N611VG

On June 4, 2023, at 1523 eastern daylight time, a Cessna Citation 560 airplane, N611VG, was destroyed when it was involved in an accident near Montebello, Virginia. The airline transport pilot and three passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to flight track records and individuals familiar with the airplane’s flight activity the day of the accident, the airplane’s first flight of the day originated from its home airport of Melbourne International Airport (MLB), Melbourne, Florida, at 1059. The accident pilot conducted the flight as a single pilot without passengers and subsequently landed at Elizabethton Municipal Airport (0A9), Elizabethton, Tennessee, at 1231. While at 0A9, 300 gallons of fuel were added to the airplane and the three passengers were picked up. The accident flight departed 0A9 at 1313, destined for Long Island MacArthur Airport (ISP), Ronkonkoma, New York.

Review of FAA air traffic control audio recordings revealed that the pilot contacted the Atlanta Air Route Traffic Control Center shortly after takeoff and reported climbing through 9,300 ft mean sea level (msl) to 10,000 ft msl. The controller subsequently cleared the airplane to 23,000 ft pressure altitude and the pilot read back the clearance.

At 1322, the pilot was handed off to another controller within Atlanta Center. The pilot contacted the controller, advising that the airplane was maintaining 23,000 ft. The controller cleared the airplane to 29,000 ft and the pilot read back the clearance. At 1325, the controller cleared the airplane to 34,000 ft and the pilot read back the clearance. According to ADS-B data, the airplane was climbing through 26,600 ft at this time. At 1328, the controller amended the previous altitude clearance, instructing the pilot to stop the climb at 33,000 ft for crossing air traffic. The pilot did not respond to the amended clearance, and the airplane continued the climb to 34,000 ft and leveled off. No further radio transmissions from the pilot were received for the remainder of the flight, despite repeated attempts to contact the pilot.

Review of ADS-B data found that the airplane’s flight track to the destination airport was consistent with the filed flight plan route. The airplane arrived overhead of ISP at 1432, maintaining 34,000 ft throughout the flight. The airplane then continued flying southwest on a ground track of about 240°. The flight path showed little deviation in track angle or altitude until 1522, when the airplane entered a rapidly descending right spiral descent into terrain. The figure depicts the ADS-B flight track, the filed flight plan waypoints, and selected time/altitude labels.

Figure. Overview of ADS-B flight track, flight plan waypoints, and accident location, with selected time and altitude labels.

According to a North American Aerospace Defense Command statement, about 1520, the airplane was intercepted by USAF fighter aircraft. The USAF pilots stated that there was nothing remarkable about the exterior of the airplane, such as holes or missing windows or doors. They did not observe any airframe icing, frost on the cockpit or passenger windows, or smoke in the cabin. They observed a person seated in the left cockpit seat, who was slumped completely over into the right seat and who remained motionless throughout their observations. The person was unresponsive to several radio transmissions, intercept flight maneuvers, and flare deployments. The USAF pilots could not see whether this person was wearing a headset or an oxygen mask, and they could not see whether there were any lights flashing in the cockpit. The passenger window shades were open. No movement was observed in the cabin area, and the USAF pilots did not see any shapes that resembled a person in the cabin area.

The airplane impacted mountainous and forested terrain about 1.5 miles north of the Montebello VOR, a short distance from where the airplane’s last ADS-B-derived position was observed. The small area of the debris field and the angle that tree limbs surrounding the debris field were severed were consistent with a high-velocity, near-vertical descent. The wreckage was fragmented and scattered around a main crater, and evidence of a postimpact fire was observed. One engine was generally intact and was located about 100 ft downhill from the impact crater. The other engine was fragmented and located in the debris field. Blades/vanes on both engines were bent opposite the direction of rotation. Flight control continuity could not be established due to the fragmentation of the wreckage. A cockpit voice recorder was not located or recovered from the accident site.

