Casualties unknown

Pilot Disregarded Smoke Warning, Forced Landing After Engine Failure (N5820H)

San Antonio, TX, US

On October 19, 1989, a Cessna 414 (registration N5820H) operated by Eglin Aero Club was involved in an aviation accident near San Antonio, TX. Investigators recorded the probable cause as: The thrust loss was due to failure of the right unfeathering accumulator hose from chaffing caused by misrouting during engine installation; the smoke was from exhaust system cracks due to previous weld repairs. 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 2026-06-10Data APIEditorial standards

During takeoff roll, the pilot was advised by tower that he was trailing smoke but disregarded it, believing it normal. He continued takeoff, then experienced right engine thrust loss. An attempted return was unsuccessful, and he executed a forced landing into a vacant lot. Investigation revealed the thrust loss was due to a misrouted unfeathering accumulator hose, and the smoke was from exhaust system cracks.

Accident Overview

During the takeoff roll, the pilot was advised by air traffic control that the aircraft was trailing smoke. The pilot disregarded the report, having observed smoke on previous occasions and considering it a normal condition. He continued the takeoff. Shortly thereafter, the aircraft experienced a thrust loss of the right engine. The pilot attempted to return to the airport but was unsuccessful. Evidence indicated single-engine performance degradation due to a 9.4% over-gross condition and the pilot's failure to raise the landing gear and feather the right propeller. The pilot executed a forced landing into a vacant lot.

Investigation Findings

Investigation revealed that the thrust loss was a result of the failure, due to chaffing, of the right unfeathering accumulator hose. The hose had been misrouted during engine installation. The original smoke observed by the pilot was due to cracks in the right exhaust system. These cracks originated from previous weld repairs performed during engine installation. Neither the hose misrouting nor the exhaust system cracks had been identified by the operator's maintenance personnel.

Probable cause

The thrust loss was due to failure of the right unfeathering accumulator hose from chaffing caused by misrouting during engine installation; the smoke was from exhaust system cracks due to previous weld repairs. Neither condition was identified by operator maintenance personnel.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X29598. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.