# NTSB LAX01FA023: Mooney M-20J, N40VF, Wheaton Springs, CA, October 23, 2000 - Type: NTSB accident investigation - Classification: Accident · Fatal · Field investigation · Final report - Date: October 23, 2000, 14:40 local (21:40 UTC) - Place: Wheaton Springs, CA - Coordinates: 38.959716, -119.900489 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=38.9597&lon=-119.9005&mi=10 - Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping) - Highest injury: Fatal - Injuries: 2 fatal - Status: Completed, report April 17, 2003 - Report: Approved by Office Director - Parties: Federal Aviation Administration, Textron Lycoming - NTSB case key (mKey): 50533 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX01FA023 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/50533/pdf - Page: https://openairdocs.org/ntsb/LAX01FA023 ## Probable cause The pilot's inadequate weather evaluation and attempted VFR flight into IMC, which resulted in the in-flight collision with mountainous terrain. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - In flight encounter with weather, cruise - weather condition - icing conditions - weather condition - low ceiling - weather evaluation - inadequate, pilot in command (cause) - weather condition - obscuration - vfr flight into imc - attempted, pilot in command (cause) - In flight collision with terrain/water, maneuvering - turn to reverse direction - terrain condition - mountainous/hilly ## Analysis The airplane impacted mountainous terrain after the instrument rated commercial pilot reported that he was in the clouds and was picking up ice during a visual flight rules (VFR) cross-country flight. The pilot obtained an updated weather briefing at the departure airport, which advised him that VFR flight along his planned route was not recommended. A review of weather data indicated that the freezing level was at 9,536 feet msl and the bases of clouds ranged anywhere from 400 feet to 3,000 feet agl. The cloud tops in the area of the accident site were 22,000 feet. The accident site was at the 4,650-foot level of the mountain. No anomalies with the engine or airplane were noted that would have prevented their normal operation. ## Factual narrative HISTORY OF FLIGHT On October 23, 2000, approximately 1440 Pacific daylight time, a Mooney M-20J single engine airplane, N40VF, collided with mountainous terrain while maneuvering in the area of Wheaton Springs, California. The airplane was destroyed and the certificated commercial pilot and his passenger received fatal injuries. The airplane was operated as a personal flight by the pilot/owner under 14 CFR Part 91 when the accident occurred. The flight originated from the Mesquite Airport, Mesquite, Nevada, earlier that afternoon, and was destined for Fallbrook, California. Instrument meteorological conditions prevailed in the area of the accident and a visual flight rules (VFR) flight plan was filed. The pilot had departed from Mesquite after making a fuel stop and updating his weather briefing with Reno flight service station (FSS). At the time of the weather update he was advised that VFR flight along his planned route was not recommended. The pilot's son told local enforcement personnel that the pilot and his passenger departed Sun Valley, Idaho, earlier that day with a filed flight plan and a scheduled fuel stop in Mesquite. He added that after refueling, his father would most likely fly closely to I-15 and toward their home in Fallbrook. The flight was approximately 35 miles southwest of Las Vegas when the pilot advised Las Vegas departure control that he was in the clouds and was picking up ice. In his last radio transmission, the pilot stated that he was turning around en route to Jean, Nevada. Radar contact was lost at 1438. When the aircraft did not arrive at Jean, or his final destination in Fallbrook, a search commenced. On October 24, 2000, at 1615, the aircraft was found on 70-degree rising terrain at the 4,650-foot level, near the intersection of Interstate 15 and Nipton road. The location was measured as 35 degrees 26.606 minutes north latitude and 115 degrees 27.798 minutes west longitude. PERSONNEL INFORMATION The pilot held a commercial pilot certificate with ratings for single engine land and instrument airplanes. The pilot's flight logbooks were not located during the course of the investigation, and his detailed flight time experience was not established. According to the pilot's last medical certificate application, he accumulated a total of 2,450 flight hours. It is unknown whether he was current in instrument meteorological flight conditions or if he had successfully completed an instrument competency check. The pilot was issued a third-class medical certificate on July 15, 1999, with a limitation to wear corrective lenses for near and distant vision. The medical certificate was "not valid for any class after May 31, 2001." According to the last medical certificate application, the pilot reported having accumulated a total of 2,450 flight hours. AIRCRAFT INFORMATION The aircraft's maintenance records were not located during the course of the investigation. It is not known whether the airplane was equipped and approved for instrument flight. The aircraft was equipped with a 200 horsepower Lycoming IO-360-A3B6D engine and a two-bladed controllable pitch propeller. METEOROLOGICAL INFORMATION The NTSB conducted a meteorology study and the following information was extracted from the report: The closest weather reporting facility was located at the Las Vegas McCarran International Airport (LAS), which was 40 miles north-northeast of the accident site. The LAS airport elevation is listed as 2,181 feet msl. At 1422, the weather reporting