Casualties unknown

2000-12-30: Schweizer 269C (I-MAGB) — Aeroporto Modena Marzaglia, IT

Aeroporto Modena Marzaglia, IT

On December 30, 2000, a Schweizer 269C (registration I-MAGB) was involved in an aviation accident near Aeroporto Modena Marzaglia, IT. Investigators recorded the probable cause as: The incident likely occurred following a possible sudden engine power loss. The takeoff method probably contributed to the event, becoming critical for the landing performed from conditions the flight manual recommends against. This summary draws on records from the Italian National Flight Safety Agency (ANSV).

Sourcesthe Italian National Flight Safety Agency (ANSV)Primary reportUpdated 1785690840Data APIEditorial standards

A Schweizer 269C helicopter, registration I-MAGB, sustained substantial damage during a forced landing at Modena Marzaglia Airport after an aborted takeoff due to a perceived power loss. The pilot and passenger were uninjured.

Event Overview

On December 30, 2000, at approximately 14:45 UTC, a Schweizer 269C helicopter (registration I-MAGB) experienced an incident during takeoff from Modena Marzaglia Airport (LIPM). The flight, a commercial sightseeing trip with a pilot and one passenger, was interrupted shortly after departure. The helicopter executed an abnormal landing that resulted in substantial damage.

Sequence of Events

The pilot reported performing a steep climb to an altitude of about 20 meters (65 feet) when a power loss was felt. In response, the pilot initiated a forced landing onto a grass area parallel to runway 11. During the landing, the helicopter impacted the ground with its ventral section, then tilted to the left, causing the main rotor blades to strike the ground. The pilot stated that the engine was shut off by grounding the magnets. Both occupants remained uninjured.

Investigation Findings

A review of the helicopter's documentation indicated that the aircraft was in compliance with maintenance requirements and was airworthy prior to the flight. Examination of the engine after disassembly revealed no anomalies, failures, or malfunctions that could be linked to a power loss. The flight manual for the helicopter advises against performing takeoffs with low translational speed, as this reduces the likelihood of a successful outcome for the emergency procedure designed for engine failure between 7 feet and 450 feet above ground.

The investigation concluded that the steep takeoff likely induced or favored the power loss experienced when the helicopter was within the height-velocity region for which the flight manual recommends against operating. The evidence suggests a controlled impact with a medium-high vertical descent rate.

Probable cause

The incident likely occurred following a possible sudden engine power loss. The takeoff method probably contributed to the event, becoming critical for the landing performed from conditions the flight manual recommends against.

Investigation report by the Italian National Flight Safety Agency (ANSV). Original record: https://ansv.it/wp-content/uploads/2024/04/I-MAGB.pdf. This page is a structured re-presentation; facts and quotes are in the Agenzia Nazionale per la Sicurezza del Volo (ANSV), Italy.