Rockwell Grand Commander 690

The twin engine aircraft departed Maracaibo Airport on a charter flight to Panama City with three passengers and one pilot on board. While cruising over the Sierra de Perija between Venezuela and Colombia, the pilot informed ATC about technical problems. Shortly later, the aircraft entered an uncontrolled descent and crashed in a mountainous terrain near Valledupar, bursting into flames. All four occupants were killed.

Approximately 37 minutes after departing on a 928-nautical mile cross-country flight under instrument flight rules, the twin-engine turboprop airplane experienced an in-flight break-up after encountering moderate turbulence while in cruise flight at the assigned altitude of FL230. In the moments preceding the break-up, the airplane had been flying approximately 15 to 20 knots above the placarded maximum airspeed for operations in moderate turbulence. The airplane was found to be approximately 1,038 pounds over the maximum takeoff weight listed in the airplane's type certificate data sheet (TCDS). The last radar returns indicated that the airplane performed a 180-degree left turn while descending at a rate of approximately 13,500 feet per minute. There were no reported eyewitnesses to the accident. The wreckage was located the next day in densely wooded terrain. The wreckage was scattered over an area approximately three miles long by one mile wide. An examination of the airframe revealed that the airplane's design limits had been exceeded, and that the examined fractures were due to overload failure.

The crew of the missing airplane was conducting a local area familiarization flight under Title 14, CFR Part 91. At the time of the flight, visual meteorological conditions prevailed, with occasional moderate turbulence forecast for the area. The airplane was routinely contracted for animal and bird counts, and the flight was to include low level flight simulating such a mission. The three occupants of the airplane were the pilot, company check pilot, and another company pilot riding along as a passenger. Both the pilot and the check pilot held airline transport certificates, and were experienced in the make and model of the accident airplane. The airplane was equipped with a satellite position reporting device that updated position, groundspeed, and altitude every 2 minutes. Radar and GPS track information indicated the accident airplane was flying low and slow along a peninsula coast over a saltwater inlet, and turned toward the center of the inlet. The track stopped about 3 miles offshore. The data indicated that while flying along the inlet, the airplane descended to 112 feet above ground level (water), and climbed as high as 495 feet, which was the airplane's altitude at the last data point. The airplane's groundspeed varied between 97 and 111 knots. The area of the presumed crash site experiences extreme tides and strong currents, with reduced visibility due to a high glacial silt content. An extensive search was conducted, but the airplane and its occupants have not been located. An examination of the airplane's maintenance logs did not disclose any unresolved maintenance issues.

Crashed near Villa el Carmen following apparent technical problems while completing a smuggling flight.

The twin engine aircraft was completing an illegal flight from Colombia to the US with three people on board. While flying at low height, it collided with trees and crashed in a wooded and hilly terrain near El Gallito. The aircraft was destroyed and all three occupants were killed. On scene were found one ton of cocaine in several boxes, large sums of money and guns. The registration N572L was probably a false one.

The twin engine aircraft stalled on approach to Courchevel Airport and touched down hard, causing substantial damage to the fuselage. There were no injuries but the aircraft was damaged beyond repair.

The pilot executed the VOR approach to runway 21. He was heard to report passing the VORTAC outbound for the procedure turn, and crossing the VORTAC (final approach fix) inbound. Witnesses said they saw the airplane emerge from the overcast slightly high and fast. They said the airplane entered a steep left bank and turned about 90 degrees before disappearing in a snow shower northeast of the airport. They heard no unusual engine noises. Another witness near the accident site saw the airplane in a steep bank and at low altitude, "just above the power lines." Based on the witness location, the airplane had turned about 270 degrees. The witness said the wings "wobbled" and the nose "dipped," then the left wing dropped and the airplane descended to the ground "almost vertically." Members of the County Sheriff's Posse, who were at a gunnery range just north of the airport, reported hearing an airplane pass over at low altitude. One posse member said he heard "an engine pitch change." He did not see the airplane because it was "snowing heavily," nor did he hear the impact. An examination of the airplane revealed no anomalies. At the time of the accident, the weather at the destination airport was few clouds 300 feet, 900 feet broken, 3,200 feet overcast; visibility, 1/2 statute and snow; temperature, 32 degrees F.; dew point, 32 degrees F.; wind, 290 degrees at 10 knots, gusting to 15 knots; altimeter, 29.71 inches.

On September 16, 2003, at 1430 central daylight time, an Aero Commander 690 twin-engine airplane, N302WB was destroyed upon impact with trees and terrain while attempting a takeoff from an airstrip near Soto La Marina, in the State of Tamaulipas, in the Republic of Mexico. The commercial pilot, sole occupant of the airplane, was fatally injured. The airplane was registered to the QEAT-4 LLC., in Naples, Florida, and was being operated by the MGS Corporation of Laredo, Texas. Visual meteorological conditions prevailed for the business flight for which no flight plan was filed. The flight's destination was reported to be Laredo, Texas. Local authorities reported that the turboprop powered airplane, serial number 11003, had previously sustained some damage to the nose landing gear and the owner had replaced the nose landing gear prior to attempting to depart from the airstrip.

The flight was in cruise flight at 27,000 feet when the airplane encountered unforecasted severe turbulence. The pilot made a "mayday" on the airplane radio to Jacksonville Center. Within several seconds the airplane accelerated from 175 knots through 300 knots ground speed and descended from 27,000 feet to 16,500 feet. The airplane disappeared from radar coverage and was located by Sheriff Department personnel 15 miles north of Homerville, Georgia, in a swampy area. Airframe components recovered from the accident site were submitted to the NTSB Materials laboratory for examination. The examinations revealed all failures were due to overload. Examination of the airframe revealed that the airframe design limits were exceeded. The pilot did not obtain a weather briefing before the flight departed.

The pilot entered the left-hand traffic pattern at an uncontrolled airport on a dark moonless night. Witnesses reported observing the airplane in a left descending turn. As the airplane turned onto the base leg, its left bank angle suddenly became steep. The airplane rapidly descended until colliding with level desert terrain 1.63 nm from runway 30's threshold. There were no ground reference lights in the accident site area. An examination of the airplane structure, control systems, engines, and propellers did not reveal any evidence of preimpact malfunctions or failures. Signatures consistent with engine power were found in both the engines and the propellers. The wreckage examination revealed that the airplane descended into the terrain in a left wing and nose low attitude. Fragmentation evidence, consisting of the left navigation light lens and left propeller spinner, was found near the initial point of impact. The wreckage was found principally distributed along a 307- to 310-degree bearing, over a 617- foot-long path. The bearing between the initial point of impact and the runway threshold was 319 degrees. The pilot's total logged experience in the accident airplane was 52 hours, of which only 1.6 hours were at night. The pilot was familiar with the area, but he had made only two nighttime landings within the preceding 90 days. Review of the recorded ATC communications tapes did not reveal any evidence of pilot impairment during voice communications with the pilot.