Casualties unknown

1992-07-12: Beech A23A (N7904L) — Evert O. Wilkerson — Chico, CA

Chico, CA, US

On July 12, 1992, a Beech A23A (registration N7904L) operated by Evert O. Wilkerson was involved in an aviation accident near Chico, CA. Investigators recorded the probable cause as: 1) THE PILOT'S INADVERTENT ENTRY INTO INSTRUMENT METEOROLOGICAL CONDITIONS, 2) HIS FAILURE TO MAINTAIN CONTROL OF THE AIRCRAFT DUE TO SPATIAL DISORIENTATION, 3) THE INADVERTENT ENTRY INTO A SPIRAL DIVE AT AN EXCESSIVE AIRSPEED, AND, 4) THE PILOT'S IMPROPER… This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot on a scenic tour of the Sierra Nevada foothills lost visual reference after entering a large cumulus cloud, resulting in a high-speed spiral dive and structural damage to the aircraft.

Incident Overview

A pilot was flying family members on a tour of the Sierra Nevada mountain range foothills when the flight encountered rapidly building cumulus clouds while cruising at an altitude of about 11,500 feet MSL. The pilot reported navigating around the buildups in an attempt to maintain visual flight rules (VFR) conditions, but the clouds eventually surrounded the aircraft.

Loss of Visual Reference

The flight inadvertently entered one of the large clouds. According to the pilot, the aircraft then entered a high-speed spiral dive, reaching an airspeed in excess of approximately 190 knots.

Recovery

The pilot stated that he, with the assistance of his son, began pulling back on the control wheel and successfully recovered control of the aircraft. Following the recovery, the flight returned to its home base and landed without further incident.

Post-Flight Examination

An examination of the aircraft by Federal Aviation Administration (FAA) inspectors revealed substantial structural damage. Both wings exhibited major buckles at the production joints between the inboard and outboard wing panels. The outboard panels showed an upward permanent set. Additionally, the fuselage immediately aft of the firewall and forward of the empennage displayed areas of skin buckling.

Conclusion

The aircraft sustained significant structural deformation as a result of the high-speed maneuver. The pilot's actions, with the help of his son, prevented a potential loss of control.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15214. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.