Casualties unknown

Engine Failure Forces Landing on Highway; Nose Gear Damaged During Rollout (N9317M)

Page, AZ, US

On May 26, 2003, a Cessna T207A (registration N9317M) was involved in an aviation accident near Page, AZ. Investigators recorded the probable cause as: a loss of engine power due to a oil starvation induced catastrophic internal failure of the engine caused by the rotation of the number 2 cylinder main bearing. This narrative was modified on February 16, 2005. 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 pilot executed a forced landing on a highway after a catastrophic engine failure, during which the nose gear was torn off. Post-landing inspection revealed holes in the engine casing and a rotated main bearing that had cut oil supply.

Incident Overview

Approximately 20 minutes after takeoff, the airplane's engine began to shake violently. The pilot responded by reducing the throttle to 15 inches of manifold pressure and decreasing engine speed to 2300 rpm. White smoke emerged from the top of the cowling, with a small amount entering the cockpit, and a substantial quantity of "very black" oil flowed from the front of the cowling.

Forced Landing Sequence

The pilot turned the airplane toward the nearest airport. About two minutes later, the engine stopped completely. The pilot then executed a base leg for a highway below. While on final approach, the airplane was overtaking vehicles on the road, prompting the pilot to deviate to the side of the highway. During the landing roll, the nose gear was torn off.

Post-Landing Inspection

After securing the airplane, the pilot observed two large holes on the top, aft portion of the engine casing. Pieces of casing and piston were scattered on and around the engine. A piston rod was found on top of the engine, and a third hole was located at the bottom of the engine casing.

Engine Disassembly Findings

Disassembly of the engine revealed that the number 2 cylinder main bearing had rotated, closing off the oil supply to that bearing. The engine had accumulated 1,464.5 hours since its last overhaul. According to the engine manufacturer, the recommended time between overhauls for this engine is 1,600 operating hours. An oil analysis conducted on December 7, 2001, indicated that wear metals appeared high for the oil time.

Conclusion

The forced landing was necessitated by a catastrophic engine failure, with the subsequent landing roll resulting in damage to the nose gear.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030530X00744. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.