Orlando-Executive (Herndon)

Following an uneventful personal flight, the pilot contacted the air traffic control tower controller and was immediately cleared to land. About 36 seconds later, the pilot reported "smoke in the cockpit." When asked to repeat, the pilot repeated "smoke in the cockpit." The tower controller cleared the pilot to land on any runway. About 47 seconds after the initial call of smoke, the pilot reported "mayday mayday mayday mayday mayday (unintelligible)." The airplane then crashed about ¼ mile short of the airport in a wooded area and burned. Security video showed the airplane pitch nose-down suddenly just before impact. The video revealed no visible smoke or fire trailing the airplane before ground impact. The pilot reported about 1,221 hours of total flight time on his Federal Aviation Administration first class medical certificate, issued about two months prior to the accident. He completed an initial training course for the airplane make and model 1 week before the accident. The airplane had recently undergone an annual inspection and extensive upgrades to its avionics. Both the left and right engines displayed contact signatures to their internal components characteristic of engines developing significant power at the time of impact, likely in the mid-to-high power range. The engines displayed no indications of any pre-impact anomalies or distress that would have precluded normal engine operation. Both propeller assemblies broke free from the engine during the crash sequence and the blades on both engines revealed signatures consistent with the development of power at impact. The center fuselage and cockpit areas were completely consumed in the postcrash fire. An examination of all remaining wires, wire bundles, switches, terminals, circuit breakers, electrical components, instruments, and avionics did not reveal evidence of precrash thermal distress. However, a small fire just before impact likely would not have had time to create thermal damage that would be discernable after an extensive postcrash fire.

Cargo was not weighed and weight and balance calculations were not performed. The airplane was about 321 pounds over gross. While taxiing, a witness reported seeing black smoke trailing the left engine which had been worked on the night before the accident. Two cylinders were worked on and a fuel injector nozzle was cleaned. The climb after takeoff was 'low and slow' during which the airplane rolled left, pitched nose down, and impacted the ground coming to rest adjacent to a house. Examination of each engine revealed no evidence of internal mechanical failure or malfunction. Heat damage precluded testing of the magnetos, turbocharger components, and fuel servos of each engine. Examination of each propeller revealed no evidence of preimpact failure or malfunction. The fuel nozzles from the left engine were examined which revealed that they were blocked in various places due to contaminants. After the accident the faa performed a focused inspection of the operator revealing that the cargo was not being weighed, the chief pilot of the company was in name only, and load manifests were not being kept by the company. The pilot, sole on board, was killed.

During arrival, the flight was issued the current Paducah altimeter setting. The pilot requested vectors for an approach to runway 18, but the ARTCC controller (ctlr) could not accommodate the request. The pilot was cleared for a VOR/DME-a approach. MDA for the approach was 1,080 feet msl (600 feet agl). At 2108 cdt, the flight changed to the FBO frequency. FBO personnel observed the aircraft fly over the airport and advised that it was too low. One of the pilots replied that they would be 'staying under the clouds.' The pilots had planned to land on runway 36, but reported they lost sight of the runway and would change to runway 18. Subsequently, the aircraft collided with a tree about 1 mile north-northeast of the airport, while on a westerly heading (approximately position of base leg for a VFR pattern). The aircraft came to rest about 700 feet west of the tree and was destroyed by impact and fire. No preimpact part failure/malfunction of the aircraft was found. Approximately 30 miles west at Paducah, the weather was in part: 200 feet scattered, 900 feet overcast visibility 3 miles with rain and fog, wind from 360° at 7 knots. The airport manager estimated there was a 200 feet ceiling at the airport. All six occupants were killed.

Following a night takeoff from Orlando-Herndon Airport, while climbing in adverse weather conditions, the pilot lost control of the airplane that crashed. All four occupants were killed.

After takeoff from Orlando-Herndon Airport, the twin engine airplane encountered serious difficulties to gain height. It went out of control and crashed in flames in a field. All three occupants were injured, one of them seriously.

On a leg from Jacksonville to Miami, the crew encountered technical problems and decided to divert to Orlando-Herndon Airport. While on a night approach, the airplane became uncontrollable and crashed onto a house located short of runway threshold. The aircraft was destroyed and all three occupants were killed while no one on the ground was injured.