No fatalities

2001-09-08: Fletcher FU-24 (ZK-CMN) — Private New Zealand — Waiotira, New Zealand

Waiotira, New ZealandTakeoff (climb)

On September 8, 2001, a Fletcher FU-24 (registration ZK-CMN) operated by Private New Zealand was involved in an aviation accident near Waiotira, New Zealand during takeoff. No fatalities were reported. Investigators recorded the probable cause as: A combination of extremely soft airstrip conditions, a quartering tailwind, and underslung spreader equipment, degraded performance to the extent that the aircraft was unable to become airborne within the available length of the strip. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781202446Data APIEditorial standards

An agricultural aircraft crashed after failing to become airborne due to soft airstrip, tailwind, and underslung equipment. The pilot was seriously injured and the aircraft destroyed.

Accident Overview

An agricultural aircraft was involved in an accident at a farm airstrip. The aircraft had been flown to the strip and loaded with a small quantity of agricultural product. During the takeoff attempt, a combination of factors prevented the aircraft from achieving flight within the available strip length.

Sequence of Events

Prior to the accident, the airstrip had extremely soft conditions. The aircraft faced a quartering tailwind and was equipped with underslung spreader equipment, which further degraded performance. As the aircraft accelerated, it was unable to become airborne. The pilot jettisoned the load in an effort to reduce weight, but the aircraft subsequently struck a fence. The left wing tip and aileron scraped the ground. Despite the damage, the aircraft managed to lift off, but control was not regained, and it struck the ground again. The impact destroyed the aircraft and seriously injured the pilot.

Probable Cause

The probable cause of the accident, as determined by the official investigation, was a combination of extremely soft airstrip conditions, a quartering tailwind, and underslung spreader equipment, which degraded performance to the extent that the aircraft was unable to become airborne within the available length of the strip.