Virginia

The airplane departed Wichita-Dwight D. Eisenhower Airport at 1739LT on a schedule service (flight AA5342/JIA5342) to Washington-Ronald Reagan-National Airport, carrying 60 passengers and 4 crew members. Following an uneventful flight, the crew was cleared to start the descent from the south. On final approach to runway 33, after being cleared to land, at an estimated altitude of 350 feet, while approximately one km short of runway, the airplane collided with a US Army Sikorsky UH-60 Blackhawk registered 00-26860 and carrying three crew members. Under callsign PAT25, the helicopter was approaching Joint Base Anacostia-Bolling when the collision occurred. Both airplanes dove into the Potomac River. All 64 occupants were killed, among them two world-champion Russian figure skaters as well as 'several members' of the US figure skating community. All three occupants in the Black Hawk were also killed. First fatal accident involving a CRJ-700 and worst accident in the US since November 2001.

After departure from Manassas-Harry P. Davis Field Airport, Virginia, the twin engine airplane continued to the southwest, bound for Georgetown, South Carolina. While cruising at an altitude of 20,000 feet and approaching an area of marginal weather conditions, the pilot apparently elected to modify his route when the airplane entered an uncontrolled descent and crashed in a wooded area located in Palmyra. Both occupants were killed.

The airplane departed Fort Lauderdale-Hollywood International Airport Runway 28R at 1346LT with five people on board. It continued to the north at FL390 then successively descended to FL370 and FL330 when the crew encountered an unexpected situation and elected to divert to Hot Springs-Ingalls Field, Virginia. On final approach, the airplane went out of control and crashed in a wooded area located few km short of runway 25. The airplane was totally destroyed by impact forces and a post crash fire and all five occupants were killed, among them one child.

The pilot and three passengers departed on a cross-country flight. Shortly after the airplane climbed through 26,600 ft, the pilot stopped responding to air traffic control instructions. According to ADS-B data, the airplane continued climbing to 34,000 ft, then flew at that altitude along its flight plan waypoints, turning southwest to overfly the intended destination about 1 hour later. The airplane continued flying for about another hour along a relatively constant track and altitude before entering a spiraling descent and impacting terrain. United States Air Force (USAF) pilots intercepted the airplane about 2 minutes before it began the spiraling descent. They observed no breaches of the airplane structure or doors, no smoke in the cockpit or passenger cabin, and no oxygen masks deployed in the cabin. One occupant was observed slumped over in the pilot seat and no movement or other occupants were observed in the cabin. Based on the lack of response to air traffic control communications, ADS-B data showing the airplane following its flight plan waypoints at the altitude last assigned by air traffic control, and the USAF pilot observations, it is likely that the pilot of the accident airplane became incapacitated during the climb to cruise altitude. It is also likely the airplane trajectory was then directed by the autopilot until a point at which it was no longer able to maintain control. The pilot had medical conditions, including high blood pressure and high cholesterol, that represented some increased risk of an impairing or incapacitating cardiovascular event. In addition, the pilot had prior prescriptions for medications that could be impairing if used too recently before flight. However, there was no evidence of the pilot being at exceptionally high incapacitation risk, or of using medications inappropriately. Based on the accident circumstances, it is likely that all the airplane occupants were incapacitated due to a common environmental condition, such as loss of cabin pressurization. Maintenance records indicated that, at the time of the accident flight, five items were overdue for inspection, including the co-pilot oxygen mask. About 4 weeks before the accident flight, maintenance personnel noted 26 discrepancies that the owner declined to address, including several related to the pressurization and environmental control system. Furthermore, 2 days before the accident flight, maintenance personnel noted that the pilot-side oxygen mask was not installed, and the supplementary oxygen was at its minimum serviceable level. At that level, oxygen would not have been available to the airplane occupants and passenger oxygen masks would not have deployed in the event of a loss of pressurization. No evidence was found to indicate that the oxygen system was serviced or that the pilot-side oxygen mask was reinstalled before the accident flight. Altitude-related hypoxia, although not verifiable from forensic medical evidence, likely explains the incapacitation of the airplane occupants. According to the FAA Pilot’s Handbook of Aeronautical Knowledge, impairing effects from hypoxia are often vague and are experienced differently by different individuals; they include confusion, disorientation, diminished judgment and reactions, worsened motor coordination, difficulty communicating and performing simple tasks, a false sense of well-being, diminished consciousness, and, if conditions aren’t remedied or mitigated, death. Between 30,000 and 35,000 ft, the time of useful consciousness for a pilot to take protective action against hypoxia, including donning an oxygen mask and descending, is about 1/2 to 2 minutes. These times depend on multiple variables, including medical factors, with substantial variation among individuals. The times are decreased by about half when depressurization is rapid. However, gradual depressurization can be as dangerous or more dangerous than rapid depressurization because of its potential to insidiously impair a pilot’s ability to recognize and respond to the developing emergency until the pilot is no longer effectively able to do so. Cognitive impairment from hypoxia makes it harder for affected individuals to recognize their own impairment. Based on the available information, it is likely that the airplane occupants became hypoxic due to a lack of oxygen during the flight and became incapacitated. However, the reason for the loss of pressurization, and whether it was rapid or progressed over time, could not be determined.

