De-icing Fluid Residue Causes Aileron Control Loss in Fokker F28

Casualties unknown • Flight control problems, Fokker F28 Mk 070, Dutch airspace, NL

A KLM Cityhopper Fokker F28 experienced a loss of aileron control during descent into Amsterdam due to frozen de-icing fluid residue in the wing mechanism.

What happened

On May 16, 2005, a KLM Cityhopper Fokker F28 Mk 070, registration PH-KZR, was operating a scheduled flight from Torp, Norway, to Amsterdam. During the descent into Amsterdam Airport Schiphol, the flight crew experienced a significant loss of aileron control, specifically finding that left-hand turns were impossible. As the aircraft continued its final approach, the crew noted that partial control of the ailerons had returned. Despite the flight control issues, the aircraft landed without incident, and all 68 passengers and 4 crew members disembarked safely.

The investigation

The investigation focused on the aircraft's powered flight control system, specifically the cables and actuators located in the wheel bay. Investigators examined the aileron pulleys following reports of similar incidents within the airline. Upon inspection, a gel-like residue from de-icing fluid was discovered on the left-hand aileron pulley.

It was determined that a gap in the seal between the wing and the fuselage fairing allowed de-icing and anti-icing fluids to seep into the wheel bay. While the aircraft had not been treated with fluid on the day of the incident, it had undergone heavy de-icing/anti-ing procedures during the preceding winter months, including the use of thickened Type II fluids. The investigation established that when these thickened fluids evaporate, they leave behind chemicals that, when exposed to moisture, expand into a gel that can freeze and obstruct mechanical components.

Findings

  • A gap in the wing-to-fuselage fairing allowed de-icing/anti-icing fluid to penetrate the wheel bay.
  • Accumulated de-icing fluid residue froze on the left-hand aileron pulley, causing the mechanical blockage.
  • The residue was highly hygroscopic, meaning it absorbed moisture from the air to form a swelling gel.
  • The use of thickened fluids (Type II) contributed to the buildup of residue in aerodynamic gaps.

Safety action

Following the discovery, an Airworthiness Directive (AD NL 2005-13) was issued, requiring all Fokker F28 Mk70/100 aircraft to inspect wing-to-fuselage fairings above the main landing gear. The airline also updated its maintenance protocols, increasing the frequency of inspections and cleanings of critical areas from once per winter to once per week or per A-check.

Probable cause

The loss of aileron control was caused by the freezing of thickened de-icing fluid residue on the aileron pulley, which had seeped through a gap in the wing-to-fuselage fairing.

Frequently asked questions

What happened in the null aircraft accident near Flight control problems, Fokker F28 Mk 070, Dutch airspace, NL?

A KLM Cityhopper Fokker F28 experienced a loss of aileron control during descent into Amsterdam due to frozen de-icing fluid residue in the wing mechanism.

What aircraft was involved and where did it happen?

The accident on null involved a aircraft, at Flight control problems, Fokker F28 Mk 070, Dutch airspace, NL.

What was the probable cause of the accident?

The loss of aileron control was caused by the freezing of thickened de-icing fluid residue on the aileron pulley, which had seeped through a gap in the wing-to-fuselage fairing.

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