Casualties unknown

2003-06-29: Cessna 210D (N3826Y) — Carefree, AZ

Carefree, AZ, US

On June 29, 2003, a Cessna 210D (registration N3826Y) was involved in an aviation accident near Carefree, AZ. Investigators recorded the probable cause as: A fuel leak from a cracked elbow fitting on the gascolator, which the inspector attributed to overtightening. 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 1781061362Data APIEditorial standards

An airplane experienced engine failure due to a fuel leak from a cracked gascolator fitting, leading to a forced landing on a road and inversion. Post-accident inspection revealed the crack was likely from overtightening.

Engine Failure and Forced Landing

The airplane lost engine power during flight, prompting a forced landing. The pilot had fueled the airplane with approximately five hours of fuel. After about four hours of flight, she contacted the tower to announce her intention to land. Shortly thereafter, the engine failed. She switched fuel tanks, which temporarily restored power, but the engine quit again. She concluded there must have been a fuel leak and radioed the tower to report the engine failure. While attempting to land at a private airport, the airplane instead touched down on a road and came to rest inverted. The forced landing involved rough terrain, causing the airplane to nosed over.

Post-Accident Inspection

No fuel was discovered at the accident scene, indicating a complete loss of fuel. A post-accident inspection identified a crack on the bottom of the elbow fitting attached to the gascolator. The gascolator is a fuel filter component in the fuel system. A Federal Aviation Administration inspector conducted a leak test using a soap-and-water solution applied under pressure. When the assembly was pressurized to between 3 and 5 pounds per square inch, bubbles formed at the crack, confirming a leak. The inspector also observed blue stains along the bottom of the airplane, consistent with fuel leakage. In the inspector's opinion, the crack was the result of excessive torque applied when tightening the fitting during previous maintenance or installation.

Conclusion

The fuel leak from the cracked fitting led to fuel exhaustion, which caused the engine to fail during flight. The pilot's attempt to reach a private airport was unsuccessful, and the airplane landed on a road, subsequently nosing over due to rough terrain. No fuel was found at the scene, supporting the finding that the fuel system leaked completely.

Probable cause

A fuel leak from a cracked elbow fitting on the gascolator, which the inspector attributed to overtightening.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030708X01043. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.