Durango

While approaching Durango Airport on a flight from Celaya, the twin engine aircraft entered an uncontrolled descent and crashed in an open field located near the village of Ceballos, about 16 km northwest of the Durango Intl Airport. The burned wreckage was found near the Peña del Aguila Dam. Both occupants were killed.

Upon landing at Durango-Guadalupe Victoria Airport following an uneventful flight from San Luis Potosí, the twin engine aircraft went out of control and crashed in a grassy area, coming to rest upside down and bursting into flames. A pilot and two passengers were killed while four other occupants were injured.

En route from Durango to Acapulco, the twin engine airplane crashed in unknown circumstances in the Infiernillo River, in the region of Las Juntas. The wreckage was found inverted and partially submerged in water. All six occupants were killed.

The takeoff from Durango-Guadalupe Victoria Airport was initiated in poor weather conditions as a thunderstorm just passed over the airport five minutes prior to the accident. The takeoff from runway 03 was completed with a wind from 047° at 33 knots. Eight seconds after liftoff, the aircraft climbed to a height of 8 feet with a speed of 145 knots. At this time, the wind came from 103° at 11 knots. The aircraft continued to climb to 30 feet when the wind changed with a tailwind component of 22 knots from 030°. The aircraft started to descend and impacted ground, causing both engines to be torn off. The aircraft continued, overran and slid for 380 metres before coming to rest, bursting into flames. All 103 occupants were evacuated and 39 were injured, 14 seriously. The aircraft was totally destroyed by a post crash fire. At the time of the accident, weather conditions were poor with thunderstorm activity, heavy rain falls and strong winds. Notable variations in wind components were noticed at the time of the accident.

During the takeoff roll on runway 15 at Toluca-Licendiado Adolfo López Mateos, after the airplane passed the V1 speed, the warning light came on in the cockpit panel, informing the crew about the deployment of the reverse on the left engine. According to published procedures, the crew continued the takeoff and shortly after rotation, during initiale climb, the aircraft rolled to the left and crashed in an open field, bursting into flames. The wreckage was found about 200 metres past the runway end. The aircraft was destroyed and both pilots were killed.

The single engine airplane departed Tayoltita Airfield around 0900LT on a charter flight to Durango, carrying nine passengers and one pilot. Twelve minutes into the flight, the pilot encountered engine problems and declared an emergency. Unable to maintain a safe altitude, he attempted an emergency landing when the aircraft crashed in the bed of the Piaxtla River. The wreckage was found about 16 km northeast of Tayoltita Airfield (N 24° 11' 2.65" W 105° 47' 12.57''). The aircraft was destroyed by impact forces and there was no fire. Three passengers were killed and seven other occupants were injured.

Shortly after takeoff from runway 05L at Mexico City-Benito Juarez Airport, while in initial climb, the aircraft encountered windshear. It lost height and crash landed on the runway. Upon impact, the landing gear were torn off. Out of control, the aircraft veered off runway, lost its right wing and came to rest. All 56 occupants evacuated safely and the aircraft was destroyed.

During an instrument approach, upon descending to the prescribed minimum descent altitude, about 1/2 mile from the missed approach point, the pilot failed to maintain flying airspeed. The airplane stalled, rolled left, and in an uncontrolled descent collided with a commercial building 0.96 nm from the runway's displaced threshold. The accident occurred during the return portion of a round trip flight, while on final approach to the pilot's alternate airport due to a weather-induced diversion. Moderate intensity snow showers and freezing fog existed. During the initial approach, the reported visibility was 1 1/2 miles. About the time the pilot passed the final approach fix, the visibility decreased to 1/2 mile, but the pilot was not informed of the decrease below his 1-mile minimum requirement. The pilot had maintained the recommended 140-knot approach speed in the icing conditions until about 3 1/2 miles from the runway. Thereafter, the airplane's speed gradually decreased until reaching about 75 knots. After the airplane started vibrating, the pilot increased engine power, but his action was not timely enough to avert stalling. Company mechanics maintained the airplane. On previous occasions overheat conditions had occurred wherein the environmental ducting melted and heat was conducted to the adjacent pneumatic tube that provides deice air to the empennage boots. During the accident investigation, the deice tube was found completely melted closed, thus rendering all of the empennage deice boots dysfunctional.

The airplane was on a non-scheduled cargo flight which was projected to fly an approximate 240 degree course for 92 nm. The accident site was located on a heavily forested steep mountain side, 15 to 16 nm north of the airplane's projected course. The debris field began at an east-west ridge line, and progressed for 300 feet on a 010 degree track to the downed airplane. Examination of the airframe and engines revealed no evidence of preimpact discrepancies. The accident site was in an area where the Fall color of the aspens was at its peak. Additionally, it was an area where elk were sometimes observed.

On approach to Santa Maria de Otaez Airstrip, the crew encountered strong winds and turbulences when the aircraft went out of control and crashed on a hill located few km from the airfield. Three passengers were seriously injured while 16 other occupants were killed. About two weeks later, one of the survivor died from his injuries.