Casualties unknown

Cabin Fire Prompts Ditching of Single-Engine Airplane; Post-Accident Exam Finds Improper Routing (N96AK)

Juneau, AK, US

On June 9, 1998, a Cessna 207A (registration N96AK) was involved in an aviation accident near Juneau, AK. Investigators recorded the probable cause as: The failure of company maintenance personnel to properly install a wire bundle clamp; chafing, electrical arcing, and subsequent leaking of a fuel line, which resulted in an in-flight fire. 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

A commercial pilot and four passengers ditch a single-engine airplane after smoke and heat from under the cabin floor. Post-accident examination reveals fuel line, wires, and antenna cable routed together with arcing evidence; a clamp was missing.

Accident Sequence

A certificated commercial pilot and four passengers departed in a single-engine airplane on a scheduled commuter flight over terrain consisting of open water and wooded islands. Thirteen minutes later, during a climb, the pilot noted smoke and heat coming from beneath the mid-cabin floor. The pilot declared an emergency, reporting a fire in the airplane, and ditched the airplane in shallow water along a shoreline of a small island. The fire, which was located under the right front seat between the cabin floor and the lower airplane belly skin, self-extinguished during the ditching.

Post-Accident Examination

Post-accident examination disclosed that a fuel line, a bundled set of electrical wires, and a Loran antenna cable had all been routed adjacent to each other under the cabin floor, contrary to FAA recommended methodology. The Loran antenna cable had been installed 10 years prior to the accident. Two small holes, consistent with arcing, were found in the fuel line. Evidence of arcing was found on one of the electrical wires. Plastic tie wraps attached the wire/antenna bundle to plastic clamps that were each secured to fuselage formers under the floor by bolts or screws. One clamp, adjacent to the holes found in the fuel line, was missing from its attach point. A screw and a small melted portion of a plastic tie wrap were found adjacent to each other in the fuselage belly, beneath the cabin floor. The FAA recommended technique for attaching clamps to structure is the use of bolts with locknuts, or self-locking nuts.

Inspection History

An annual inspection was accomplished six months before the accident. A 100-hour inspection was completed 11 days before the accident. Each company inspection checklist includes an inspection of the internal structure of the fuselage, and an inspection of antenna cables.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X10200. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.