Preliminary report
Preliminary report released 15 March 2007
On 4 February 2007, the owner pilot of a Piper Aircraft Co PA 30 Twin Comanche aircraft, registered VH-DIC, was conducting a private flight from the Gold Coast aerodrome. The pilot was the sole occupant. Approximately 11 minutes after takeoff, at 1622 Eastern Standard Time, the pilot declared an emergency reporting an engine failure and some 15 seconds later that he was also experiencing problems with the left engine. Approximately 13 minutes after departure, the aircraft impacted the water about 100 m from Kingscliff beach, adjacent to the suburb of Casuarina, New South Wales. The pilot sustained fatal injuries.
The aircraft wreckage, including most of the lower centre fuselage, wings, and both engines and propellers, were recovered 2 days after the accident. The right propeller was recovered with the blades in the feathered position. The left propeller blades were recovered in the normal operating range with bending consistent with power being applied at the time of the accident.
The pilot held a commercial pilot license and at the time of the accident, had accrued approximately 2,544 hrs total flying time. He purchased the accident aircraft in 1996, and had accrued approximately 940 hrs in that aircraft.
At the time of the accident, the weather was generally fine.
Summary
On 4 February 2007, the owner-pilot of a Piper Aircraft Co. PA-30 Twin Comanche aircraft, registered VH-DIC, was conducting a private flight from Gold Coast Airport, Qld. The pilot was the sole occupant. Approximately 11 minutes into the flight, at 1622 Eastern Standard Time, the pilot declared an emergency reporting an engine failure and some 15 seconds later that he was also experiencing problems with the 'left engine'. Approximately 13 minutes after departure, the aircraft impacted the water about 100 m off Kingscliff beach, adjacent to the suburb of Casuarina, NSW. The pilot received fatal injuries.
Two days following the accident, the aircraft wreckage including most of the lower centre fuselage, wings, and both engines and propellers, was recovered and examined. The right propeller was recovered with the blades in the feathered position. The left propeller was recovered with the blades in the normal operating range with bending consistent with power being applied at the time of the impact with the sea.
The investigation determined that most probably the right engine stopped operating, followed by an unexplained power loss of the left engine. The aircraft airspeed then decreased below the minimum controllable airspeed during the emergency landing before power suddenly returned to the left engine causing the aircraft to pitch nose up and bank sharply to the right and impacting the water.
Occurrence summary
| Investigation number | 200700358 |
|---|---|
| Occurrence date | 04/02/2007 |
| Location | 15 km SE Gold Coast Airport |
| State | Queensland |
| Report release date | 17/04/2008 |
| Report status | Final |
| Investigation type | Occurrence Investigation |
| Investigation status | Completed |
| Mode of transport | Aviation |
| Aviation occurrence category | Propeller/rotor malfunction |
| Occurrence class | Accident |
| Highest injury level | Fatal |
Aircraft details
| Manufacturer | Piper Aircraft Corp |
|---|---|
| Model | PA-30 |
| Registration | VH-DIC |
| Serial number | 30-1775 |
| Sector | Piston |
| Operation type | Private |
| Departure point | Gold Coast airport, Qld |
| Destination | Gold Coast airport, Qld |
| Damage | Destroyed |