No fatalities

Serious Incident Involving Schweizer S 269C at Caresana (D-ALTG)

Aeroporto di Roma Fiumicino, IT

On January 26, 2003, an A320, (registration D-ALTG) was involved in an aviation accident near Aeroporto di Roma Fiumicino, IT. No fatalities were reported. Investigators recorded the probable cause as: Technical factor, likely due to a strong stress. This summary draws on records from the Italian National Flight Safety Agency (ANSV).

Sourcesthe Italian National Flight Safety Agency (ANSV)Primary reportUpdated 2026-10-18Data APIEditorial standards
Aircraft registered D-ALTG
Aircraft registered D-ALTG. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

On 27 May 2002, a Schweizer S 269C helicopter experienced strong tail rotor vibrations during an agricultural spraying flight near Caresana, Italy. The pilot performed a precautionary off-field landing; investigation found damage to a tail rotor blade tip.

Aircraft and Registration

The aircraft involved was a Schweizer S 269C helicopter, registration I-GUAN.

Date and Location

The incident occurred on 27 May 2002 at 07:30 UTC near Caresana (VC), Italy.

Event Description

During an agricultural flight involving the spraying of substances for anti-larval treatment of rice fields, the pilot, while in translational flight at about 6 meters above ground, perceived strong vibrations from the tail rotor. As a precaution, he decided to perform an off-field landing. After touchdown, it was found that the tip of one tail rotor blade had ruptured.

Pilot Information

The pilot was a 30-year-old male of Italian nationality, holding a valid commercial helicopter pilot license and a valid medical certificate. He had a total of 628 flight hours, of which about 616 on type. In the last 24 hours, he had flown 0 hours; in the last 7 days, 18 hours 40 minutes; in the last 30 days, 38 hours 43 minutes.

Aircraft Information

The Schweizer S 269C is a single-engine helicopter with a maximum takeoff weight of 930 kg. It has a length of 9.40 m, a height of 2.66 m, and a main rotor diameter of 8.18 m.

Meteorological Information

Visibility was greater than 10 km, no wind, and 6/8 cloud cover.

Analysis

Examination of the tail rotor blade indicated that the tip failure likely resulted from the detachment of the resin fillets securing the basal tip during operation. This material, flung outward by centrifugal force, would have caused the rupture of the tip cap. The breakage and partial detachment of paint along the entire trailing edge and partial laminate failure indicated that the blade had undergone significant deformation, predominantly elastic, due to a strong stress applied in a rear-to-front direction. This stress was probably caused by an impact. The investigation did not find evidence to determine whether the impact occurred before or after the resin fillet detachment.

Probable Cause

The cause of the detachment of the blade tip was attributed to a technical factor, likely due to a strong stress.

Frequently asked questions

What happened in the 26 Jan 2003 A320, accident near Aeroporto di Roma Fiumicino, IT?

On 27 May 2002, a Schweizer S 269C helicopter experienced strong tail rotor vibrations during an agricultural spraying flight near Caresana, Italy. The pilot performed a precautionary off-field landing; investigation found damage to a tail rotor blade tip.

Were there any fatalities in the 26 Jan 2003 A320, accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 26 Jan 2003 involved an A320,, registration D-ALTG, at Aeroporto di Roma Fiumicino, IT.

What was the probable cause of the accident?

Technical factor, likely due to a strong stress.