facility issued a special weather observation, which reported the wind from 340 degrees at 6 knots; visibility 10 statute miles; a few clouds at 400 feet agl; ceiling broken at 3,300 feet agl; overcast clouds at 5,000 feet agl; temperature 13 degrees Celsius; dew point 11 degrees Celsius; and an altimeter setting of 30.03 inches of mercury. The remarks section of that special observation reported, "cumulus fractus clouds southeast over mountains and brakes in overcast east." Weather radar data displayed a band of radar echoes running north to south in the immediate vicinity of the accident site. The radar intensity levels ranged between light and moderate precipitation intensities. The closest upper air sounding was located 75 miles northwest of the accident site. The sounding indicated that the atmosphere was moist with a mean surface to 18,000 feet relative humidity of 87.24 percent, and a lifted condensation level (LCL), or base layer of the clouds was observed at 6,272 feet msl (approximately 3,000 feet agl). The air was saturated between the LCL and 23,000 feet. The freezing level was reported as 9,536 feet msl. The Geostationary Operational Environmental Satellite number (GOES-10) data was examined between 1400 and 1500. The data displayed a band of cyclonically curved clouds over the southwestern United States. The infrared image depicted an area of nimbostratus to stratocumulus clouds blanketing the accident site. The radiative temperatures located over the accident site corresponded to a cloud top height of 22,000 feet. WRECKAGE AND IMPACT INFORMATION The airplane wreckage was located on the west side of a mountain that sloped up to its ridge at an approximate 45-50 degree angle. The mountain rose up from a valley located to the west of the accident site. The wreckage debris distribution was along a 093-degree magnetic track. The initial ground scar contained a section of the left wing tip and the left navigation light. The remaining left wing was located 25 feet from the initial impact point. The main wreckage, consisting of the fuselage, empennage, right wing and engine, came to rest approximately 50 feet beyond the left wing (or 75 feet from the initial impact point). The propeller blades and left wing flap were located along the debris path. The cockpit/cabin area was consumed by fire damage. The empennage remained attached to the cabin via resolidified molten metal. Flight control continuity could not be established due to the extent of the fire and impact damage. The right wing's landing gear and flap appeared to be in the retracted position. The emergency locator transmitter was found in the wreckage. A faint signal was audible over the radio receiver in the San Bernardino County Sheriff's emergency response helicopter only when it was directly over the accident site. The engine remained attached to the engine mount, and the mount remained partially attached to the fuselage. The propeller hub was shattered and the propeller blades were detached from the propeller at their hubs. Both blades displayed heavy leading edge gouging, chordwise scrapes and "S" bending. One of the propeller blade tips (approximately 3 inches) was torn from the blade. The engine's number 2 cylinder sustained impact damage to the rocker box, rockers, and valves. The induction and exhaust pipes were displaced aft. The accessories mounted at the rear of the engine sustained thermal damage. The dual magneto was melted and destroyed. The vacuum pump remained attached to the engine and its drive shaft was found intact; however, disassembly revealed that the rotor and vanes were shattered. The bottom spark plugs were removed and displayed normal wear and coloration when compared to the Champion Spark Plug Check-a-Plug chart. The cylinders were examined via the use of a lighted bore scope. There was no evidence of foreign object damage or internal malfunction. Impact damage prevented the full rotation of the crankshaft; however, accessory gear movement was observed during the limited crankshaft rotation. The oil suction screen was removed and found free of visible contaminates. The fuel injection servo was separated from its engine mount and the throttle valve was found in the 3/4-open position. The fuel servo control arms remained attached to their respective controls. The fuel injecti ## Aircraft - Registration: [N40VF](https://openairdocs.org/deregistered/N40VF-2002-05-20), registration cancelled 2002-05-20, S/N 24-3315, built 1993 (OpenAirDocs) - Reported make and model: Mooney M-20J - Registry model: [Mooney M20J](https://openairdocs.org/model/mooney-m20j) (registry code 5870219) (OpenAirDocs) - Registry engine: [Lycoming I0360 SER A&C](https://openairdocs.org/engine/lycoming-i0360-ser-a-c) (registry code 41511, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 24-3315 - Engines: Lycoming IO-360-A3B6D 200 horsepower reciprocating - Damage: Destroyed - Fire: On-Ground - Flight: Personal, Part 91 - Registered owner: William Howard Beamer - Airworthiness certificate: Standard, Normal - Departed: 67L, Mesquite, NV - Destination: L18, Fallbrook, CA - Flight plan: VFR ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 82; injuries: fatal; commercial; airplane ratings: single-engine land; instrument ratings: airplane; medical: class 3, valid medical--w/ waivers/lim; seat: left; toxicology performed; flight hours: 2,450 total ## Weather - Conditions: Day - Wind: 340° at 6 knots - Visibility: 10 statute miles - Lowest ceiling: 3,300 ft broken - Temperature: 55 °F, dew point 52 °F - Altimeter: 30.03 inHg - Observed at: LAS, 40 nm away 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. --- 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.