# NTSB LAX98FA306: Beech 95-B55, N554MB, Hawthorne, NV, September 26, 1998

- Type: NTSB accident investigation
- Classification: Accident · Fatal · Field investigation · Final report
- Date: September 26, 1998, 08:30 local (15:30 UTC)
- Place: Hawthorne, NV
- Coordinates: 38.479682, -118.639892 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=38.4797&lon=-118.6399&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: Fatal
- Injuries: 1 fatal
- Status: Completed, report April 20, 2000
- Report: Approved by Office Director
- NTSB case key (mKey): 44074
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX98FA306
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/44074/pdf
- Page: https://openairdocs.org/ntsb/LAX98FA306

## 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 performance capability of the aircraft. The pilot's disregard for the pilot operating handbook prohibition against flight into icing conditions is also causal.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- In flight encounter with weather, cruise
  - terrain condition - high terrain
  - weather condition - obscuration
  - weather condition - icing conditions
  - weather condition - turbulence in clouds
  - weather forecast - disregarded, pilot in command (cause)
  - flight into adverse weather - attempted, pilot in command (cause)
- Loss of control - in flight, cruise
  - weather condition - icing conditions
  - flight manuals - disregarded, pilot in command (cause)
  - aircraft performance,climb capability - exceeded
  - airspeed - not maintained, pilot in command (cause)
  - stall/mush - encountered, pilot in command
- In flight collision with terrain/water, descent

## Analysis

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.

## Factual narrative

HISTORY OF FLIGHT

On September 26, 1998, at 0830 hours Pacific daylight time, a Beech 95-B55 airplane, N554MB, collided with mountainous terrain following the loss of engine power approximately 10 miles northwest of Hawthorne, Nevada.  The aircraft, owned and operated by High Performance Aircraft, Incorporated, was destroyed in the collision sequence and post crash fire.  The pilot, the sole occupant, sustained fatal injuries.  The personal flight originated at Red Bluff Municipal Airport, Red Bluff, California, at an unknown time.

According to family members, the pilot told his wife that he was going to leave Red Bluff approximately 0530-0600 to depart for St. George, Utah.  He was going to St. George to run in a marathon race.

According to records from the Rancho Murietta AFSS, the pilot called the flight service station at 0635 and obtained a full weather briefing.  He told the briefer that he planned to fly visual flight rules (VFR) from Red Bluff to Sacramento to Reno at 11,500 feet, with a planned departure time of 0730.  The briefer told the pilot that VFR flight was not recommended.  The pilot asked about flying from Red Bluff south to the Fresno/Bakersfield area, then eastward across the Sierra Nevada Mountains to St. George, Utah.  The briefer told the pilot that VFR was not recommended due to mountain obscuration, icing, and turbulence along his proposed route of flight.

The pilot took off from the airport at an unknown time, activated his VFR fight plan, and began to talk with air traffic control (ATC).

The aircraft was on VFR flight following with Oakland Air Route Traffic Control Center (ARTCC).  At 0824:44, the pilot told the controller that he was "going to climb up to fifteen five (15,500 feet), or climb to fifteen to catch a hard IFR."  The controller asked him, "November four mike bravo roger and do you want your IFR at this time?"  At 0824:55, the pilot replied "if it's possible we'll take it now."  The controller verified that the pilot's destination was St. George, and then at 1825:24, cleared the pilot to St. George Airport via "direct Tonopah direct climb and maintain flight level, correction climb and maintain one five thousand (15,000)."

At 0827:52, the pilot called the controller and said that he had a system failure.  The controller asked him what type of system failure he had, and the pilot replied that he had lost control of the airplane.  At 0828:15, the pilot informed the controller that he was "losing altitude two thousand feet a minute."

The following section is a verbatim transcript of recorded conversations with the pilot and ATC.  The recorded conversation contains references to direction, which are incorrect given that the airplane was traveling in an easterly direction.  The pilot asked the controller if he could get a heading for the closest airport.  The controller told him that the closest airport was behind him on a heading of zero seven zero (070 degrees).  The controller issued a terrain alert for the pilot at 11,000 feet at 0829:18.  He asked the pilot if he could hold that altitude.  The pilot replied that he was holding nine five (9,500 feet).  The controller asked him if he had the terrain and ground in sight and the pilot replied "I do not."

The terminal control facility at NAS Fallon recorded conversations with the pilot on the emergency guard frequency of 121.5/243.0.  At 0831:09, the pilot reported, "121.5, Baron 554MB, I've got an engine out in the clouds."  He then reported that he was holding 9,500 feet.  At 0832:10, he said "mayday mayday."

The pilot replied to a query by a passing Northwest Airlines airplane, that attempted to contact him at the controller's request, by stating, "I'm descending through 9,500 . . . can't hold altitude, terrain is around me . . . I could sure use a radar vector somewhere . . ."

