Casualties unknown

2003-05-13: Piper PA-28R-200 (ZS-FWG) — Approximatley 500m from runway 18 and 30m to the right of the extended center line of runway 18, ZA

Approximatley 500m from runway 18 and 30m to the right of the extended center line of runway 18, ZA

On May 13, 2003, a Piper PA-28R-200 (registration ZS-FWG) was involved in an aviation accident near Approximatley 500m from runway 18 and 30m to the right of the extended center line of runway 18, ZA. Investigators recorded the probable cause as: Due to a restricted fuel flow in one of the fuel injector nozzles, the engine was unable to produce full power which caused the aircraft to lose height after take-off, resulting in a forced landing to the right of the extended center line of the runway. 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 Piper PA-28R-200 (ZS-FWG) experienced reduced engine power after takeoff from Klerksdorp due to a restricted fuel injector nozzle, resulting in a forced landing. The aircraft struck a tree, and the three occupants were hospitalized with serious and minor injuries.

Accident Overview

On 13 May 2003, at approximately 1610Z, a Piper PA-28R-200 aircraft registered ZS-FWG departed from Klerksdorp Airport (FAKD) for a night sightseeing flight. The pilot, a private license holder aged 30 with 137.6 total flying hours (5.7 on type), was accompanied by two passengers.

Flight and Engine Anomaly

After a satisfactory power check, the pilot took off from Runway 18. He rotated at 70 mph and climbed at 90 mph before retracting the undercarriage following a positive rate of climb. All engine parameters appeared normal initially. Shortly thereafter, the vertical speed indicator (VSI) showed a negative climb rate and airspeed decreased. The pilot perceived that the engine was not developing sufficient power.

Forced Landing

Unable to identify the cause of power loss, the pilot committed to a forced landing in a field obstructed by trees and vegetation. During landing, the left wing struck a tree, severing the wing from the fuselage.

Injuries and Damage

The pilot and one passenger sustained serious injuries; the other passenger sustained minor injuries and was discharged from the hospital the following day. No fatalities occurred.

Weather Conditions

Meteorological information indicated CAVOK conditions with no wind and a 3/4 moon.

Probable Cause

The accident investigation determined the probable cause to be a restricted fuel flow in one of the fuel injector nozzles, which prevented the engine from producing full power, leading to a loss of altitude after take-off and a subsequent forced landing to the right of the extended centerline of the runway.