1 fatality

1980-04-03: Canadair CL-600 Challenger (C-GCGR-X) — Bombardier Aerospace — California City, United States of America

California City, United States of AmericaFlight

On April 3, 1980, a Canadair CL-600 Challenger (registration C-GCGR-X) operated by Bombardier Aerospace was involved in an aviation accident near California City, United States of America in flight. One person was killed. Investigators recorded the probable cause as: Uncontrolled collision with ground following an emergency descent due to technical problems with instruments/equipment. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781224085Data APIEditorial standards

During a test flight, a Bombardier prototype stalled at 34° angle of attack, entered a dive, and crashed after all three crew members bailed out. Two were injured, and one died due to parachute failure.

Accident Sequence

The accident occurred during a morning departure from Mojave-Kern County Airport. The crew was executing a series of tests on the new Bombardier prototype. While at cruising altitude, an unscheduled stall was performed, and the aircraft reached an angle of attack of 34°. Control was lost, and the airplane entered a dive. All three crew members evacuated the aircraft via parachute. The airplane subsequently crashed in a desert area. Two crew members sustained injuries, while the third occupant died because his parachute failed to deploy properly.

Investigation

Official investigation into the accident identified the probable cause and contributing factors. The findings highlighted technical problems with instruments and equipment leading to an emergency descent and subsequent uncontrolled collision with the ground.

Probable Cause

The probable cause was determined to be an uncontrolled collision with the ground following an emergency descent due to technical problems with instruments and equipment. Contributing factors included:

  • Angle of attack indicator issues (binding)
  • Deteriorated seals in the hydraulic system
  • Unknown failure in the emergency chute jettison system