Casualties unknown

2021-08-19: Diamond DA 42 (SP-TRL) — Goldwings Flight Academy — Modlin (EPMO), PL

Modlin (EPMO), PL

On August 19, 2021, a Diamond DA 42 (registration SP-TRL) operated by Goldwings Flight Academy was involved in an aviation accident near Modlin (EPMO), PL. Investigators recorded the probable cause as: The accident was caused by (1) both engines failure simulated just after take-off in the climb phase, which was inconsistent with Exercise No. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 9 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 19 August 2021, a Diamond DA 42 (SP-TRL) operated by Goldwings Flight Academy sustained substantial damage during a training flight at Warszawa-Modlin aerodrome (EPMO) after the instructor simulated a dual engine failure at low altitude.

Factual Information

On 19 August 2021, at 14:22 UTC, a Diamond DA 42 aircraft (registration SP-TRL) took off from Warszawa-Babice aerodrome (EPBC) for a visual flight rules training flight as part of multi-engine piston (MEP) training. The crew consisted of an instructor-pilot and a student-pilot. The flight proceeded to Warszawa-Modlin aerodrome (EPMO) to perform exercise No. 6—powerplant failure simulation during aerodrome circuit flights.

Nine take-offs and landings were completed uneventfully. After the ninth landing, the crew stopped the aircraft on the runway and, after a short break, initiated another take-off. During the climb, at an altitude of approximately 500 feet, the instructor-pilot reduced the power of both engines to idle, simulating a powerplant failure. To maintain airspeed, the crew began a descent intending a straight-in landing. The descent was performed with a significant nose-down pitch, resulting in a high-speed touchdown at approximately 16:05 UTC.

Damage to Aircraft

The aircraft was substantially damaged. The landing gear was destroyed: the main landing gear struts broke, and the wheels detached. The nose landing gear strut and its wheel were pressed into the nose landing gear well. As the main landing gear collapsed, the aircraft rested on the lower fuselage, causing the rotating propellers to strike the runway surface. Both three-blade propellers, which had wooden blades, were destroyed. The lower fuselage was also damaged. The wings did not detach but sustained cracks and delamination, especially at the root areas. The horizontal stabilizer leading edge was damaged.

Injuries to Persons

Both crew members—the instructor and the student—were uninjured. No other persons were onboard.

Cause and Contributing Factors

The investigation determined that the accident was caused by: 1) Simulating a dual engine failure just after take-off during the climb, which was inconsistent with Exercise No. 6 of the training program. 2) Insufficient flight altitude at the initiation of the powerplant failure simulation.

A contributing factor was the incorrect estimation of the flight altitude prior to simulating the powerplant failure.

No safety recommendations were proposed by the State Commission on Aircraft Accidents Investigation (PKBWL).

Probable cause

The accident was caused by (1) both engines failure simulated just after take-off in the climb phase, which was inconsistent with Exercise No. 6 of the training program; and (2) insufficient flight altitude during initiation of the powerplant failure simulation during climb phase.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2021-3056/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.