On February 1, 2001, 0638 central standard time, a Beech BE-58 multi-engine airplane, N448DH, was substantially damaged during a precautionary landing to a soft muddy field near Brinkley, Arkansas. The airplane was registered to and operated by Market Aviation of Hot Springs, Arkansas. The instrument-rated private pilot, sole occupant of the airplane, received minor injuries. Visual meteorological conditions prevailed and an instrument flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight originated from Memphis International Airport (MEM), Memphis, Tennessee, at 0613, and was destined for Little Rock, Arkansas. Use your browsers 'back' function to return to synopsisReturn to Query Page
A review of the air traffic control data by the NTSB investigator-in-charge (IIC), revealed that at 0622:22, the pilot reported to the Memphis Air Route Traffic Control Center (ARTCC) controller that the airplane was level at 4,000 feet msl. At 0630:47, the pilot advised the controller of an overheat indication on a cylinder, and that he needed to land the airplane at the nearest airport. At 0631:08, the controller advised the pilot that Brinkley was at the 12 o'clock position, 9 miles. At 0631:58, the pilot stated "stuff going on here and have to trouble shoot." At 0632:45, the controller called the position of the airport as 12 o'clock, 5 miles. At 0632:50, the pilot transmitted that he was looking for the airport. At 0633:28, the controller advised the pilot to turn the airplane 15 degrees left and that the airport was at 10 o'clock, 3 miles. At 0633:28, the pilot reported that he was having a "control problem, airplane shaking, not sure got control, but it's intermittent." At 0634:21, the controller advised the airport was 1 1/2 miles south of the airplane. At 0644:44, the pilot stated that he was looking. At 0635:37, the pilot advised that he was not going to make the airport, losing altitude, and not able to control the airplane very well. At 0637:11, the pilot advised that he was going to land the airplane in a field. At 0723:14, another aircraft in the area picked up the emergency locator transmitter (ELT) signal and located the airplane in a field 4.9 nautical miles from the airport.
During a telephone interview conducted by the NTSB IIC, the pilot reported that prior to his flight, a local fixed based operator fueled the airplane with a total of 80 gallons of fuel. After the pilot's preflight of the airplane, he received a weather briefing, and filed an instrument flight plan direct to Little Rock. During cruise flight at 4,000 feet, the pilot set the propeller and throttle controls to 2,300 rpm and 23" of manifold pressure respectively, and the cylinder head temperature (CHT) gauge was indicating 180 degrees on each engine. Approximately 20 minutes into the flight, the pilot noticed the right engine CHT was rising above "350 degrees and the oil temperature [was rising] above the top of the green arc." (The airplane's CHT gauge maximum temperature (red line) is 238 degrees centigrade, and the gauge maximum indication is 250 degrees centigrade.) The pilot stated that he "shut down the engine, feathered the propeller, and cutoff the fuel." The pilot advised ARTCC that he needed to land the airplane at the nearest airport, and he received air traffic control vectors to the Frank Federer Memorial Airport (M36) near Brinkley, Arkansas. Approximately 6 miles from M36, the pilot stated the airplane began to "porpoise," and he was having trouble maintaining altitude and airspeed. Due to the lack of daylight, the pilot was unable to locate the airport, and he executed a precautionary landing to a muddy field. During the landing roll, the nose landing gear separated, and the right main landing gear collapsed. In addition, the pilot reported that the CHT ran high (out of the green arc) on the right engine while taxiing a few months prior to the accident.
On the NTSB Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot reported that he had accumulated 2,700 total hours in the accident aircraft make and model, and 3,500 multi-engine airplane hours.
On February 1, 2001, FAA inspectors, who responded to the accident site, reported the nose and right main landing gears separated from the airplane, the fuselage was wrinkled, and the propeller blades on both propellers were bent aft. The inspectors found the throttle levers in the "full" forward position, the right propeller lever in the "mid range" position, and the left propeller lever in the full aft (feather) position. The inspectors reported the flight and engine controls were manipulated and found to operate with no anomalies noted. The left and right propellers were not found in the feather position.
On February 2, 2001, an FAA inspector, an airframe manufacturer representative, and an engine manufacturer representative examined the aircraft and engines at the accident site. The 300-horsepower Teledyne Continental IO-550-C (31) engines were test run on the airplane in the field to 1,500 rpm, and a successful magneto check was performed. There were no anomalies noted with the engine test run. At the time of the accident, the airframe and engines had accumulated 110.0 hours.
On March 16, 2001, the CHT gauge (P/N 58-380104-5, S/N D201039) was examined by the airframe manufacturer, under the supervision of the FAA, and no anomalies were noted during the examination.
A mechanic at Dawson Aircraft, Clinton, Arkansas, was requested by the NTSB IIC, to perform a continuity check of the right engine CHT probe electrical wire #E13A20, which runs from the probe to the gauge. Continuity was confirmed on wire E13A20.
On March 20 and 21, 2001, the engines were examined under NTSB supervision at the Teledyne Continental Motors facility in Mobile, Alabama. The right engine (serial number 684402) was run in a test cell for 2 hours; at a takeoff power setting for 10 minutes, and at a cruise (75% HP) power setting for 1.5 hours. During the test run, rapid power changes were applied to the engine with no anomalies noted. The number 2 CHT (probe location for the cockpit indication) did not exceed it's maximum limits during the 2-hour test run, and the CHT remained consistent with the other 5 CHTs. The left engine (serial number 684410) was run in a test cell for 2 hours at the same power settings and duration as the right engine. The CHTs for the left engine were consistent with the CHTs from the right engine. There were no indications of an overheating cylinder on either engine, and no anomalies were noted during the examinations.
Toxicological testing on the pilot's blood and serum was performed at the FAA Civil Aeromedical Institute (CAMI) Forensic Toxicology and Accident Research Center in Oklahoma City, Oklahoma. The toxicological test indicated that 2.296 (ug/ml, ug/g) of nefazodone was detected in the serum. Nefazodone is a prescription antidepressant, often known by the trade name Serzone. According to medical information obtained under subpoena, from 2/11/00 to 9/22/01, the pilot was taking Serzone for depression, Xanax (alprazolam, a perscription tranquilizer) for anxiety, and Ambien (zolpidem, a perscription hypnotic medication) for insomnia. Between 2/11/00 and 1/30/01, prescriptions were filled for the pilot for alprazolam, Ambien, and Serzone. Medical records obtained from the FAA Civil Aeromedical Institute Aeromedical Certification Division revealed that the pilot did not report the use of the aforementioned drugs on his most recent medical application dated March 16, 2000. The FAA's 1999 Guide for Aviation Medical Examiners notes that "the use of a psychotropic drug is considered disqualifying. This includes all sedatives, tranquilizers, antipsychotic drugs, antidepressant drugs (including SSRI's), analeptics, anxiolytics, and hallucinogens."