Casualties unknown

2014-08-25: Cessna 414 (ZS-FPU) — Runway 06 at FAEL, ZA

Runway 06 at FAEL, ZA

On August 25, 2014, a Cessna 414 (registration ZS-FPU) was involved in an aviation accident near Runway 06 at FAEL, ZA. Investigators recorded the probable cause as: Unsuccessful forced landing due to the left main gear failure to extend on final approach as a result of the failed rigid hydraulic pipe fitted in the main wheel well. 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 Cessna 414 undergoing a maintenance test flight experienced a left main gear failure on approach. The pilot landed with nose and right gear; the aircraft veered off the runway. No injuries reported.

History of Flight

On 25 August 2014, a Cessna C414A registered ZS-FPU was flown from East London Aerodrome (FAEL) for a maintenance test flight. The aircraft had been repaired earlier for a hydraulic leak in the left main wheel well. During final approach to Runway 06, the pilot selected the undercarriage down, but the left main gear did not extend. The pilot deployed the emergency blow-down system, which extended only the nose and right main gear. After a fly-past to confirm the left gear was still retracted, the pilot landed with the two extended wheels. Once slowed, the left wing contacted the runway, and the aircraft veered left, stopping on the grass near the intersection of Runways 06/24 and 11/29.

Injuries to Persons

The pilot was the sole occupant; no passengers were carried. No injuries were reported.

Damage to Aircraft

The aircraft sustained substantial damage to the left wing, left propeller, and underbelly.

Aircraft and Pilot Information

The aircraft, a Cessna C414A (serial 414-A0505, built 1980), had 4,218.4 total airframe hours. The pilot held a Commercial Pilot Licence with type endorsement and had 542.8 total flying hours, including 248.1 hours on type. The flight was conducted under Part 43 (maintenance test flight) and was the pilot's second flight that day.

Meteorological Conditions

Wind was from 300° at 8 knots, visibility greater than 10 km, temperature 18°C. No significant cloud cover. The accident occurred during daylight at 0735Z.

Investigation

Post-accident examination revealed that a rigid hydraulic pipe in the left main wheel well had separated from the main landing gear up-lock cylinder, allowing hydraulic fluid to leak. This prevented the left main gear from extending. The supporting sleeve at the attachment to the up-lock cylinder was cracked. All other components were found properly installed. No evidence of preexisting faults or pilot incapacitation was found.

Probable cause

Unsuccessful forced landing due to the left main gear failure to extend on final approach as a result of the failed rigid hydraulic pipe fitted in the main wheel well.