Casualties unknown

2010-04-10: Robinson R22 Beta (ZS-SCS) — At the helipad at GPS position determined as S33° 59. 07´ E18° 36.13´, ZA

At the helipad at GPS position determined as S33° 59. 07´ E18° 36.13´, ZA

On April 10, 2010, a Robinson R22 Beta (registration ZS-SCS) was involved in an aviation accident near At the helipad at GPS position determined as S33° 59. 07´ E18° 36.13´, ZA. Investigators recorded the probable cause as: Forward flex plate fractured after lift-off, resulting in a tail rotor drive shaft failure. 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

A Robinson R22 Beta training flight at Cape Town ended with substantial damage when the forward flex plate failed in fatigue, causing tail rotor drive shaft failure. No injuries occurred.

History of Flight

On 10 April 2010, a certified flight instructor and a student pilot conducted a training flight under Visual Flight Rules (VFR) from Cape Town International Aerodrome (FACT) with the intention to return. The helicopter was refueled before departure. After clearance from FACT tower, the student pilot lifted off. When the helicopter was stable and hovering at about two feet above the helipad, the instructor took control and positioned it for transition. While hover taxiing, the instructor heard a loud bang from the engine, which immediately stopped. The helicopter spun approximately 90 degrees before coming to rest on its skids. Fuel (Avgas LL100) was observed leaking; the instructor shut off the fuel valve, pulled the mixture, and turned off all switches. Both occupants vacated the helicopter unharmed.

Damage

The helicopter sustained substantial damage. Examination revealed that the forward flex plate on the gearbox sheared off. The drive shaft ripped open both main and auxiliary fuel tanks, pulled wiring out of the loom and off the frame. The aft flex plate on the free wheel bent but did not break. The clutch was fully engaged and bent to one side. Both V-belts climbed off the pulleys and sheared. The sheave alignment rod was bent and the rod end pulled off the bearing. The aft cross tube was bent from hard landing.

Metallurgical Examination

Expert metallurgical examination determined that the forward flex plate failed in fatigue on takeoff, resulting in extensive damage.

Probable Cause

The forward flex plate fractured after lift-off, resulting in a tail rotor drive shaft failure.

Personnel and Meteorological Information

The instructor held a Commercial pilot licence with 2015.6 total hours and 870 hours on type. The student pilot was not identified. Weather at the time was clear with visibility 10 km, wind from 150° at 15 knots, temperature 17°C, and few clouds.