# NTSB WPR18FA253: Commander 114, N6064C, Jean, NV, September 6, 2018 - Type: NTSB accident investigation - Classification: Accident · Fatal · Class 2 · Field · Final report - Date: September 5, 2018, 21:45 local (Sep 6, 2018, 04:45 UTC) - Place: Jean, NV - Coordinates: 35.790832, -115.319442 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=35.7908&lon=-115.3194&mi=10 - Phase of flight: [Approach](https://openairdocs.org/ntsb-phases/500) (OpenAirDocs' grouping) - Defining event: [Approach-VFR pattern base: Loss of control in flight](https://openairdocs.org/ntsb-events/240) - Highest injury: Fatal - Injuries: 1 fatal - Status: Completed - Report: Approved by Office Director - Investigation class: Class 2 - NTSB office: Western Pacific Region - Parties: Federal Aviation Administration, Lycoming Engines - NTSB case key (mKey): 98250 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR18FA253 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/98250/pdf - NTSB docket: https://data.ntsb.gov/Docket?ProjectID=98250 - Page: https://openairdocs.org/ntsb/WPR18FA253 ## Probable cause The pilot failed to maintain adequate speed while maneuvering at a low attitude during night and entered an aerodynamic stall and subsequent spin. ## Findings NTSB's coded findings; those marked are part of the probable cause. - [Use of equip/info: aircraft control](https://openairdocs.org/ntsb-findings/02063040): Personnel issues › Task performance · Pilot (probable cause); cases with it: [Commander 114TC, 2 cases](https://openairdocs.org/ntsb-findings/02063040/cases.md?model=0145002), [All aircraft, 9,295 cases](https://openairdocs.org/ntsb-findings/02063040/cases.md) - [Light condition: dark](https://openairdocs.org/ntsb-findings/03036020): Environmental issues › Conditions/weather/phenomena · Effect on personnel (probable cause); cases with it: [Commander 114TC, 1 case](https://openairdocs.org/ntsb-findings/03036020/cases.md?model=0145002), [All aircraft, 448 cases](https://openairdocs.org/ntsb-findings/03036020/cases.md) - [Performance/control parameters: airspeed](https://openairdocs.org/ntsb-findings/01062010): Aircraft › Aircraft oper/perf/capability · Not attained/maintained (probable cause); cases with it: [Commander 114TC, 2 cases](https://openairdocs.org/ntsb-findings/01062010/cases.md?model=0145002), [All aircraft, 1,681 cases](https://openairdocs.org/ntsb-findings/01062010/cases.md) ## Sequence of events The events NTSB coded, in order, by phase of flight. The defining event best describes what happened. - [Approach-VFR pattern base: Loss of control in flight](https://openairdocs.org/ntsb-events/240) (defining event); cases with it: [Commander 114TC, 3 cases](https://openairdocs.org/ntsb-events/240/sequence.md?model=0145002), [All aircraft, 5,002 cases](https://openairdocs.org/ntsb-events/240/sequence.md) - [Approach-VFR pattern base: Aerodynamic stall/spin](https://openairdocs.org/ntsb-events/241); cases with it: [Commander 114TC, 1 case](https://openairdocs.org/ntsb-events/241/sequence.md?model=0145002), [All aircraft, 1,529 cases](https://openairdocs.org/ntsb-events/241/sequence.md) ## Analysis The pilot departed on a personal cross-country flight in night visual meteorological conditions. While approaching and maneuvering to land at the destination airport, the airplane made a right turn consistent with a right base turn to the destination runway. As the airplane began the base-to-final turn, just before entering a small cloud, it entered a steep, nosedown spin. Subsequently, the airplane impacted terrain and a postimpact fire ensued. The airplane damage and ground scars at the accident site were consistent with a near wings-level attitude at the time of impact. Postaccident examination of the airplane and engine revealed no preimpact anomalies or malfunctions that would have precluded normal operation. It is likely that, while maneuvering to avoid the cloud, the pilot failed to maintain the proper airspeed, which resulted in the airplane entering an accelerated stall. ## Factual narrative Accident Environment A right traffic pattern to land on runway 20R at 0L7 would place the base turn in a relative position close to where the accident site was located. Over a two-day period following the accident, several airplanes landing to the south at 07L were observed flying directly over the accident site, while on the base leg turn to land on runway 20R. The airframe and engine maintenance logbooks were not located during the investigation. According to FAA information, 0L7 had no control tower and had two runways – 2L/20R, and 2R/20L. The traffic pattern altitude was 3,635 ft msl. Runway 02L/20R had pilot activated medium intensity runway lights (MIRL) lighting. A white-green beacon was also operational from sunset to sunrise. Runway 20R was 4,600 ft long and 75 ft wide. On September 5, 2018, about 2145 Pacific daylight time, a Commander Aircraft Company AC-114TC, N6064C, was destroyed when it was involved in an accident near Jean, Nevada. The private pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. A review of the Nevada’s Department of Transportation, traffic camera video, showed the accident airplane flying west of and parallel to Interstate 15. The airplane turned to a course consistent with a right base turn to runway 20R at Jean Airport (0L7). The airplane then began another right turn and about halfway through the turn and just before entering a small cloud, the airplane entered a steep nose-down descent and spin then impacted the ground. A post impact fire ensued that consumed most of the airplane. The Clark County Coroner/Medical Examiner Office, Las Vegas, Nevada, conducted an autopsy on the pilot. The medical examiner determined that the cause of death was “multiple blunt force injuries.” The FAA's Forensic Sciences Laboratory performed toxicological testing on the pilot. Testing was negative for drugs and volatiles, except for ethanol detected in the brain and muscle specimens. Some or all of the ethanol may be from sources other than consumption. The airplane impacted desert terrain populated with light vegetation about 1 mile north of 0L7. The site was surveyed by the National Transportation Safety