Corrosion-Induced Spring Failure Leads to Emergency Landing of ATR72

Casualties unknown • near Nelson latitude: 41° 17.9´ south longitude: 175° 13.3´ east, NZ

A landing gear malfunction caused by corroded locking springs forced an ATR72 to divert to Palmerston North, resulting in a single tyre burst upon landing.

What happened

On 9 April 2017, an ATR72-212A, registration ZK-MCY, was performing a scheduled flight from Auckland to Nelson with 71 people on board. During the approach to Nelson, the flight crew activated the landing gear lever, only to receive an alert indicating that the right-hand main landing gear had failed to lock in the down position.

Following a go-around, the crew attempted to resolve the issue by performing various checklists and even recycling the gear by retracting and re-extending it. The crew also performed steep turns to use centrifugal force to attempt to lock the gear. Despite these efforts, the unsafe indication persisted. The crew decided to divert to Palmerston North Aerodrome, a location with a longer runway and favorable weather.

Upon arrival at Palmerston North, the aircraft landed, with the captain intentionally touching down on the left main gear first before lowering the nose and right gear. During the landing roll, the right outer main tyre deflated and eventually burst after skidding. There were no injuries to the 66 passengers or five crew members.

The investigation

Investigators examined the aircraft's landing gear assembly and the fractured components. The investigation focused on the two locking springs responsible for holding the right-hand main landing gear in the down and locked position.

Metallurgical analysis of the springs revealed that the failure originated from intergranular corrosion and stress corrosion cracking. Chemical analysis (EDAX) identified the presence of chlorine and sodium at the crack initiation sites, suggesting that the saline environment of the aircraft's operating area played a role. The cracks progressed through fatigue and corrosion fatigue until the remaining metal could no longer support the load, leading to an overload failure.

Findings

  • The primary cause of the landing gear failure was the failure of the two landing gear locking springs due to corrosion-induced cracking.
  • The corrosion was likely initiated by salt exposure from the aircraft's saline operating environment.
  • The crew's decision to divert to Palmerston North was appropriate and well-managed, though the decision to recycle the landing gear was outside of documented procedures and had the potential to worsen the mechanical condition.
  • The existing maintenance inspection programme was unlikely to have detected the corrosion cracking before the failure occurred, as there was no specific requirement for preventive maintenance of these springs.

Safety action

  • The investigation highlighted the importance of pre-flight visual inspections for critical components like landing gear.
  • It was noted that while recycling the gear did not cause further damage in this instance, such actions can exacerbate mechanical failures and should be avoided unless permitted by the flight crew operating manual.

Probable cause

The failure of the right-hand main landing gear was caused by the breakage of two locking springs due to stress corrosion cracking and subsequent corrosion fatigue, likely initiated by salt exposure from the aircraft's operating environment.

Frequently asked questions

What happened in the 2017-04-09 ATR72-212A, 703 accident near near Nelson latitude: 41° 17.9´ south longitude: 175° 13.3´ east, NZ?

A landing gear malfunction caused by corroded locking springs forced an ATR72 to divert to Palmerston North, resulting in a single tyre burst upon landing.

What aircraft was involved and where did it happen?

The accident on 2017-04-09 involved a ATR72-212A, 703, registration ZK-MCY, operated by Mount Cook Airline, at near Nelson latitude: 41° 17.9´ south longitude: 175° 13.3´ east, NZ.

What was the probable cause of the accident?

The failure of the right-hand main landing gear was caused by the breakage of two locking springs due to stress corrosion cracking and subsequent corrosion fatigue, likely initiated by salt exposure from the aircraft's operating environment.

Investigation report by the New Zealand Transport Accident Investigation Commission (TAIC). Original record: https://taic.org.nz/inquiry/ao-2017-003. This page is a structured re-presentation; facts and quotes are in the Transport Accident Investigation Commission (TAIC), New Zealand.

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