Jeffersonville

On November 30, 2018, about 1028 central standard time, a Cessna 525A (Citation) airplane, N525EG, was destroyed when it was involved in an accident near Memphis, Indiana. The pilot and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 business flight. The cross-country flight originated from Clark Regional Airport (JVY), Jeffersonville, Indiana, and was en route to Chicago Midway International Airport (MDW), Chicago, Illinois. The airplane was equipped with automatic dependent surveillance–broadcast (ADS-B), which recorded latitude and longitude from GPS, pressure and geometric altitude, and selected altitude and heading. The airplane was also equipped with a cockpit voice recorder (CVR), which recorded the accident flight and annunciations from the enhanced ground proximity warning system (EGPWS). It was not equipped with a flight data recorder (FDR) nor was it required to be. Review of the CVR transcript showed that the pilot operated as a single pilot but verbalized his actions as he configured the airplane before departure. He referenced items from the Before Taxi checklist and included in his crew briefing that in the event of a problem after takeoff decision speed, he would handle it as an in-flight emergency and “fly the airplane, address the problem, get the autopilot on, talk on the radios, divert over to Stanford.” The air traffic controller provided initial clearance for the pilot to fly direct to the STREP intersection and to climb and maintain 3,000 ft mean sea level. Before the departure from JVY, the pilot announced on the common traffic advisory frequency that he was departing runway 36 and verbalized in the cockpit “this is three six” before he advanced the throttles. The flight departed JVY about 1024:36 into instrument meteorological conditions. The CVR recorded the pilot state that he set power to maximum cruise thrust, switched the engine sync on, and turned on the yaw dampers. The pilot also verbalized his interaction with the autopilot, including navigation mode, direct STREP, and vertical speed climb up to 3,000 ft. According to the National Transportation Safety Board’s (NTSB) airplane performance study, the airplane climbed to about 1,400 ft msl before it turned left onto a course of 330° and continued to climb. The CVR recorded the pilot state he was turning on the autopilot at 1025:22. At 1025:39, the pilot was cleared up to 10,000 ft and asked to “ident,” and the airplane was subsequently identified on radar. The pilot verbalized setting the autopilot for 10,000 ft and read items on the After Takeoff/Climb checklist. The performance study indicated that the airplane passed 3,000 ft about 1026, with an airspeed between 230 and 240 kts, and continued to climb steadily. At 1026:29, while the pilot was conducting the checklist, the controller instructed him to contact the Indianapolis Air Route Traffic Control Center; the pilot acknowledged. At 1026:38, the pilot resumed the checklist and stated, “uhhh lets seeee. Pressurization pressurizing anti ice de-ice systems are not required at this time.” The performance study indicated that, at 1026:45, the airplane began to bank to the left at a rate of about 5° per second and that after the onset of the roll, the airplane maintained airspeed while it continued to climb for 12 seconds, consistent with engine power not being reduced in response to the roll onset. At 1026:48, the CVR recorded the airplane’s autopilot disconnect annunciation, “autopilot.” The performance study indicated that about this time, the airplane was in about a 30° left bank. About 1 second later, the pilot stated, “whooooaaaaah.” Over the next 8 seconds, the airplane’s EGPWS annunciated six “bank angle” alerts. At 1026:57, the airplane reached its maximum altitude of about 6,100 ft msl and then began to descend rapidly, in excess of 11,000 ft per minute. At 1026:58, the bank angle was about 70° left wing down, and by 1027:05, the airplane was near 90° left wing down. At 1027:04, the CVR recorded a sound similar to an overspeed warning alert, which continued to the end of the flight. The performance study indicated that about the time of the overspeed warning, the airplane passed about 250 kts calibrated airspeed at an altitude of about 5,600 ft. After the overspeed warning, the pilot shouted three expletives, and the bank angle alert sounded two more times. According to the performance study, at 1027:18, the final ADS-B data point, the airplane was about 1,000 ft msl, with the airspeed about 380 kts and in a 53° left bank. At 1027:11, the CVR recorded the pilot shouting a radio transmission, “mayday mayday mayday citation five two five echo golf is in an emergency descent unable to gain control of the aircraft.” At 1027:16, the CVR recorded the EGPWS annunciating “terrain terrain.” The sound of impact was recorded about 1027:20. The total time from the beginning of the left roll until ground impact was about 35 seconds. The accident site was located about 8.5 miles northwest of JVY.

