Beechcraft 200 Super King Air

En route from Chagual to Lima, at a distance of of 25 miles from Lima-Callao-Jorge Chávez Airport, the fuel pressure dropped and the left engine stopped. The crew continued the descent to Lima when, on final, the right engine failed as well. Both propellers were feathered and the crew attempted an emergency landing in an open field. The aircraft came to rest 3,5 km from the runway threshold. All 12 occupants escaped uninjured while the aircraft was damaged beyond repair.

While attempting to depart from the 3,500-foot long grass airstrip with a 14 knot quartering tailwind, the 5,800-hour pilot reported that at an airspeed of approximately 95 knots, "the airplane yawed left and rolled left abruptly as the aircraft came off the ground briefly." The airplane settled back onto the ground, before again climbing back into the air approximately 20 degrees left of the runway heading. Subsequently, the airplane’s landing gear struck tree tops before it impacted the ground. A passenger added that he "noticed the flaps were up during takeoff." Approximately three minutes after the accident, a weather reporting station located 5.6 nautical miles southwest of the accident site reported wind from 010 degrees at 14 knots. Examination of the engines revealed rotational scoring throughout the first and second stage turbines. No mechanical anomalies were observed.

The 2,100-hour instrument-rated private pilot stated that prior to departure for a 507 nautical mile cross-country flight, the fuel gauges indicated approximately 800 pounds of fuel on each side for a total of 1600 pounds; however, he did not visually check the amount of fuel that the tanks contained. During his approach to the destination airport, the right engine started to "sputter" before it finally quit. The pilot then "looked over at the fuel gauges and both tanks were showing empty." The left engine quit just a few moments later. The auto ignition installed in the airplane attempted to restart the engines. The engines restarted momentarily and then shut-off once more. The pilot declared an emergency and executed a forced landing onto a street below. After a hard landing onto the street, the right wing hit a telephone pole, and the left wing then hit several tree limbs before the airplane impacted a hill and came to a stop. The Federal Aviation Administration (FAA) inspector, who responded to the accident site, found the fuel transfer switch in the "right-crossfeed" position. The fuel system was examined and no leaks or anomalies were found. Approximately three-quarters of a gallon of unusable fuel was found in the right engine nacelle. Approximately four gallons (28 pounds) of usable fuel was found in the left engine nacelle.

On October 24, 2004, about 1235 eastern daylight time (all times in this brief are eastern daylight time based on a 24-hour clock), a Beech King Air 200, N501RH, operated by Hendrick Motorsports, Inc., crashed into mountainous terrain in Stuart, Virginia, during a missed approach to Martinsville/Blue Ridge Airport (MTV), Martinsville, Virginia. The flight was transporting Hendrick Motorsports employees and others to an automobile race in Martinsville, Virginia. The two flight crewmembers and eight passengers were killed, and the airplane was destroyed by impact forces and post crash fire. The flight was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 91 on an instrument flight rules (IFR) flight plan. Instrument meteorological conditions (IMC) prevailed at the time of the accident.