Casualties unknown

2001-06-29: Beech F33A (ZS-INH) — 5nm SE of Kromdraai near the Witbank mines, ZA

5nm SE of Kromdraai near the Witbank mines, ZA

On June 29, 2001, a Beech F33A (registration ZS-INH) was involved in an aviation accident near 5nm SE of Kromdraai near the Witbank mines, ZA. Investigators recorded the probable cause as: The camshaft fractured at the number 3 camshaft bearing machined oil transfer pick up point causing the CSU (constant speed unit) bevel gear to become ineffective and the propeller to overspeed with a partial loss of power. 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

On 29 June 2001, a Beech F33A (ZS-INH) experienced a propeller overspeed after a camshaft fracture, forcing a landing near Witbank. The aircraft was substantially damaged; the pilot was not injured.

Accident Details

On 29 June 2001, at 1100Z, a Beech F33A aircraft, registration ZS-INH, departed Grand Central Aerodrome on a private flight to Nelspruit Aerodrome. While near Witbank, the pilot suddenly experienced a propeller overspeed condition. As Witbank Aerodrome was beyond gliding distance, the pilot executed a forced landing on an open field near the Witbank coal mine. During the landing roll, the aircraft traversed a ditch, causing the nose landing gear to separate, the left main landing gear to collapse, and the propeller to contact the ground. The aircraft sustained substantial damage, but the pilot was not injured. The accident occurred during daylight conditions with fine weather.

Aircraft Information

The Beech F33A (ZS-INH) had a last mandatory periodic inspection (MPI) at a total of 3488.53 airframe hours, and the accident occurred 65.53 hours after that MPI and after the engine was overhauled. The pilot held a private pilot license with a total of 148.10 flying hours, of which 60.60 hours were on type. The license was valid.

Probable Cause

The camshaft fractured at the number 3 camshaft bearing machined oil transfer pick-up point, causing the constant speed unit (CSU) bevel gear to become ineffective. This resulted in the propeller overspeed with partial loss of power. The subsequent forced landing on an open field led to substantial damage to the aircraft.