No fatalities

Forced Landing of Cessna 172E Following Engine Power Loss on Final Approach (N5383T)

Troutdale, OR, US

On June 20, 2002, a Cessna 172E (registration N5383T) operated by Carric A. Scott was involved in an aviation accident near Troutdale, OR. No fatalities were reported. Investigators recorded the probable cause as: A loss of engine power for an undetermined (non-mechanical) reason. Contributing factors were high grass and soft terrain which lead to the collapse of the nose gear during the landing roll. 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 2026-07-04Data APIEditorial standards

During a maintenance check flight, a Cessna 172E experienced engine power loss on final approach after encountering turbulence. The pilot executed a 180-degree turn and landed off-airport, collapsing the nose gear. Post-crash examination found no mechanical malfunction but noted a non-functioning right fuel tank vent.

Flight Details

The pilot completed an uneventful one-hour flight in a Cessna 172E equipped with a Continental O-300-D engine. After topping off the fuel tanks, the pilot departed on a second one-hour flight. Both flights were maintenance checks following the replacement of all six cylinder piston rings and the re-honing of all six cylinders.

Accident Sequence

While on final approach to Runway 25, the pilot encountered "very rough turbulence" as he reduced power. The engine then lost power. Believing he could not reach the runway, the pilot executed a 180-degree course reversal and performed an off-airport landing in soft terrain covered by high grass. During the landing roll, the aircraft's nose gear collapsed.

Post-Crash Examination

On-site examination revealed fuel present in the aircraft's fuel system immediately after the forced landing. Subsequent post-crash examination found no evidence of mechanical malfunction in the engine, ignition, air delivery, or fuel system. The only discrepancy noted was the non-functionality of the right wing gas cap vent, which was required under FAA Airworthiness Directive 79-10-14R. Examination showed that the rubber gasket would not unseat and allowed normal venting. The left fuel tank vent was examined and found to function satisfactorily. The engine was test run with a new carburetor and then with the reassembled original carburetor; both tests yielded satisfactory results. The fuel system was examined, and no blockages were found in any lines, nor were any particulates found in the fuel filters.

Frequently asked questions

What happened in the 20 Jun 2002 Cessna 172E accident near Troutdale, OR?

During a maintenance check flight, a Cessna 172E experienced engine power loss on final approach after encountering turbulence. The pilot executed a 180-degree turn and landed off-airport, collapsing the nose gear. Post-crash examination found no mechanical malfunction but noted a non-functioning right fuel tank vent.

Were there any fatalities in the 20 Jun 2002 Cessna 172E accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 20 Jun 2002 involved a Cessna 172E, registration N5383T, operated by Carric A. Scott, at Troutdale, OR.

What was the probable cause of the accident?

A loss of engine power for an undetermined (non-mechanical) reason. Contributing factors were high grass and soft terrain which lead to the collapse of the nose gear during the landing roll.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020627X00990. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.