The oxygen high pressure relief valve overboard discharge indicator was found intact. A bleed air flow valve and sections of ducting were also located in the debris. Two passenger oxygen masks were located, which remained attached to their respective box assemblies. One oxygen mask stowage/dropout box assembly and its oxygen shutoff valve were found capped with a dust cap rather than an approved AN cap. No other major portions of the oxygen or pressurization system were located in the debris. No evidence of any preaccident mechanical failures or malfunctions were found that would have precluded normal operation of the airplane or its subsystems.

According to the airframe manufacturer, the airplane’s environmental control system used engine bleed air to pressurize and air condition the cabin, and to defog the cabin and cockpit windows. Flight crew controls for this system were located on the Pressurization – Environmental Control Panel at the front of the center pedestal. This panel included gauges for pressure differential (between the cabin and outside atmosphere), cabin altitude, and cabin altitude rate of change. Also included were controls for the desired cabin altitude, cabin altitude rate of change, cabin temperature, airflow distribution (between the passenger cabin and cockpit), and pressurization source. Flight crew could also use a guarded emergency dump switch to open the pressurization outflow valves and equalize the cabin altitude with airplane altitude up to about 13,000 ft (± 1,500 ft). The cockpit annunciator panel included a red “CAB ALT 10,000 FEET” light that would illuminate when the cabin pressure altitude was above 10,000 ft. This light would also trigger the master warning system, illuminating the master warning light.

Supplementary oxygen was provided to flight crew via sweep-on masks stowed in retainers below each cockpit side window and to passengers via continuous flow masks stowed in the cabin overhead panel at each seat. The passenger system oxygen flow was controlled by an electrically operated solenoid valve, which was actuated by an altitude pressure switch. In the event of a possible decompression, the altitude pressure switch was designed to actuate the solenoid valve between 12,900 to 14,100 ft cabin altitude. When the door actuators were energized with pressure from the supplementary oxygen tank, the stowage/dropout boxes would then open, releasing the masks.

Flight crew controls for the oxygen system were located on the left console. An oxygen control valve switch could be used to direct the flow of oxygen to flight crew only or to both flight crew and passengers; this switch could also be used to manually drop the passenger oxygen masks if they did not drop automatically. Flight crew and passenger supplementary oxygen was provided from a single 76 cubic ft bottle located in the tailcone compartment. When fully charged, it would provide about one hour of oxygen for two flight crewmembers and six passengers. An oxygen pressure gauge was located on the right instrument panel.

According to Continuous Airworthiness Maintenance Program records for the airplane, 5 maintenance items were overdue on the date of the accident, including an inspection of the co-pilot oxygen mask. The most recent maintenance record was a discrepancy report from a visual inspection completed on May 10, 2023. This report listed 26 items, including the emergency exit door seal sticking out of the airplane, improper installation of the humidity regulator, and improper securing of the cabin temperature sensor. The airplane owner declined to address these items. The airplane was taken back to the same maintenance provider on June 1 because the pilot had reported a problem with avionics installed by a different maintenance shop the preceding April. During a visual inspection conducted on June 2, a mechanic from the maintenance provider observed that the airplane looked the same as it did on May 10, except that the pilot-side oxygen mask was not installed. The mechanic also noted that the oxygen level on the airplane was at its minimum servicing level before the airplane departed.

The airplane flight manual preflight cockpit inspection stated that flight crews were to check that oxygen masks were onboard. In addition, the before starting engines checklist included the following step:

Oxygen System - CHECK and STOW (With regulator set at 100% and EMER. Verify green band visible in 02 supply line). Check quantity gage at 1600-1800 PSI and crew masks connected to side console outlets. Pilot's side console oxygen control valve properly positioned to NORMAL. Caution should be exercised as inadvertently placing the oxygen control valve to MANUAL DROP will result in deployment of the cabin masks. The crew masks must be stowed in the quick donning hook and set on 100% for flight above FL 250.

Although the May 10, 2023, discrepancy report indicated that the airplane was equipped with a cockpit voice recorder (CVR), a CVR was not located at the accident site. The airplane was not equipped with a flight data recorder, nor was it required to be.

The pilot did not undergo autopsy or postmortem toxicology testing. Records from the pilot’s primary care provider documented t...