1 fatality

1987-10-23: Piper PA-60 Aerostar (Ted Smith 600) (N554AC) — Air Continental — Kalamazoo-Battle Creek, United States of America

Kalamazoo-Battle Creek, United States of AmericaLanding (descent or approach)

On October 23, 1987, a Piper PA-60 Aerostar (Ted Smith 600) (registration N554AC) operated by Air Continental was involved in an aviation accident near Kalamazoo-Battle Creek, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: Loss of engine power due to mechanical failure/malfunction during cruise; improper maintenance (major repair) by other maintenance personnel; fatigue of the engine assembly; separation of the cylinder; separation of the cowling. 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 1781215856Data APIEditorial standards
Aircraft registered N554AC
Aircraft registered N554AC. Photo: Bill Ingalls / Public domain, via Wikimedia Commons

Aircraft N554AC experienced right engine failure during cruise at 9,000 feet. The pilot reported cowling separation and attempted to reach Kalamazoo Airport but impacted trees near I-5 miles away. The pilot, sole occupant, was killed.

Incident Overview

At an altitude of 9,000 feet and approximately 20 minutes into the flight, the pilot of N554AC reported a loss of right engine power. Chicago Air Route Traffic Control Center (ARTCC) advised that the nearest airport was Kalamazoo, located 28 miles west. The aircraft began to descend. At 0330:53, Chicago ARTCC reported that N554AC was approximately 6 miles from Kalamazoo Airport. The pilot stated, "my right engine cowling is gone...I don't know if I'm going to make it."

Witness Observations and Crash Site

Witnesses observed the aircraft flying at "tree top level" before it impacted in a heavily wooded area near Interstate 94, approximately 5 miles from the airport. The pilot, the sole occupant, was killed.

Investigation Findings

Examination revealed that the right engine case had been improperly repaired with welds. The number 2 cylinder separated from the case due to fatigue cracking in the through bolts and studs. The force of the cylinder separation caused the top section of the engine cowling to detach.

Official Probable Cause

The official probable cause includes:

  • Loss of engine power due to mechanical failure/malfunction during cruise.
  • Improper maintenance (major repair) by other maintenance personnel.
  • Fatigue of the engine assembly.
  • Separation of the cylinder.
  • Separation of the cowling.
  • Forced landing due to unsuitable terrain and bright night light conditions.
  • In-flight collision with trees.