Casualties unknown

1987-12-21: Beech 99 (N6724D) — Air New Orleans — Tampa, FL

Tampa, FL, US

On December 21, 1987, a Beech 99 (registration N6724D) operated by Air New Orleans was involved in an aviation accident near Tampa, FL. Investigators recorded the probable cause as: A fatigue failure of the right main landing gear actuator end cap, which resulted in the loss of all hydraulic pressure and the subsequent inability to extend the nose landing gear. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A commuter airliner landed on its belly after losing all hydraulic pressure due to a fatigue-failed landing gear actuator, despite attempts to extend the nose gear.

What happened

During the final approach phase of flight, the crew of a commuter air carrier aircraft received an unsafe indication regarding the status of the nose landing gear. Recognizing the discrepancy, the flight crew immediately abandoned the landing attempt and initiated a go-around procedure. All available emergency extension procedures were executed in an effort to lower the nose gear, but these efforts proved unsuccessful.

With the nose gear unable to extend, the crew secured both engines while still on final approach. The aircraft subsequently touched down on the runway with the nose gear retracted, resulting in a nose-gear-up landing event. No further details regarding passenger or crew injury are provided in the source text.

The investigation

Post-accident examination of the aircraft revealed that all hydraulic pressure had been lost prior to the landing. Technical analysis identified the root cause of this pressure loss as a failure of the end cap on the right main landing gear actuator. The component failed due to fatigue, which compromised the hydraulic system's integrity and prevented proper operation of the landing gear mechanisms.

Findings

The primary contributing factor was the structural failure of the right main landing gear actuator end cap caused by fatigue. This mechanical failure led to a total loss of hydraulic pressure, which in turn prevented the nose landing gear from extending despite the crew's use of emergency procedures.

Probable cause

A fatigue failure of the right main landing gear actuator end cap, which resulted in the loss of all hydraulic pressure and the subsequent inability to extend the nose landing gear.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X32731. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.