Casualties unknown

1998-09-26: Beech 95-B55 (N554MB) — Hawthorne, NV

Hawthorne, NV, US

On September 26, 1998, a Beech 95-B55 (registration N554MB) was involved in an aviation accident near Hawthorne, NV. Investigators recorded the probable cause as: The pilot's disregard of the weather briefing information and his decision to attempt flight into forecast adverse weather conditions, which led to an encounter with icing conditions beyond the performance capability of the aircraft. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

A pilot who received multiple warnings about IFR conditions, mountain obscuration, icing, and thunderstorms picked up an IFR clearance, then reported a systems failure and loss of control. Neither engine had mechanical issues; the airplane lacked deicing equipment.

Weather Briefing

The pilot called the flight service station and obtained a weather briefing prior to the flight. He was told several times that VFR flight was not recommended due in part to IFR conditions along a portion of his route, mountain obscurement along the entire route, and moderate rime and mixed icing along the route between 8,000 and 18,000 feet. Additionally, he was told there were thunderstorms over the Sierra Nevada Mountains, Southern California, and throughout Utah and Nevada.

Flight Events

The pilot picked up an IFR clearance moments before he told controllers that he had a "system's failure." The controller asked him what type of system's problem he had, and he told the controller that he had lost control of the aircraft and was descending at 2,000 feet per minute.

Search and Rescue

Ground units that were launched to locate the missing aircraft were hampered by inclement weather. An H-60 military helicopter that was conducting an airborne search entered clouds and crashed not far from the site of the downed aircraft.

Engine and Propeller Examination

Teardown reports on both engines concluded that there were no mechanical malfunctions noted that would have caused an operational problem. The left propeller was found feathered prior to impact, with no preimpact discrepancies noted on either propeller that would have precluded normal operation. The right propeller had indications of rotation and power development on impact.

Icing Conditions

The airplane was not equipped for flight into icing conditions and did not have any propeller or wing deicing boots. Analysis of meteorological data showed that the aircraft entered the clouds where significant light to moderate clear/mixed airframe icing was present, and encountered a convective cell in the minutes prior to the accident.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11089. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.