Main Landing Gear Retraction Failure on Flight 4317

Casualties unknown • Savannah, GA, US

During takeoff, the main landing gear of Flight 4317 failed to retract, leading to an emergency checklist execution and a subsequent safe landing.

What happened

Following takeoff, the main landing gear of Flight 4317 failed to retract into the aircraft. The flight crew responded by performing the emergency checklist, which included extending the landing gear. The aircraft subsequently completed an uneventful landing.

The investigation

An examination of the aircraft revealed that the right landing gear retraction fitting had failed, resulting in a severed hydraulic line. Investigators also found that the quantity limiting valves were corroded, which restricted the movement of the respective pistons. As a result of these failures, both hydraulic systems were drained of fluid.

Further inspection of the fitting attachment bolts showed that the top bolt had lost torque and suffered a fatigue failure, while the bottom bolts failed due to overload. Additionally, the fitting spigot failed because of hydrogen embrittlement.

Following the incident, the operator conducted a fleet campaign and discovered 13 loose bolts in other 100 series aircraft. This led to the issuance of several airworthiness directives to address the loss of torque on attachment bolts, specifically requiring torque checks during the 300-hour landing gear inspection.

Probable cause

The failure of the right landing gear retraction fitting due to fatigue of a top attachment bolt and hydrogen embrittlement of the fitting spigot.

Frequently asked questions

What happened in the 1991-07-17 DE Havilland DHC-8-102 accident near Savannah, GA?

During takeoff, the main landing gear of Flight 4317 failed to retract, leading to an emergency checklist execution and a subsequent safe landing.

What aircraft was involved and where did it happen?

The accident on 1991-07-17 involved a DE Havilland DHC-8-102, registration N922HA, operated by Henson Airlines, at Savannah, GA.

What was the probable cause of the accident?

The failure of the right landing gear retraction fitting due to fatigue of a top attachment bolt and hydrogen embrittlement of the fitting spigot.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X17430. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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