Hydraulic Leak Causes Emergency Landing of Cessna 210 in Brazil

Casualties unknown • CARAVELAS, BA, BR

A Cessna 210 experienced a landing gear failure due to a disconnected hydraulic line, leading to an emergency landing and substantial aircraft damage in Caravelas, Brazil.

What happened

On February 8, 2017, a Cessna 210R, registration PR-ORL, departed from the Destilaria Medasa airfield in Caravelas, Bahia, bound for Vitória, Espírito Santo. The flight was a private ferry mission operated by Quanti Participações Ltda. Shortly after takeoff, the pilot noticed that the main landing gear failed to lock in the up position.

Despite multiple attempts to manually extend the gear, the pilot was unable to secure the landing gear in the down position. After approximately two hours and twenty minutes of flight, the pilot decided to perform an emergency landing back at the point of origin. During the landing roll, the aircraft drifted to the right, veering off the runway and striking a perimeter fence with the right wing, resulting in substantial damage to the aircraft.

The investigation

CENIPA investigators examined the aircraft's hydraulic system, which utilizes a single reservoir to power both normal and emergency gear extension. The investigation established that the pilot observed a red "gear unlocked" light and noted that the hydraulic pump temperature had increased, causing the hydraulic pump breaker to trip. The hydraulic reservoir was found to be empty.

Upon inspection of the hydraulic lines, investigators discovered that an aluminum flanged tube (P/N 1280523-1) had disconnected from the left actuator cylinder. The flange had slipped inside the sleeve and nut, allowing the entire hydraulic fluid volume to leak out. Further analysis of the tube revealed that its total length was insufficient to allow both flanges to reach their connections properly. This improper installation, likely occurring during a previous maintenance intervention, subjected the tube to tensile stress. Under operational vibrations and pressure, the non-compliant flange—which featured incorrect thickness and angles—deformed, leading to the eventual disconnection.

Findings

  • Maintenance error involving the improper installation of a hydraulic flanged tube.
  • The hydraulic fluid reservoir was depleted due to a leak caused by a disconnected aluminum tube.
  • The tube (P/N 1280523-1) was of an incorrect length, preventing proper coupling at the connections.
  • The flange on the affected tube did not meet specifications regarding thickness, size, or angle.
  • Standard maintenance inspections (50, 100, and 200-hour intervals) were unable to detect the defect because they did not require the disassembly of the affected component.

Probable cause

The accident was caused by a hydraulic system failure resulting from the improper installation of a hydraulic line during maintenance, which led to a complete loss of hydraulic fluid and the subsequent inability to extend the main landing gear.

Frequently asked questions

What happened in the 2017-02-08 aircraft accident near CARAVELAS, BA, BR?

A Cessna 210 experienced a landing gear failure due to a disconnected hydraulic line, leading to an emergency landing and substantial aircraft damage in Caravelas, Brazil.

What aircraft was involved and where did it happen?

The accident on 2017-02-08 involved a aircraft, registration PRORL, at CARAVELAS, BA, BR.

What was the probable cause of the accident?

The accident was caused by a hydraulic system failure resulting from the improper installation of a hydraulic line during maintenance, which led to a complete loss of hydraulic fluid and the subsequent inability to extend the main landing gear.

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