N305LMooney Aircraft M20K

On June 10, 2022, about 0800 Pacific daylight time, a Mooney M20K, N305L was destroyed when it was involved in an accident near Camarillo, California. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot had flown from his home base of Phoenix Deer Valley Airport (DVT), Phoenix, Arizona, to Camarillo Airport (CMA), Camarillo, California, on the day before the accident, and the accident flight was to be the return trip. The pilot’s wife stated that he called her at 0600 on the day of the accident to tell her that he would delay the departure because of cloudy weather.

About 0724 the pilot contacted Leidos Flight Service and requested an abbreviated weather briefing. The briefer stated that a marine layer was present in Camarillo, and the pilot responded that it was “socked in.” The pilot requested cloud top information and was provided with a pilot report (PIREP) that indicated 700-ft cloud tops along the coast about 40 miles to the southeast at Los Angeles International Airport, Los Angeles, California, in the adjoining Los Angeles Basin. The pilot responded, “there you go.” After receiving information on a local temporary flight restriction, the pilot asked how he should file a VFR-on-top flight plan with the briefer. The briefer stated that he would need to file an IFR flight plan with a VFR-on-top clearance and that they could do it immediately. The weather at the time included calm wind, a visibility of 4 miles, a 300ft agl overcast ceiling, and mist.

After the flight was plan filed, the pilot contacted the CMA tower controller. The controller provided the pilot with an IFR clearance to DVT with instructions to turn right to 275° after departure for radar vectors, climb and maintain 3,000 ft, and expect 7,000 ft 5 minutes after departure. The pilot replied but omitted the initial 3,000-ft altitude instruction, which was corrected by the controller. About 8 minutes later, the pilot stated that he was ready to taxi the airplane and was given instructions to taxi to runway 26 via taxiways F and A. During the next few minutes, the pilot began to taxi the airplane but appeared to be using taxiway G. The pilot then told the controller that he had not previously departed from CMA, and the controller provided the pilot with amended taxi instructions to the runway 26 run-up area.

About 0758, the airplane was cleared for takeoff; about 90 seconds later, the pilot was instructed to contact the departure controller. The pilot acknowledged the instruction but did not contact the departure controller. About 1 minute later, a controller from the Southern California Terminal Radar Approach Control called the CMA tower controller and reported that the pilot had not made contact and that the airplane did not appear on radar.

A witness driving along Route 101, a freeway located parallel to and about 0.5 miles north of the departure runway, reported seeing a low flying airplane traveling at a high speed from south to north. The witness stated that the airplane did not appear to have any trailing smoke or vapors and that he could hear the engine operating. The airplane was in a 90° right bank with its belly in view. The airplane then collided with the ground just past the freeway, and a postcrash fire ensued. A video from another witness’ dashboardmounted camera captured the flames and the low clouds and fog enveloping the area.

The pilot’s most recent flight review occurred on May 22, 2021. The NTSB’s attempts to reach the flight instructor who provided the pilot with his most recent flight review were unsuccessful.

FAA regulations require that for a pilot to act as pilot in command under IFR conditions they must maintain currency by performing and logging within a 6-calendar month period preceding the flight, at least; 6 instrument approaches, holding procedures and tasks, and intercepting and tracking courses through the use of navigational electronic systems. The procedures should be performed in actual weather conditions, or under simulated conditions using a view-limiting device.

The pilot’s last logbook showed that he generally documented the specific flights required as part of flight currency and proficiency, such as instrument approaches and flight reviews. The remaining flight time was entered in block entries covering periods of time that often coincided with engine oil changes.

An entry dated March 31, 2022, indicated the pilot had performed an unknown number of RNAV (area navigation) instrument approaches during a round-trip flight from DVT to Hayward, California. A review of publicly available flight data for the accident airplane revealed that its last eight flights from May 4 to June 9, 2022, were not documented in the pilot’s logbook. An entry dated June 6, 2022, noted that the pilot had performed two instrument landing system approaches at Casa Grande Municipal Airport (CGZ), Casa Grande, Arizona.

The first logbook entry, dated July 11, 2012, indicated that the pilot’s total previous flight experience was 1,672 hours. The remaining 11 pages showed that the pilot had flown about 787 hours, 80 hours of which were in actual instrument conditions. The logbook had four references to “VFR on top,” the last of which occurred in May 2019.

The pilot’s most recent FAA medical certification examination was in 2014, and his third-class medical certificate expired in 2016. According to FAA records, the pilot completed a BasicMed Course on May 6, 2019, and reported completing the BasicMed comprehensive medical examination checklist (CMEC) the same day. No CMEC form was found with the pilot’s logbook or was otherwise recovered during the investigation. Records were requested from and provided by the physician who the pilot indicated had performed the CMEC examination. These records did not include a CMEC examination or a record of an examination on May 6, 2019. (The FAA does not require a physician to retain records related to a BasicMed examination, and CMEC forms are not routinely submitted to the FAA.)

The pilot’s wife stated that he had previously flown in actual instrument conditions and that he might have flown in such conditions during a trip to Alameda, California, in February 2022. She stated that he had no appointments, meetings, or compelling reason to return home on the day of the accident.

FAA records indicated that the pilot purchased the airplane in 2006.

The airplane was fueled to capacity at a CMA fixed-base operator shortly after the airplane landed on the day before the accident. The fuel supplier tested the fuel after the accident, which yielded nominal results.

The airplane was equipped with an autopilot. The roll servo was repaired on March 11, 2021. and an overhauled vacuum pump was installed on March 8, 2022.

CMA is located within a coastal basin about 7.5 miles from the Pacific Ocean. The area is affected by marine layer weather patterns, particularly during the early summer months.

