# Accident 19980926026639A: Beech 95B55, Hawthorne, NV, September 26, 1998 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: September 26, 1998, 08:30 local time - Place: Hawthorne, NV - Damage: Destroyed - Phase of flight: Scud Running - Operating rules: General operating rules (Part 91) - Location: 38.4797° N, 118.6399° W: From the FAA, an estimate near the named town, within about 3 miles - Nearby events: https://openairdocs.org/map.md?lat=38.4797&lon=-118.6399&mi=10 - Aircraft: N554MB, a cancelled registration (https://openairdocs.org/deregistered/N554MB-2001-04-09) (OpenAirDocs) - Registry model: Beech 95-B55 (T42A) (registry code 1152706, https://openairdocs.org/model/beech-95-b55-t42a) (OpenAirDocs) - Reported make and model: BEECH 95B55 - Reported engine: CONT IO470L - People aboard: 1 - Fatal injuries: 1 - Pilot flight hours: 1,839 total, 407 in this make and model, 62 in the last 90 days - NTSB investigation: [NTSB LAX98FA306](https://openairdocs.org/ntsb/LAX98FA306) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/19980926026639A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (.19)ON SEPTEMBER 26, 1998, AT 0830 HOURS PACIFIC DAYLIGHT TIME, A BEECH 95-B55 AIRPLANE, N554MB, COLLIDED WITH MOUNTAINOUS TERRAIN FOLLOWING THE PILOT'S REPORT OF AN ENGINE LOSS APPROXIMATELY 10 MILES NORTHEAST OF HAWTHORNE, NEVADA. THE AIRCRAFT, OWNED AND OPERATED BY HIGH PERFORMANCE AIRCRAFT, INCORPORATED, WAS DESTROYED IN THE COLLISION SEQUENCE AND POSTCRASH FIRE. THE PILOT, THE SOLE OCCUPANT, SUSTAINED FATAL INJURIES. THE FLIGHT ORIGINATED AT RED BLUFF MUNICIPAL AIRPORT AT AN UNKNOWN TIME. THE PILOT CALLED THE FEDERAL AVIATION ADMINISTRATION RANCHO MURIETA FLIGHT SERVICE STATION AND OBTAINED A FULL WEATHER BRIEFING. HE TOLD THE BRIEFER THAT HE PLANNED TO FLY FROM RED BLUFF TO THE FRESNO/BAKERSFIELD AREA, THEN EASTWARD ACROSS THE SIERRA NEVADA MOUNTAINS TO ST. GEORGE, UTAH. THE BRIEFER TOLD THE PILOT THAT VISUAL FLIGHT RULES (VFR) FLIGHT WAS NOT RECOMMENDED DUE TO MOUNTAIN OBSCURATION, ICING, AND TURBULENCE ALONG HIS PROPOSED ROUTE OF FLIGHT. THE AIRCRAFT WAS ON VFR FLIGHT FOLLOWING WITH OAKLAND AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC). SHORTLY BEFORE THE ACCIDENT, THE CONTROLLER ASKED THE PILOT IF HE WANTED HIS INSTRUMENT FLIGHT RULES (IFR) CLEARANCE. THE PILOT REPLIE D "IF POSSIBLE." THE TERMINAL CONTROL FACILITY AT NAS FALLON RECORDED CONVERSATIONS WITH THE PILOT ON THE EMERGENCY GUARD FREQUENCY OF 121.5/245.0, AND THE PILOT REPORTED "121.5, BARON 554MB, I'VE GOT AN ENGINE OUT IN THE CLOUDS." (.4) 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 OBSCURMENT 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. 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. GROUND UNITS THAT WERE LAUNCHED TO LOCATE THE MISSING AIRCRAFT WERE HAMPERED BY INCLIMATE WEATHER, AND AN H-60 MILITARY HELICOPTER THAT WAS CONDUCTING AN AIRBORNE SEARCH ENTERED CLOUDS AND CRASHED NOT FAR FROM THE SITE OF THE DOWNED AIRCRAFT. 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. 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. (-23) ON SEPTEMBER 26, 1998, AT APPROXIMATELY 0830 HOURS PACIFIC DAYLIGHT TIME, THE BEECH BARON 95-B55B, AIRPLANE N554MB, COLLIDED WITH MOUNTAINOUS TERRAIN AT APPROXIMATELY 8900 FT., FOLLOWING THE PILOT'S REPORT OF AN ENGINE LOSS IN THE CLOUDS, APPROXIMATELY 10 MILES NORTHEAST OF HAWTHORNE, NV. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX98FA306](https://openairdocs.org/ntsb/LAX98FA306), Sep 26, 1998: Beech 95-B55 (N554MB), Hawthorne, NV, destroyed, 1 fatal. Probable cause: 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… From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.