Casualties unknown

2020-10-14: Guimbal Cabri G-2 (SP-NGU) — Pilot instruktor CPL(H) — Dęblin (EPDE), PL

Dęblin (EPDE), PL

On October 14, 2020, a Guimbal Cabri G-2 (registration SP-NGU) operated by Pilot instruktor CPL(H) was involved in an aviation accident near Dęblin (EPDE), PL. Investigators recorded the probable cause as: Corroded safety pins securing the door from sliding out of the hinges. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 2 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 14 October 2020, a Guimbal-Cabri-G2 helicopter (SP-NGU) lost its left door during a training flight at Dęblin EPDE due to corroded safety pins. The crew landed safely without injuries, but the aircraft sustained damage.

Incident Overview

On 14 October 2020, at 13:17 local time, a training flight was planned at the Academic Centre of Aviation Training in Dęblin, Poland, involving a Guimbal-Cabri-G2 helicopter (registration SP-NGU). The exercise was to simulate an autorotation. The instructor in the left seat had opened the left door for easier access to the throttle and collective controls. After entering the autorotation, the initially ajar door remained held by the gas spring. Due to vibrations at an altitude of 500 feet AGL, the door separated from the fuselage.

Post-Separation Actions

The pilot-in-command recovered engine power, synchronized it with the main rotor, and continued the approach to the grass strip at EPDE Dęblin. The landing was uneventful, and the crew sustained no injuries. The flight was conducted under day VFR.

Damage Assessment

After shutdown, the crew inspected the helicopter and found:

  • Damage to the left fuselage near the fuel filler
  • Impact marks on the left skid cross tube
  • Impact marks on the left horizontal stabilizer
  • Destroyed position light
  • The left door was found 922 meters from the grass strip threshold and 1,130 meters from the touchdown point.

Cause and Contributing Factors

The investigation determined the cause of the door detachment: corroded safety pins that were intended to secure the door from sliding out of the hinges. The helicopter's Flight Manual (sections 9, 10, 11) permits opening the door during flight, which was a contributing factor to the incident.

Preventive Measures

The operator took the following actions:

  • Conducted a detailed briefing of the incident with instructors, civil and military students, and technical personnel, emphasizing crew focus and procedures for a door loss during flight.
  • Contacted Helicopters Guimbal (the manufacturer) to develop a repair bulletin for a complete repair.
  • The manufacturer issued Service Bulletin SB 14-005A, requiring replacement of hinges with a version without additional safety pins, and repair of the left door and other damage.
  • The helicopter was grounded until a scheduled major overhaul (planned for Q2 2021), which would incorporate the service bulletin.

The Polish State Commission on Aircraft Accident Investigation accepted these preventive actions and issued no additional safety recommendations.

Probable cause

Corroded safety pins securing the door from sliding out of the hinges.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2020-3294/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.