Casualties unknown

2003-10-26: Schweizer 269C (N191GC) — Ann Arbor, MI

Ann Arbor, MI, US

On October 26, 2003, a Schweizer 269C (registration N191GC) was involved in an aviation accident near Ann Arbor, MI. Investigators recorded the probable cause as: The loss of engine power due to carburetor ice. Weather conditions conducive to the formation of carburetor ice and a roadway were contributing factors. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A helicopter was substantially damaged during a hard landing after the engine lost power and the flight instructor initiated an autorotation. Post-accident inspection found no anomalies, and weather conditions were conducive to carburetor icing.

Incident Overview

A helicopter sustained substantial damage during a hard landing following a loss of engine power and subsequent autorotation. The flight instructor reported that shortly after takeoff and within two miles of the departure airport, the helicopter suddenly yawed to the left and the engine began to uncontrollably increase and decrease speed. He noted that it sounded as if the throttle was being rolled on and off. No warning lights were illuminated.

Pilot Actions

The instructor took control of the helicopter and instructed the dual student to apply carburetor heat. However, the engine continued to rev and was "making a popping sound, like it was backfiring." The instructor observed a drop in rotor speed and elected to initiate an autorotation at an estimated altitude of 500 feet above ground level. He described the safest landing spot as a paved road in a subdivision, where the helicopter struck the ground hard, resulting in damage.

Post-Accident Inspection

A post-accident inspection revealed no anomalies. The engine was subsequently removed and torn down, but no abnormalities were found during disassembly and examination.

Weather Conditions

Weather conditions recorded at the departure airport approximately 20 minutes after the accident included a temperature of 9°C and a dew point of 1°C. Data concerning the probability of carburetor icing was obtained from Transport Canada. The conditions bordered regions of serious icing at any power setting and moderate icing at cruise power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20031107X01874. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.