Beech 76 accident near Julian, California, May 11, 2018
On May 11, 2018 at about 3:31 am local time, a 1979 Beech 76, registered N803FC, was destroyed in an accident during maneuvering near Julian, California. It was an instructional flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).
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The NTSB's probable cause their words, unchanged
The pilot's failure to maintain sufficient altitude above mountainous terrain while maneuvering during night conditions in an area prone to turbulence, which resulted in a collision with terrain. Contributing to the accident was the flight instructor's decision to conduct maneuvers over mountainous terrain at night, and failure to ensure that the maneuver was conducted with sufficient separation from terrain.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 11, 2018 · about 3:31 am local time
- Place
- Julian, California · map
- Type
- Accident
- Injuries
- 3 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech 76 NO SERIES, built 1979 · all 76s on the register
- Registration
- N803FC · no longer on the register · serial ME-150
- Damage
- Destroyed
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
During the 2-hour nighttime visual flight rules instructional cross-country flight, radar data identified the airplane on an easterly flight track when the first of two maneuvers over mountainous terrain was initiated. The first maneuver was a left turn from about a 48° course heading to about a 176° course heading. Throughout the turn, the airplane's altitude remained about 5,600 ft mean sea level (msl), and the groundspeed decreased to 55 knots. At the completion of the turn, the groundspeed increased to about 67 knots, and the airplane began to climb to 6,600 ft msl while continuing to the southwest on a course heading of about 195°. The airplane then made a right turn course reversal and resumed the easterly heading for about 10 miles. The radar data then depicted the airplane initiated a second left 180° turn maneuver at an altitude of 6,200 ft msl and a groundspeed of about 121 knots. At the apparent apex of the turn, the airplane was at 6,100 ft msl and a groundspeed of 50 knots. The airplane then began to descend, and the groundspeed increased to 74 knots and then decreased to 50 knots. The last radar return showed the airplane at an altitude of 5,700 ft msl and a groundspeed of 67 knots near the accident site. Radar data revealed that both maneuvers were similar except that the second maneuver began over higher elevation terrain. The airplane's separation from the terrain during the second maneuver was as low as 1,200 ft above ground level (when the airplane was at an altitude of 6,100 ft and was over terrain that was 4,900 ft) before radar contact was lost. Weather reporting in the aera of the accident site indicated extreme turbulence and severe up and downdrafts during high wind conditions. Although there is evidence of strong wind in the area at the time of the second maneuver, there is no consensus among the available wind data. However, the upset occurred immediately downwind of relatively high terrain and inside of a temperature inversion, which can promote wave action and turbulence. Thus, the airplane likely encountered a downdraft and the pilot was unable to recover, resulting in the airplane's subsequent impact with terrain. The operator reported that the instructor was newly hired to the flight school and that the accident flight was his first instructional flight with the company. The course syllabus for the flight identified that several tasks were to be accomplished. A representative of the operator reported that maneuvers were usually performed to facilitate a 2-hour flight. All flight was prohibited below 500 ft agl and minimum cruise altitude of 2,000 ft agl in mountainous terrain. No flight plan had been filed for the nighttime flight, and any en route flight planning documentation was destroyed in the postimpact fire; thus it could not be determined if the pilot or the flight instructor were aware of the weather conditions or terrain elevations while performing the maneuvers.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Controlled flight into terrain or object (CFIT) during maneuvering defining event
The NTSB's findings
- cause Personnel issues › Task performance › Planning/preparation › Flight planning/navigation › Student/instructed pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
- factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Instructor/check pilot
- Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Effect on equipment
- Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on operation
- Environmental issues › Conditions/weather/phenomena › Turbulence › Terrain induced turbulence › Effect on operation
Flight instructor
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 2,000 hours in all; 1,500 as pilot in command
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: fatal
Dual student
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 190 hours in all; 7 in this make and model; 50 in the last 90 days; 8 in the last 30 days; 87 as pilot in command
- Last flight review: April 9, 2018
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 14,150.9 hours
- Last inspection: annual inspection, March 3, 2018; 13 hours since
- Maximum gross weight: 3,916 lb
- Seats: 4
- Landing gear: retractable
- Engine 1: Lycoming O-360-A1G6D (piston); 5,122 hours total
- Engine 2: Lycoming O-360-A1G6D (piston); 7,508 hours total
- Fire on the ground
The flight
- Departed from: APV Apple Valley CA at 2:32 am
- Destination: SEE San Diego/El Cajon CA
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: night
- Wind: from 290° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 61°F (16°C), dew point 55°F (13°C)
- Altimeter: 29.86 inHg
- Observation at 2:53 am from KRNM, 18 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number WPR18FA139.
