In the late 1970s and early 1980s, the safety of the Beechcraft V35 Bonanza became a major issue. The problem was a pattern of in-flight airframe failures. Many of these disintegrations occurred in instrument meteorological conditions and with non-instrument-rated pilots at the controls. There was considerable speculation that the V35's V-tail design was partially to blame. It was learned that under certain high G loadings, the tail structure could twist and bend to an unusually large degree. Once again, a certification review was ordered, and once again, it was determined that the airplane met the rules. Eventually, a method of strengthening the V-tail's tail spar assemblies was developed by Beech, then offered to owners free of charge.