3 fatalities

Swiss FFA AS 202/15-1 Bravo Crash at Samedan (HB-HFY)

Samedan, GR, CH

On October 28, 2001, a FLUG- UND FAHRZEUGWERKE AG ALTENRHEIN (FFA) AS202/15-1 (registration HB-HFY) was involved in an aviation accident near Samedan, GR, CH. 3 people were killed. Investigators recorded the probable cause as: Loss of control following inadequate flight tactics during a mountain takeoff, with contributing factors of insufficient flight preparation and exceeding the maximum takeoff weight. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-10-18Data APIEditorial standards

On 29 October 2001, FFA AS 202/15-1 Bravo HB-HFY crashed near Samedan, Switzerland, killing all three on board. The Swiss accident investigation attributed the loss of control to inadequate flight tactics during a mountain takeoff.

Incident Overview and Aircraft Details On 29 October 2001, an FFA AS 202/15-1 Bravo, registration HB-HFY, operated by Fliegerschule Altenrhein, crashed near Samedan in the canton of Graubünden, Switzerland. The aircraft was destroyed, and all three occupants—one pilot and two passengers—were killed. The accident occurred during the takeoff phase of a commercial VFR flight. ## Flight Sequence and Contributing Factors The pilot, a Swiss national born in 1948, had arranged a paid flight from Altenrhein to Samedan and back with two passengers. After a 77-minute flight, the aircraft landed at Samedan. The pilot then prepared for the return leg, choosing runway 21 for the takeoff. Witnesses reported that the aircraft struggled to gain altitude shortly after liftoff. The pilot initiated a left turn, likely to avoid the hill of San Gian, during which the aircraft rolled over its left wing and crashed. ## Investigation Findings The Swiss Federal Accident Investigation Board (Büro für Flugunfalluntersuchungen) determined that the accident was caused by the loss of control following inadequate flight tactics during a mountain takeoff. Contributing factors included insufficient flight preparation and a takeoff weight exceeding the maximum limit. The aircraft's takeoff weight at Samedan was calculated to be between 1,015 kg and 1,022 kg, exceeding the approved maximum of 999 kg. The center of gravity was also outside prescribed limits. ## Technical and Environmental Conditions The aircraft was equipped with a Lycoming O-320-E2A engine, which produced approximately 120 horsepower at the site's elevation of 1,706 meters, a 20% reduction from sea-level performance. The pilot held a valid Swiss limited commercial pilot license and had no known health impairments. The ELT was found in the off position, and no flight data recorder was installed. The investigation noted that the aircraft's performance was further affected by the high-altitude environment and the overloading condition.

Probable cause

Loss of control following inadequate flight tactics during a mountain takeoff, with contributing factors of insufficient flight preparation and exceeding the maximum takeoff weight.

Frequently asked questions

What happened in the 28 Oct 2001 FLUG- UND FAHRZEUGWERKE AG ALTENRHEIN (FFA) AS202/15-1 accident near Samedan, GR, CH?

On 29 October 2001, FFA AS 202/15-1 Bravo HB-HFY crashed near Samedan, Switzerland, killing all three on board. The Swiss accident investigation attributed the loss of control to inadequate flight tactics during a mountain takeoff.

Were there any fatalities in the 28 Oct 2001 FLUG- UND FAHRZEUGWERKE AG ALTENRHEIN (FFA) AS202/15-1 accident?

The accident was fatal, resulting in 3 fatalities.

What aircraft was involved and where did it happen?

The accident on 28 Oct 2001 involved a FLUG- UND FAHRZEUGWERKE AG ALTENRHEIN (FFA) AS202/15-1, registration HB-HFY, at Samedan, GR, CH.

What was the probable cause of the accident?

Loss of control following inadequate flight tactics during a mountain takeoff, with contributing factors of insufficient flight preparation and exceeding the maximum takeoff weight.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1783.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.