Casualties unknown

2024-08-01: Robinson R44 (SP-NHM) — Prywatny (Private) — Toruń Włościański, PL

Toruń Włościański, PL

On August 1, 2024, a Robinson R44 (registration SP-NHM) operated by Prywatny (Private) was involved in an aviation accident near Toruń Włościański, PL. Investigators recorded the probable cause as: Unjustified decision to perform an emergency landing (autorotation) instead of a precautionary landing (with the engine running) and improperly executed emergency landing without engine power reduction. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 16 related events involving the same aircraft type or operator are linked below.

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards

On 1 August 2024, a Robinson R44 Cadet (SP-NHM) operated by Salt Aviation executed an emergency landing near Toruń. The pilot reported fluctuating manifold pressure and reduced power. The helicopter was destroyed; the pilot sustained minor injuries. The investigation determined the pilot made an unjustified decision to perform autorotation instead of a running landing and executed the landing improperly.

Flight History

On 1 August 2024, the pilot planned a non-commercial flight from Warsaw-Modlin (EPMO) to Niedźwiedzi Róg in a Robinson R44 Cadet helicopter, registration SP-NHM. After arriving at the airport at approximately 2:00 p.m., the pilot checked weather forecasts and current meteorological conditions as well as zone occupancy. He performed a preflight inspection and moved the helicopter out of the hangar. The pilot took his seat, obtained take-off clearance, started the engine, and conducted engine tests. He took off from FATO 26 at 3:43 p.m. After take-off, he climbed to 1,500 ft AMSL and maintained course toward the YANKEE point.

During the climb, the pilot noticed a lower than normal vertical speed and observed that the charge pressure gauge pointer fluctuated within +/- 1 inHg while all other parameters were normal. Above 1,000 ft AMSL, the fluctuation increased to +/- 2.5 inHg with a noticeable decrease in power. The pilot corrected the power shortfall with the collective pitch lever, but even with it near maximum, he continued to lose altitude while maintaining forward speed.

At approximately 900 ft AMSL, the pilot decided to make an emergency landing and selected a landing site. Shortly before touchdown, he performed a flare maneuver and a run-in touchdown. The helicopter crashed into the ground. The pilot exited the helicopter by his own efforts.

Injuries and Damage

The pilot suffered minor injuries. The helicopter was destroyed.

Causes of the Occurrence

The investigation identified two causes: 1) Unjustified decision to perform an emergency landing (autorotation) instead of a precautionary landing (with the engine running). 2) Improperly executed emergency landing without engine power reduction.

Probable cause

Unjustified decision to perform an emergency landing (autorotation) instead of a precautionary landing (with the engine running) and improperly executed emergency landing without engine power reduction.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2024-0057/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.