Board (NTSB) drone support team. The debris field was determined to be about 280 ft in length. The first point of impact was a large disturbance in the ground which was consistent with the front of the airplane and wings impacting terrain at a near wings level attitude. The area of disturb dirt measured about 10 ft lengthwise, 28 ft wide, and 2 ft in depth at the middle portion and 6 inches in depth where the wings impacted terrain. Several parts of the airplane’s fuselage and wings were located within the disturbance. Parts of the left-wing tip were observed on the left edge of the ground disturbance. A burnt fan pattern was observed on the desert sand forward of each wing, consistent with fuel being sprayed out during impact and then being ignited. Allmajor structural components and primary flight controls of the airplane were located at the accident site. The main wreckage consisted of the fuselage, engine, wings, and empennage. The fuselage was mostly consumed by the postimpact fire. The engine remained attached to the fuselage. The front of the aircraft and cabin area were destroyed during the impact sequence and the postimpact fire. The empennage was folded under the left wing and remained partially attached to the fuselage; the tail cone had separated. The airplane was identified by the registration plate located in the aft fuselage. The leading edges of the wings displayed compression and impact damage. The vertical stabilizer was almost entirely consumed by the fire. The rudder remained attached to the vertical stabilizer. The elevators remained attached to the empennage, and the elevator trim was observed near the neutral position. Flight control continuity was established from the ailerons to the cockpit controls. Flight control continuity was also established to the rudder and elevator despite observed overload separations of flight control cables. Both the left and right wings remained attached to the fuselage. Both ailerons and flaps were attached. The right aileron remained partially attached only by the outboard connection. The engine displayed impact and thermal damage. The three-bladed propeller remained attached and one blade was bent aft near the hub. Another blade was intact and was bent and curled near the tip. The third blade was intact and exhibited gouging, torsional twisting, and chordwise striations across the cambered surface and trailing edge. The landing gear was observed in the extended position. Additionally, impact marks and damage on the main landing gear assembly were consistent with the gear in the extended position. The cockpit area sustained substantial thermal damage and no instrumentation was readable. The fuel selector handle was not observed. The examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. ## Aircraft - Registration: [N6064C](https://openairdocs.org/deregistered/N6064C-2019-10-23), registration cancelled 2019-10-23, S/N 20024, built 1999 (OpenAirDocs) - Reported make and model: Commander 114 (TC) - Registry model: [Commander 114TC](https://openairdocs.org/model/commander-114tc) (registry code 0145002) (OpenAirDocs) - Registry engine: [Lycoming IO-540 series](https://openairdocs.org/engine/lycoming-io-540-series) (registry code 41530, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 20024 - Year built: 1999 - Engines: Lycoming IO-580-B1A 315 horsepower reciprocating - Damage: Destroyed - Fire: On-Ground - Flight: Personal, Part 91 - Airworthiness certificate: Standard, Normal - Departed: RAL, Riverside, CA - Destination: Same as departure - Airport: 0L7, Jean, runway 20R, 4,600 × 75 ft - Equipment: Unknown ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 75; injuries: fatal; private; airplane ratings: single-engine land; medical: class 3, with waivers/limitations; seat: left; toxicology performed; flight hours: 1,718 total ## Weather - Conditions: Visual (VMC), Night/dark - Wind: 190° at 6 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 82 °F, dew point 48 °F - Altimeter: 30.02 inHg - Observed at: KHND, 14 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 20180905013159A](https://openairdocs.org/incident/20180905013159A), Sep 5, 2018: Commander Aircraft Co 114TC, Jean, NV, Destroyed, 1 fatal. On September 5, 2018, at approximately 2145 PDT, a rockwell Commander 114TC, single engine airplane impacted desert terrain approximately 1 mile north of the… ## Docket (8 files) The files NTSB released with the investigation on December 2, 2020, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=98250. 5.6 MB in all. - Materials laboratory factual report 18-101 (item 1, PDF, 3 pages, 640 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=7176774&FileExtension=pdf&FileName=18-101%20-%20elevator%20bell%20crank-Rel.pdf - Record of email (item 2, PDF, 1 page, 48 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9480704&FileExtension=pdf&FileName=Record%20of%20Email%20WPR18FA253-Rel.pdf - Aerial imagery field notes (item 3, PDF, 6 pages, 2.0 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9615799&FileExtension=pdf&FileName=WPRN6064C%20-%20JeanNV%20Aerial%20Imagery%20Field%20Notes-Rel.pdf - Airframe and engine examination report (item 4, PDF, 3 pages, 100 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9615781&FileExtension=pdf&FileName=WPR18FA253%20-%20Engine-Airframe%20Exam%20Notes-Rel.pdf - Statement of party representatives to NTSB investigation (item 5, PDF, 1 page, 85 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9481011&FileExtension=pdf&FileName=NTSB%20party%20form_Lycoming-WPR18FA253_Redacted-Rel.pdf - Release of aircraft wreckage, NTSB form 6120.15 (item 6, PDF, 1 page, 42 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9481020&FileExtension=pdf&FileName=2020%20Retention-Release-of-Wreckage-Form_Redacted-Rel.pdf - Toxicological report (item 7, PDF, 1 page, 118 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9481002&FileExtension=pdf&FileName=Tox%20Test_Redacted-Rel.pdf - Highway video (video courtesy of michael jorgensen) (item 8, MP4, 2.6 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=9615146&FileExtension=mp4&FileName=Highway%20Video-Rel.mp4 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.