The controller asked the Northwest airplane the Baron's location.  The Northwest Airlines pilot advised the controller that it sounded like N554MB had said that he was descending out of 9,500 feet over Tonopah on a heading of 090 degrees, direct west.

NAS Fallon FACTS radar data was reviewed.  At 0823:43, the accident airplane flight path showed the airplane at 13,700 feet on a ground track of 101 degrees with an estimated ground speed of 190 knots.  Approximately 3 minutes later at 0826:34, the flight path indicated it was at 14,600 feet with a ground track of 079 degrees, and an estimated ground speed of 130 knots.  At 0827:47, the radar data indicated it was at 13,700 feet with a ground track of 237 degrees, and an estimated ground speed of 110 knots.  The last confirmed radar hit on the airplane was at 0829:42, and indicated it was at 10,900 feet with a ground track of 247 degrees, and an estimated ground speed of 120 knots.

PERSONNEL INFORMATION

The pilot held a commercial pilot certificate with airplane single and multiengine land and instrument airplane ratings.  His most recent flight review located in his logbook was dated December 2, 1995.  No other entries were found to indicate a more recent flight review.  A review of the pilot's logbook indicated that he had logged 21.5 hours of flight time during 1998.  The 21.5 hours were logged as pilot-in-command, cross-country, and actual instrument time.  All the flights were completed in the accident aircraft, which he was a co-owner.  His most recent logbook entry was dated August 18, 1998.  A review of his medical certificate information supplied by the Federal Aviation Administration (FAA) indicates he had approximately 1,800 hours of total flight time as of the date of his last medical examination dated December 1, 1997.  His most recent medical certificate was a second-class with a restriction that he must wear corrective lenses.

The operator of the aircraft told Safety Board investigators that he had flown with the pilot (referred to by the operator as "Danny") numerous times.  He said that the pilot was a very conservative pilot, and a good "stick and rudder pilot."  He said that the pilot would fly "mild layer" IFR, but he had never seen him fly "hard" IFR flights.  He said that if the weather were really bad, Danny would drive to the location by car.  He also mentioned that he had never seen him fly over the mountains, instead he would fly up a valley to his location; and he had never seen him fly over mountainous terrain in IFR conditions.  He mentioned that he wasn't sure if Danny would know what to do if he was picking up ice.  He said to the best of his knowledge, Danny had never flown into actual icing conditions in the airplane.  The pilot of the accident airplane had been a 50 percent owner in the accident airplane for 3 years prior to the accident date.

AIRCRAFT INFORMATION

A review of the pilot's credit card statement, and review of the truck fuel slip indicate that the pilot purchased fuel at the Red Bluff Airport after he arrived on September 25, 1998.  The truck fuel slip indicates a purchase of 92.8 gallons of Avgas 100LL for a total purchase price of $181.80.

The aircraft was not equipped with any ice protection on the leading edges of the wings, horizontal stabilizer, or vertical stabilizer; therefore, according to Raytheon Aircraft, this aircraft was not equipped to fly into known icing conditions.

Under the section entitled "Normal Procedures" of the Pilot's Operating Handbook (POH), it lists various equipment that when installed and operable will provide the pilot a degree of protection when icing conditions are inadvertently encountered.  It states that since this equipment has not been demonstrated to meet current requirements for flight into known icing conditions, the pilot must exit such conditions as soon as possible if ice accumulates on the airplane.  The equipment required for icing conditions is appended to this report.

Section X of the POH states that pilot's must carefully review the POH and FAA approved airplane flight manual in

## Aircraft

- Registration: [N554MB](https://openairdocs.org/deregistered/N554MB-2001-04-09), registration cancelled 2001-04-09, S/N TC-2358 (OpenAirDocs)
- Reported make and model: Beech 95-B55
- Registry model: [Beech 95-B55 (T42A)](https://openairdocs.org/model/beech-95-b55-t42a) (registry code 1152706) (OpenAirDocs)
- Category: Airplane
- Serial number: TC-2358
- Airframe hours: 2070
- Engines: Continental IO-470-L 260 horsepower reciprocating
- Damage: Destroyed
- Fire: On-Ground
- Flight: Personal, Part 91
- Registered owner: High Performance Aircraft Inc.
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, January 10, 1998, 40 hours before
- Departed: RBL, RED BLUFF MUNI, CA
- Destination: SGU, ST. GEORGE, UT

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 60; commercial; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: left; toxicology performed; flight hours: 1,839 total, 407 in this make and model, 62 in the last 90 days, 11 in the last 30 days

## Weather

- Conditions: Instrument (IMC), Day
- Wind: 30° at 5 knots
- Visibility: 10 statute miles
- Lowest ceiling: 1,100 ft broken
- Altimeter: 29.00 inHg
- Observed at: NFL, 62 nm away

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 19980926026639A](https://openairdocs.org/incident/19980926026639A), Sep 26, 1998: Beech 95B55, Hawthorne, NV, Destroyed, 1 fatal. (.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…

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.

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