Casualties unknown

2005-03-18: Cessna 305 C, (I-EIAD) — Aeroporto di L'Aquila Preturo, IT

Aeroporto di L'Aquila Preturo, IT

On March 18, 2005, a Cessna 305 C, (registration I-EIAD) was involved in an aviation accident near Aeroporto di L'Aquila Preturo, IT. Investigators recorded the probable cause as: The accident was caused by a heavy landing resulting from a misjudged descent rate, compounded by the pilot's limited experience with tailwheel-type aircraft. This summary draws on records from the Italian National Flight Safety Agency (ANSV).

Sourcesthe Italian National Flight Safety Agency (ANSV)Primary reportUpdated 1785083425Data APIEditorial standards

A training flight ended in structural damage and a lost main wheel after a pilot misjudged the descent rate during landing at L’Aquila Preturo airport.

What happened

On March 18, 2005, a Cessna 305 C, registration I-EIAD, was performing a training flight at L’Aquila Preturo airport. During the landing roll on runway 36, the aircraft experienced a significant yawing motion. This instability caused the wingtips to strike the runway surface. The impact of the landing gear against the pavement was severe enough to cause the left main wheel to detach from the aircraft. The aircraft sustained structural damage, including abrasions and deformations to the fuselage and wingtips, but the two occupants—the pilot and a passenger—remained uninjured.

The investigation

The ANSV investigation focused on the sequence of events during the landing phase and the technical state of the aircraft. Investigators reviewed the pilot's flight history, noting that while the pilot was highly experienced in large multi-engine aircraft, they had very limited experience flying this specific type of single-engine aircraft with a tailwheel configuration, having logged only 58 total hours on the Cessna 305 C. The investigation also examined the aircraft's maintenance records and the meteorological conditions at the time of the accident, which were reported as CAVOK with no wind.

Findings

  • The primary cause of the accident was the pilot's incorrect assessment of the descent rate during the final approach, which resulted in a heavy landing.
  • The loss of control and subsequent yawing motion led to the wingtip strikes and the detachment of the left main wheel.
  • A contributing factor was the pilot's lack of experience operating a single-engine aircraft with a tailwheel configuration.

Probable cause

The accident was caused by a heavy landing resulting from a misjudged descent rate, compounded by the pilot's limited experience with tailwheel-type aircraft.