A terminal aerodrome forecast for CMA issued at 0506 on the day of the accident indicated persistent marine layer conditions throughout the morning and early afternoon with a 3-knot wind, 6-mile visibility, mist, and a broken ceiling at 600 ft agl. A forecast issued at 0713 indicated that these conditions would worsen between 0700 and 0900 with expected variable wind at 3 knots, 1/2mile visibility, fog, and an overcast ceiling at 200 ft agl.

Area PIREPs surrounding the time of the accident indicated cloud tops between 400 and 1,600 ft. A Graphical Forecasts for Aviation issued before the accident flight, which was valid at the accident time, indicated broken cloud coverage with bases at 300 ft and tops at 2,100 ft.

As previously stated, weather information was relayed to the pilot during his 0724 call to Leidos Flight Service. No evidence indicated what, if any, additional weather information the pilot received before or during the accident flight.

The weather observations surrounding the accident time were consistent with low IFR to IFR conditions. Low IFR is defined as ceilings below 500 ft agl and/or visibility less than 1 statute mile.

FAA records indicated that the pilot purchased the airplane in 2006.

The airplane was fueled to capacity at a CMA fixed-base operator shortly after the airplane landed on the day before the accident. The fuel supplier tested the fuel after the accident, which yielded nominal results.

The airplane was equipped with an autopilot. The roll servo was repaired on March 11, 2021. and an overhauled vacuum pump was installed on March 8, 2022.

The first point of impact was identified by a wing-shaped imprint at the top wall of a building located south of the freeway, 1 mile west-northwest of the departure end of runway 26. The imprint was about 50 ft agl, and its shape corresponded to a 15° rightwing-low impact attitude. The outboard section of the right wing and aileron were located on the building’s flat roof. A trail of debris consisting of wing skin fragments and the right flap continued on a heading of about 035° and across the freeway to a secondary impact point in a strawberry field that was 750 ft beyond the first impact point (as shown in figures 1 and 2).

Figure 1. Location of the wreckage and debris field in relation to the departure runway.

Figure 2. Debris field facing southeast.

Note: The debris field travels from right to left, with the initial impact point to the right on the other side of the freeway. The departure end of runway 8 is 1 mile in the background beyond the clouds.

The debris beyond the secondary impact point consisted of the propeller assembly, cabin skin fragments, and flight instruments, all of which led to the main wreckage, which was on the same heading about 250 ft downrange.

The airframe sustained extensive impact and thermal damage through to the leading edge of the tail assembly. Impact and thermally damaged remnants of the entire left wing, along with the inboard section of the right wing, remained attached to the center of the cabin.

The elevator trim jack screw located in the moving tail assembly showed an extension was extended consistent with the takeoff trim setting. Both the left and right main landing gear remained within their wheel wells, and examination of the landing gear electric actuator revealed that its jackscrew was extended, consistent with the landing gear being in the up-and-raised position. A section of the right seat rail and lower seat was located and appeared to be set in the middle of its travel range.

The flight controls from the cabin to each control surface sustained significant bend, crush, and thermal damage. Examination indicated that all failures and separations exhibited overload damage signatures.

The vacuum pump was undamaged and remained attached to its pad on the engine accessory case. The unit’s plastic drive coupling was intact, and disassembly of the pump revealed that the internal rotor and vanes were undamaged and intact. Damage prevented an accurate assessment of the operational viability of the attitude indicator and horizontal situation indicator, both of which were vacuum driven. Thermal and impact damage prevented an accurate assessment of the condition and operation of the remaining flight electrical instruments and the autopilot.

No evidence indicated a catastrophic engine failure, and the top spark plugs exhibited gray coloration to their electrodes, consistent with normal engine operation, and wear signatures consistent with a short service life. The turbocharger assembly compressor blades exhibited tears and bending opposite the direction of rotation, and rubbing was observed between the blade tips and outer scroll of the turbine wheel.

All three propeller blades remained attached to their hub, which had detached from the engine crankshaft. The blades exhibited leadingedge nicks and abrasions along with chordwise scratches and tip serrations. One blade exhibited trailing edge s-bending, and multiple slash marks in the dirt in the debris field were consistent with propeller rotation at impact.

No evidence indicated any preimpact mechanical or engine malfunction that would have precluded normal operation. No evidence indicated a bird strike.

Radar and ADS-B flight tracks for the accident airplane were not captured by any FAA or an associated facility. At runway elevation (77 ft mean sea level), CMA sits along the edge of the Point Mugu Naval Air Station radar sensor coverage area, which is the closest radar sensor to the accident site. The accident site was about the same elevation as CMA airport. Even though the accident airplane was equipped with an ADS-B transponder, theoretical ADS-B coverage models are not available for altitudes below 500 ft mean sea level, so radar sensor coverage for the accident site could not be determined.

The Medical Examiner of Ventura County, State of California, performed an autopsy on the pilot. According to the autopsy report, the pilot’s cause of death was blunt trauma. The pilot had evidence of an enlarged heart, 60% narrowing of a coronary artery, a localized area of scarring of the heart, a mitral valve replacement, and an implanted cardiac pacemaker/defibrillator. The autopsy report stated that a representative from the pacemaker/defibrillator manufacturer attempted to download recorded data from the damaged device but was unsuccessful.

As previously stated, the pilot was operating the airplane with BasicMed provisions, which allow pilots who meet certain requirements to fly without current medical certification. Among those requirements are the following: a pilot must have completed a BasicMed Course within 24 calendar months and must have had a medical examination with a state-licensed physician using the CMEC within 48 months. Pilots with certain medical conditions, including heart valve replacement, may not exercise BasicMed privileges unless they have completed the process for obtaining an FAA Authorization for Special Issuance of a Medical Certificate for the relevant conditions. The accident pilot had not completed this process for his mitral valve replacement.