Casualties unknown

Engine Failure and Ballistic Parachute Deployment in a Cirrus SR22 (F-HAPH)

FR

On January 6, 2014, a Cirrus SR22 (registration F-HAPH) was involved in an aviation accident near FR. Investigators recorded the probable cause as: The engine failure was caused by the rupture of the connecting rod head for cylinder number 2 at its attachment to the crankshaft. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Cirrus SR22 suffered an engine failure during a night flight in 2014. The pilot deployed the ballistic parachute, landing safely in a field near Le Pin, France.

Incident Overview and Flight Details On January 6, 2014, at approximately 07:45 local time, a private Cirrus SR22 with registration F-HAPH experienced a severe engine failure during a night flight. The aircraft was operating under an Instrument Flight Rules (IFR) flight plan, traveling from La Roche-sur-Yon-Les Ajoncs (85) to Grenoble-Saint-Geoir (38). The pilot and one passenger were on board. The incident occurred approximately 20 minutes after takeoff while the aircraft was climbing toward Flight Level 100. The pilot reported hearing abnormal noises and observing a red low oil pressure warning light before the engine stopped completely. Following the failure, the pilot issued a distress call on the Nantes Approach frequency and began a descent in Instrument Meteorological Conditions (IMC) toward Mauléon (79), located about 15 nautical miles to the north. After exiting the cloud layer between 2,000 and 3,000 feet, the pilot determined that a gliding landing at the airfield was not possible and activated the aircraft's ballistic recovery system, resulting in a landing in a field near Le Pin (79).

Probable cause

The engine failure was caused by the rupture of the connecting rod head for cylinder number 2 at its attachment to the crankshaft. The specific cause of the rupture could not be established as the manufacturer's examination results were not communicated to the investigation authority.