Casualties unknown

Instrument Flight Ends in Crash into Straits of Florida (N1905S)

Key West, FL, US

On November 5, 2004, a Socata TB 20 (registration N1905S) operated by Marc Paquin was involved in an aviation accident near Key West, FL. Investigators recorded the probable cause as: The pilot's failure to maintain aircraft control as a result of spatial disorientation. A related factor was the dark, night conditions. 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

An instrument-rated pilot flying an IFR departure from Runway 9 crashed into the Straits of Florida after being cleared to turn. Wreckage showed no preimpact failure, but postcrash instruments indicated steep nose-down and right bank.

Flight History

The airplane departed with an IFR clearance from Runway 9. After takeoff, it turned to a heading of 180 degrees and climbed to 1,900 feet. Approximately 25 seconds before the last radar target was recorded, the flight was cleared to turn right to a heading of 360 degrees. Recorded radar targets occurred every 12 seconds; there was no report of a failure or malfunction of the radar site at or after the last recorded radar target. No distress call was made by the pilot.

Wreckage and Impact

The airplane crashed into the Straits of Florida. The wreckage was located approximately 0.55 nautical mile and 278 degrees from the last recorded radar target. The fuselage and both wings were fragmented. No evidence of preimpact failure or malfunction was noted to the airframe, engine, or flight instruments. Additionally, no heat or fire damage was noted to any recovered piece of the wreckage.

Examination of Instruments

The airplane was equipped with a standby electrically controlled vacuum pump and a standby electrically operated attitude indicator installed on the co-pilot's side of the instrument panel. The pilot's and co-pilot's attitude indicators, each powered by separate sources, both depicted postaccident the airplane in a steep nose-down attitude and right bank angle of approximately 60 degrees. The turn coordinator also indicated a bank angle greater than standard rate. The tachometer and airspeed indications both exceeded maximum limitations.

Pilot Information

The instrument-rated pilot had accumulated a total flight time of 829 hours, 16 hours of which were accumulated on the accident airplane from April to November of 2004. The pilot's most recent logbook could not be located, and no information was obtained regarding the pilot's currency on flying by instruments.

Aircraft Information

According to the aircraft logbook, a new engine-driven vacuum pump was installed in July 2003. Altimeter, automatic pressure altitude reporting system, and static pressure system inspections, as well as transponder inspections and tests due every 24 calendar months, were last recorded as occurring in October 2002. The airplane was scheduled for an annual inspection 4 days after the accident. Dark night conditions existed in the area where the airplane was lost from radar.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041110X01801. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.