The crew departed Norfolk-Chambers Field NAS on a local mission. En route, the airplane crashed in unknown circumstances in the Chincoteague Bay, off Wallops Island. The aircraft came to rest partially submerged in shallow waters. Two crew members were rescued while the pilot Lt Hyrum Hanlon was killed.

The aircraft, assigned to Airborne Command & Control Squadron (VAW) 120 Fleet Replacement Squadron, departed Norfolk-Chambers Field NAS on a training flight. In the afternoon, the crew encountered an unexpected situation, abandoned the aircraft and bailed out. Out of control, the aircraft entered a dive and crashed in a field located near Wallops Island. All four occupants parachuted to safety while the aircraft was totally destroyed by impact forces and a post crash fire.

The instrument rated private pilot was drinking alcohol before he arrived at the airport. Before the flight, he did not obtain a weather briefing or file an instrument flight rules flight plan for the flight that was conducted in instrument meteorological conditions. The pilot performed a 3-minute preflight inspection of the airplane and departed with a tailwind (even though he had initially taxied the airplane to the runway that favored the wind) and without communicating on the airport Unicom frequency. After departure, the airplane climbed to a maximum altitude of 11,500 feet mean sea level (msl), and then the airplane descended to 4,300 ft msl (which was 1,400 ft below the minimum safe altitude for the destination airport) and remained at that altitude for 9 minutes. Afterward, the airplane began a descending left turn, and radar contact was lost at 2054. The pilot did not talk to air traffic control during the flight and while operating in night instrument meteorological conditions. During the flight, the airplane flew through a line of severe thunderstorms with heavy rain, tornados, hail, and multiple lightning strikes. Before the airplane's descending left turn began, it encountered moderate-to-heavy rain. The airplane's high descent rate of at least 6,000 ft per minute and impact with a mountain that was about 450 ft from the last radar return, the damage to the airplane, and the distribution of the wreckage were consistent with a loss of control and a high-velocity impact. Examination of the airplane revealed no evidence of any preimpact mechanical anomalies. Based on the reported weather conditions at the time the flight, the pilot likely completed the entire flight in night instrument meteorological conditions. His decision to operate at night in an area with widespread thunderstorms and reduced visibility were conducive to the development of spatial disorientation. The airplane's descending left turn and its high-energy impact were consistent with the known effects of spatial disorientation. The pilot was not aware of the conditions near and at the destination airport because he failed to obtain a weather briefing and was not communicating with air traffic control. Also, the pilot's decision to operate an airplane within 8 hours of consuming alcohol was inconsistent with the Federal Aviation Administration's regulation prohibiting such operations, and the level of ethanol in the pilot's toxicology exceeded the level allowed by the regulation. Overall, the pilot's intoxication, combined with the impairing effects of cetirizine, affected his judgment; contributed to his unsafe decision-making; and increased his susceptibility to spatial disorientation, which resulted in the loss of control of the airplane.

The instrument-rated pilot was on a cross-country flight. According to air traffic control records, an air traffic controller provided the pilot vectors to an intersection to fly a GPS approach. Federal Aviation Administration radar data showed that the airplane tracked off course of the assigned intersection by 6 nautical miles and descended 800 ft below its assigned altitude before correcting toward the initial approach fix. The airplane then crossed the final approach fix 400 ft below the minimum crossing altitude and then continued to descend to the minimum descent altitude, at which point, the pilot performed a missed approach. The missed approach procedure would have required the airplane to make a climbing right turn to 2,500 ft mean sea level (msl) while navigating southwest back to the intersection; however, radar data showed that the airplane flew southeast and ascended and descended several times before leveling off at 2,800 ft msl. The airplane then entered a right 360-degree turn and almost completed another circle before it descended into terrain. Examination of the wreckage revealed no evidence of any preimpact mechanical malfunctions or failures. During the altitude and heading deviations just before impact, the pilot reported to an air traffic controller that adverse weather was causing the airplane to lose "tremendous" amounts of altitude; however, weather radar did not indicate any convective activity or heavy rain at the airplane's location. The recorded weather at the destination airport about the time of the accident included a cloud ceiling of 400 ft above ground level and visibility of 3 miles. Although the pilot reported over 4,000 total hours on his most recent medical application, the investigation could not corroborate those reported hours or document any recent or overall actual instrument experience. In addition, it could not be determined whether the pilot had experience using the onboard GPS system, which had been installed on the airplane about 6 months before the accident; however, the accident flight track is indicative of the pilot not using the GPS effectively, possibly due to a lack of proficiency or familiarity with the equipment. The restricted visibility and precipitation and maneuvering during the missed approach would have been conducive to the development of spatial disorientation, and the variable flightpath off the intended course was consistent with the pilot losing airplane control due to spatial disorientation. Toxicological tests detected ethanol and other volatiles in the pilot's muscle indicative of postmortem production.