conducted in the aerial work category, under the instrument flight rules. Shortly after the aircraft became airborne, while still over the runway, the pilot recognized symptoms that he associated with a failure of the right engine and elected to continue the takeoff. The pilot retracted the landing gear, selected the wing flaps to the up position and feathered the propeller of the right engine. The pilot later reported that he was concerned about clearing a residential area and obstructions along the flight path ahead, including high-voltage powerlines crossing the aircraft’s flight path 2,400 m beyond the runway. The aircraft was approximately 450 m beyond the upwind threshold of runway 24R when the pilot initiated a series of left turns. Analysis of radar records indicated that during the turns, the airspeed of the aircraft reduced significantly below the airspeed required for optimum single-engine performance. The pilot transmitted to the aerodrome controller that he was returning for a landing and indicated an intention to land on runway 30. However, the airspeed decayed during the subsequent manoeuvring such that he was unable to safely complete the approach to that runway. The pilot was unable to maintain altitude and the aircraft descended into an area of scrub-type terrain, moderately populated with trees. During the impact sequence at about 1537, the outboard portion of the left wing collided with a tree trunk and was sheared off. A significant quantity of fuel was spilled from the wing’s fuel tank and ignited. An intense postimpact fire broke out in the vicinity of the wreckage and destroyed the aircraft. Four passengers and the pilot vacated the aircraft, but sustained serious burns in the process. One of those passengers died from those injuries 85 days after the accident. A fifth passenger did not survive the post-impact fire.

Aircraft reference details include registration VH-ANV, MSN 404-0820, year of manufacture 1981.

Geospatial coordinates for this crash are approximately -32.0977°, 115.8737°.