1 fatality

Pilot Killed in Accident Following Improper Aileron Control Rigging (N1435Z)

Anchorage-Lake Hood, United States of AmericaTakeoff (climb)

On May 20, 1988, a De Havilland DHC-2 Beaver (registration N1435Z) operated by Anglers Island Lodge was involved in an aviation accident near Anchorage-Lake Hood, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Occurrence #1: loss of control - in flight. Phase of operation: takeoff - initial climb. Findings: 1. (c) flt control syst, aileron control - incorrect; 2. (c) maintenance, major repair - improper - other maintenance personnel; 3. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

During takeoff from water, the airplane entered an uncontrolled left bank and struck the ground. Post-crash examination revealed reversed control cables and improper maintenance; the pilot, sole occupant, was killed.

Background

The airplane had undergone extensive maintenance that included work on the control column. The upper half of the control column was replaced with a throw-over yoke, and the aileron system was rerigged. The pilot-in-command picked up the airplane after it had been tied down outside for three months.

Accident Sequence

According to a witness, the airplane lifted off the water and started a left bank which increased until the airplane struck the ground. The pilot, the sole person on board, was killed.

Investigation Findings

Post-accident examination revealed that the control cables at the base of the control column operated in reverse of the description in the maintenance manual. Complete control continuity could not be concluded because of the extensive post-impact fire, which destroyed the overhead bellcrank, pulley, and interconnect system.

The official probable cause findings include:

  • Occurrence #1: Loss of control in flight during takeoff initial climb.
  • Findings: (1) Aileron control incorrect; (2) Improper major repair by other maintenance personnel; (3) Inadequate preflight by the pilot in command.
  • Occurrence #2: In-flight collision with terrain/water during uncontrolled descent.