Prior to the flight, the pilot preflighted the airplane and recalled observing the fuel gauge indicating full; however, he did not visually check the fuel tanks. The airplane departed and the en route portion of the flight was uneventful. During the downwind leg of the circling approach, the engines began to surge and the pilot added full power and turned on the fuel boost pumps. While abeam the approach end of the runway on the downwind leg, the engines again started to surge and subsequently lost power. He executed a forced landing and the airplane impacted terrain short of the runway. A postaccident examination by Federal Aviation Administration inspectors revealed the fuselage was buckled in several areas, and the left wing was crushed and bent upward. The fuel tanks were intact and approximately one cup of fuel was drained from the single fuel sump. Fueling records indicated the airplane was fueled 3 days prior to the accident with 135 gallons of fuel or approximately 4 hours of operational time. Flight records indicated the airplane had flown approximately 4 hours since refueling when the engines lost power.

On January 27, 2001, about 1737 mountain standard time, a Raytheon (Beechcraft) Super King Air 200, N81PF, owned by North Bay Charter, LLC, and operated by Jet Express Services, crashed into rolling terrain near Strasburg, Colorado. The flight was operating on an instrument flight rules (IFR) flight plan under 14 Code of Federal Regulations (CFR) Part 91. The flight departed about 1718 from Jefferson County Airport (BJC), Broomfield, Colorado, with two pilots and eight passengers aboard. The pilot who occupied the left seat in the cockpit was solely responsible for the flight. The pilot who occupied the right seat in the cockpit, referred to in this report as the "second pilot," was not a required flight crewmember. N81PF was one of three airplanes transporting members of the Oklahoma State University (OSU) basketball team and associated team personnel to Stillwater Regional Airport (SWO), Stillwater, Oklahoma, after a game at the University of Colorado at Boulder that afternoon. All 10 occupants aboard N81PF were killed, and the airplane was destroyed by impact forces and a post crash fire. Instrument meteorological conditions (IMC) prevailed at the time of the accident.

The pilot said that he 'landed properly' on the runway, touching down at about 700 feet from the approach end. He said that he 'applied brakes, which had no effect, ran out of runway, and turned to the right to avoid trees. [The] Grassy field should have worked out, except for the drainage ditch.' The pilot said that later he was told that there was a tail wind estimated at 45 knots, when he landed. Examination of the airplane revealed no anomalies. Approximately 34 minutes before the accident, the weather observation at Louisville, Kentucky, 11 miles south of the accident site, reported winds of 320 degrees at 16 knots, with gusts to 20 knots.

The flight was for the purpose of transporting six Crane officials from Chicago, Illinois, to Louisville, Kentucky, to attend a business convention. Departure was from O'Hare-Chicago International Airport on a VFR flight plan (changed en route to IFR) with the Crane Company's Chief Pilot Randolph A. Mulherin in command, and Robert H. Robinette, also a Crane pilot, as copilot. Gross weight upon departure was estimated to be 27,360 pounds; the maximum permissible takeoff weight was 31,000 pounds. Shortly after takeoff the pilot gave a routine report to Chicago radio of his time off as 0908 and his estimated elapsed flight time as one hour and 20 minutes. He did not request weather information at that time. Other radio contacts followed as the flight progressed, the final one being at 1034 over the Jeffersonville intersection. An approach was then started from that point to the Standiford Airport, 6-9/10 miles distant. During this approach the aircraft struck trees and crashed at a point one-half mile north of the Jeffersonville intersection. The airplane was destroyed and all eight occupants have been killed.

The aircraft crashed in unknown circumstances in Jeffersonville, some 3 km north of Louisville. There was at least one fatality, the captain John Nagel.