Casualties unknown

2019-05-19: Robinson R44 II (B-KTK) — Loss of Control – Inflight of Robinson R44 II over Lam Kam Road in Tai Po, Hong Kong, HK

Loss of Control – Inflight of Robinson R44 II over Lam Kam Road in Tai Po, Hong Kong, HK

On May 19, 2019, a Robinson R44 II (registration B-KTK) was involved in an aviation accident near Loss of Control – Inflight of Robinson R44 II over Lam Kam Road in Tai Po, Hong Kong, HK. This summary draws on records from the Air Accident Investigation Authority of Hong Kong (AAIA).

Sourcesthe Air Accident Investigation Authority of Hong Kong (AAIA)Primary reportUpdated 1785027978Data APIEditorial standards

On 19 May 2019, a Robinson R44 Clipper II helicopter suffered an inflight breakup near Kadoorie Gap, Hong Kong. The pilot was fatally injured and the aircraft was destroyed by fire.

Summary

On 19 May 2019, a Robinson R44 Clipper II helicopter, registration B-KTK, operated by the Hong Kong Aviation Club, broke up in flight while returning from a solo flight to Shek Kong Airfield. The accident occurred at approximately 1725 hrs local time near Lam Kam Road, Hong Kong, at an altitude of about 2,000 ft above mean sea level. The fuselage impacted terrain on a private farm and botanic garden west of Tai Mo Shan Country Park and was partially destroyed by fire. No distress call was made. The pilot sustained fatal injuries.

Flight History

The pilot was returning from a solo flight in the Tai Po area. While approaching Kadoorie Gap, the helicopter experienced an inflight breakup. The wreckage trail extended approximately 500 meters from the fuselage impact point.

Aircraft Information

The aircraft was a Robinson R44 Clipper II, registration B-KTK. It was equipped with a Lycoming engine. The helicopter was maintained by the Hong Kong Aviation Club and had a valid airworthiness certificate at the time of the accident. Various components, including the main and tail rotors, flight controls, and hydraulic system, were examined during the investigation.

Wreckage and Impact

The main wreckage was found at the impact site. The cockpit, main rotor, and other components showed extensive damage. The pitch change link was later examined metallurgically. The engine was inspected post-accident by the manufacturer.

Injuries and Damage

The pilot was fatally injured. The helicopter was substantially damaged by impact and post-crash fire. No other persons were injured.

Investigation Findings

The investigation did not determine a single probable cause. It analyzed several potential factors, including low-G flight conditions, mast bumping, and possible pilot incapacitation or distraction. The report mentioned that the right door was removed during the flight, and loose objects in the cockpit were considered. No evidence of pre-existing mechanical failure was found in the powerplant or transmission. The helicopter had no flight data recorder.

Safety Recommendation

The Air Accident Investigation Authority issued one safety recommendation following the investigation.