Government

The airplane was making a public use flight between two islands for the purpose of transporting residents of a correctional facility to court hearings. During descent to the destination airport, at an altitude of approximately 1,400 feet, both engines started surging. The pilot's attempts to restore normal engine power were unsuccessful, and he ditched the airplane in ocean water with both engines still surging. The airplane stayed afloat as he and the passengers exited, and then it sank. The airplane was not recovered from the ocean, precluding its examination and determination of the reason for the dual loss of engine power.

The aircraft departed Toluca Airport at 1516LT on a flight to Colima, carrying five members of the Colima Government and two pilots. Fifteen minutes into the flight, while cruising at an altitude of 16,000 feet, the crew informed ATC about control problems and was cleared to divert to Morelia Airport via radial 160. Shortly later, the aircraft entered an uncontrolled descent and crashed in a wooded and mountainous terrain located near El Devanador. The aircraft was totally destroyed and all seven occupants were killed.
Crew:
Mario Torres, pilot,
Germán Ascencio, copilot.
Passengers:
Gustavo Vázquez Montes, Governor of the State of Colima,
Roberto Preciado Cuevas, delegate secretary for Tourism,
Ignacio Peralta, delegate secretary for Economy,
Luis Barreda Cedillo, delegate secretary for Finances,
Guillermo Díaz, Director of Tourism.

On November 27, 2004, about 0820 Afghanistan time, a Construcciones Aeronauticas Sociedad Anonima C-212-CC (CASA 212) twin-engine, turboprop airplane, N960BW, registered to Aviation Worldwide Services, LLC, and operated by Presidential Airways, Inc., of Melbourne, Florida, collided with mountainous terrain in the vicinity of the Bamiyan Valley, near Bamiyan, Afghanistan. The Department of Defense (DoD) contract flight was operated under the provisions of 14 Code of Federal Regulations (CFR) Part 135, with a company flight plan filed. Daylight visual meteorological conditions (VMC) prevailed. The captain, the first officer, and the mechanic-certificated passenger, who were U.S. civilians employed by the operator, and the three military passengers, who were active-duty U.S. Army soldiers, received fatal injuries. The airplane was destroyed. The flight departed Bagram Air Base (OAIX), Bagram, Afghanistan, about 0738.

Following an uneventful flight from Tijuana, the aircraft landed too far down the runway 28 at Mexicali-General Rodolfo Sanchez Taboada Airport. Unable to stop within the remaining distance, it overran, rolled for about 750 metres, collided with an embankment and came to rest in a sandy area. All six occupants escaped uninjured while the aircraft was damaged beyond repair. The aircraft had the dual registration XC-PFN (civil) and PF-213 (military).

The single engine aircraft departed Ciudad Bolívar at 1016LT on a flight to Uonquén, State of Bolívar. En route, around 1100LT, the pilot reported flying at 11,500 feet in poor weather conditions. About 45 minutes later, while cruising at an altitude of 7,000 feet, the aircraft struck the slope of Mt Awakapa Tepuy located in the Chimanta Mountain Range. All seven occupants were killed, among them two church women.

On May 2, 2004, at 1600 central daylight time, a Twin Commander 840 twin turbo-prop airplane, Mexican registration XC-JEH, was destroyed following a loss of control following an encounter with weather while in cruise flight near Milpillas, State of Aguas Calientes, in the Republic of Mexico. The airline transport rated pilot, first officer and the 5 passengers on board were fatally injured. The public use flight originated from Ciudad Juarez, State of Chihuahua, approximately 1400, and was destined for the Mexico City International Airport, in Mexico City. Instrument meteorological conditions prevailed for the domestic cross-country flight for which an instrument flight rules (IFR) flight plan was filed.

The twin engine aircraft departed Skopje on an official flight to Mostar, carrying two pilots and seven passengers, among them Boris Trajkovski, President of the Republic of Macedonia. He was flying to Mostar with members of his government to take part to an economic conference. On approach by night and limited visibility due to marginal weather conditions, the aircraft struck the slope of a mountain located near Berkovići, about 32 km southeast of the airport. The aircraft was destroyed by impact forces and a post crash fire and all nine occupants were killed.

After landing at Badiraguato Airport, the twin engine aircraft went out of control and veered off runway. It collided with rocks, lost its tail and came to rest. All five occupants escaped uninjured while the aircraft was damaged beyond repair.

The twin engine aircraft was returning from Busia to Nairobi, carrying a delegation of the Kenyan Government who made a local visit in Busia following the national elections. Shortly after takeoff from runway 13/31 which is 3,281 feet long, the aircraft encountered difficulties to gain height. It struck power cables and crashed onto a house. Both pilots and a passenger, the Labour Minister Ahmed Mohamed Khalif were killed while nine other occupants were seriously injured. The aircraft was destroyed. There were no casualties on the ground.

The aircraft was cleared direct and to climb to 14,000 feet. During the climb out, the controller inquired several times as to the flights altitude. The pilot's response to the controllers queries were exactly 10,000 feet lower than what the controller was indicating on radar. Eventually the controller instructed the pilot to stop altitude squawk, which he did. During the last communication with the pilot, he reported that he was level at 14,000 feet. During the next approximately 45 minutes, the aircraft was observed proceeding generally in the direction of its destination. When the controller observed the flight track turn approximately 45 degrees to the right and headed generally northwest, he attempted to contact the pilot without a response. The tracking then turned about 90 degrees to the left for a few minutes, then turned 180 degrees to the right. The aircraft dropped from radar coverage shortly thereafter. On site investigation revealed that the aircraft broke-up in flight as the wreckage was scattered generally east-to-west over the mountainous terrain for approximately .3 nautical miles. Further investigation revealed that the right wing separated at the wing root in an upward direction. Separation points indicated features typical of overload. The right side horizontal stabilizer separated upward and aft. The left side horizontal stabilizer remained attached however, it was twisted down and aft. The aft fuselage was twisted to the left. Both engines separated in flight from the wings. Post-crash examinations of the airframe and engines did not reveal evidence of a mechanical failure or malfunction. Both altimeters were too badly damaged to test. Autopsy and toxicology results indicated that the pilot had severe coronary artery disease with greater than 95% narrowing of the left anterior descending coronary artery by atherosclerotic plaque. The coroner also reported that superimposed upon this severe narrowing was complete occlusion of the lumen by brown thrombus. Toxicology results indicated a moderate level of diabetes. The pilot's actions leading up to the accident were consistent with an incapacitation due to hypoxia. The role of a possible heart attack was unclear, since it is possible that it occurred as a result of the hypoxia.