1 fatality

1986-10-28: Grumman G-73 Mallard (N604SS) — Virgin Island Seaplane Shuttle — Christiansted, US Virgin Islands

Christiansted, US Virgin IslandsTakeoff (climb)

On October 28, 1986, a Grumman G-73 Mallard (registration N604SS) operated by Virgin Island Seaplane Shuttle was involved in an aviation accident near Christiansted, US Virgin Islands during takeoff. One person was killed. Investigators recorded the probable cause as: Occurrence #1: airframe/component/system failure/malfunction during climb. Findings: (c) electrical system wiring incorrect; (c) maintenance improper by company maintenance personnel; (c) electrical wiring chafed; (c) electrical wiring arcing; (c) aileron… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781216987Data APIEditorial standards

Shortly after takeoff, pilots lost aileron control during a left turn. The aircraft crash-landed in the Caribbean Sea, killing one passenger and rescuing 14 others. Post-crash inspection found aileron cable chafed and separated due to improper maintenance.

Incident Summary

Shortly after takeoff, while executing a left turn, the flight crew lost aileron control. The aircraft exhibited uncorrectable left turning tendencies and subsequently crash-landed in the Caribbean Sea. One passenger was killed, and the other 14 occupants were rescued.

Investigation Findings

Post-crash inspection revealed that the left aileron control cable had become trapped within a bundle of electrical wires and cables. This entrapment occurred when an electrical cable connecting a reverse current relay in the right wing to the main junction box in the left cabin area at the center wing was changed and secured. The aileron cable chafed through the protective cover of the large electrical cable. Upon contact with the metal electrical cable, the aileron cable experienced arcing at several points and separated completely at two locations, resulting in a total loss of aileron control.

Probable Cause

The official probable cause is documented as a sequence of occurrences:

  • Occurrence #1 (Airframe/component/system failure/malfunction during climb): Findings include: electrical system wiring incorrect; maintenance improper by company maintenance personnel; electrical wiring chafed; electrical wiring arcing; aileron control separation; aileron control total loss.
  • Occurrence #2 (Loss of control in flight during climb): Finding: aircraft handling not possible by pilot.
  • Occurrence #3 (Forced landing during descent): No specific findings beyond forced landing.
  • Occurrence #4 (In-flight collision with terrain/water during landing flare/touchdown): Finding: terrain condition water rough.