Training

The twin engine aircraft departed Moulins-Montbeugny Airport in the morning on a training flight to Clermont-Ferrand, carrying two passengers and two pilots. The goal of the flight was to extend the IFR rating of the pilot in the left seat. Following a stop in Clermont-Ferrand, the crew returned to Moulins. Over Moulins, the crew was cleared by ATC to leave the frequency and reported his intention to perform several manoeuvres in the area of Moulins Airport for a period of 30 minutes. Three touch-and-go were conducted on runway 26 then the crew continued at an altitude of about 2,000 feet when the aircraft became unstable on its roll axis. It nosed down and crashed in a wooded area called 'Bois de Bordes' located 7 km north of the airport, bursting into flames. The aircraft was totally destroyed and all four occupants were killed.

During a forced landing the left wing struck a light standard pole, and the airplane came to rest inverted after colliding with a fence. The purpose of the flight was to conduct recurrent training to include emergency procedures. On the accident flight the certified flight instructor (CFI) initiated a simulated engine failure after takeoff during the initial climb out. The student advised the tower, and turned crosswind at 700 feet agl. The student set up for landing, which included lowering the landing gear and adding 10 degrees of flaps. On short final, descending through 400 feet agl, both the CFI and student realized they would not make the runway. Both pilot's advanced the throttle, to arrest the descent and perform a go-around. There was no corresponding response from the engine. During the final stages of the emergency descent, the pilot maneuvered the airplane to avoid a work crew at the airport boundary fence and the airplane collided with the light standard pole and a fence. An airframe and engine examination discovered no discrepancies with any system. Following documentation of the engine and related systems it was removed and installed in an instrumented engine test cell for a functional test. The engine started without hesitation and was operated for 44 minutes at various factory new engine acceptance test points. During acceleration response tests, technicians rapidly advanced the throttle to the full open position, and the engine accelerated with no hesitation. A second acceleration response test produced the same results. According to Textron Lycoming, there were no discrepancies that would have precluded the engine from being capable of producing power.

The copilot inadvertently induced a lateral oscillation and lost control of the airplane while practicing touch-and-go landings. The pilot made the first touch-and-go. The copilot successfully made the second touch-and-go. The copilot attempted the third touch-and-go. At 50 feet, he disengaged the yaw damper and entered a pilot induced lateral oscillation. The airplane rapidly decelerated and developed a high sink rate. The airplane dragged the right tip fuel tank, which separated from the airplane, and the airplane bounced back into the air. The airplane landed hard, the main landing gear collapsed, and the airplane skidded to a stop off the right side of the runway. Both pilots and the passenger deplaned through the main entry door. The pilot-in-command had not demonstrated the handling characteristics of the airplane with the yaw damper off, and he felt he did not react quickly enough to prevent the accident.

After takeoff from Mendoza-El Plumerillo Airport, while climbing to a height of about 50 metres, the right engine lost power. The crew declared an emergency and initiated a left turn to return to the airport when control was lost. The aircraft stalled and crashed 300 metres past the runway end, bursting into flames. All five crew members were killed. They were completing a training flight to Paraná.

The flight crew stated that while making a missed approach after a practice instrument landing system approach, the right engine failed. The captain took control of the airplane from the copilot. The captain stated that while he performed the emergency procedures for engine failure, he noticed the left engine was not producing power. He then made a forced landing in water east of the airport. He stated that just before impact, he feathered the left propeller. The copilot stated he observed the captain activate the propeller feathering button for the left engine as he performed the emergency procedures for the right engine failure. The reason for failure of the right engine was not determined.

The crew was completing a local training flight at Surabaya-Juanda Airport, consisting of touch-and-go manoeuvres. While approaching the airport to complete the eighth landing, at an altitude of 500 feet, the aircraft rolled to the left then stalled and crashed in a pond located 3 km short of runway, bursting into flames. All three pilots were killed. Both captains were operating on Casa-Nurtanio CN-235 (IPTN) and making a transition to Fokker F27.

The instructor was accompanied by a trainee pilot and two passengers (also pilots) on a local training flight and was in the process of doing type conversion training when the accident happened. On the third circuit after a touch and go landing on runway 06L, the right-hand engine failed soon after take-off. The aircraft was flown at low altitude in a left-hand circuit in an attempt to land onto runway 17. During this circuit the left-hand engine also failed. The aircraft collided with, and severed, three 11kV electrical conductors and executed a forced landing with the gear retracted to the North of FALA approximately 1 km from threshold of runway 17. The pilot only sustained minor injuries with no one else injured. The initial on-site inspection revealed that both front tanks, which were selected at the fuel tank selector, were empty. The pilot who was undergoing conversion training refueled the aircraft prior to the accident and stated that 70 litres of fuel was uplifted into each "inboard auxiliary" tank and that what he presumed to be the "main" tanks were filled to capacity. The instructor stated that upon his arrival, the pilot who refueled the aircraft told him that he had filled the "mains" and that the "centre aux. tanks" were partially filled. The instructor further stated that the "main" tanks were selected for the duration of the flight. The aircraft is equipped with three fuel tanks in each wing. These tanks are: Front, Rear Auxiliary and Auxiliary tanks. Only one fuel quantity gauge is installed in the aircraft. A seven position selector knob above the fuel quantity gauge determines the tank to which the gauge is connected which then indicates the amount of fuel in that respective tank. The left and right front tanks were selected on the fuel gauge selector knob.

The crew was completing a local training flight at Morón AFB. In unknown circumstances, the aircraft crashed in the swimming pool of a private residence located in the district of Moreno, west of the airbase. Both pilots (Cpt Reyna and Lt Pesci) were killed while there were no injuries on the ground.

The crew (two pilots and one technician) departed Kayseri-Erkilet AFB on a local training flight. While flying at a relative low altitude, the twin engine aircraft entered an uncontrolled descent, dove into the ground and crashed near the Sarimsakli Dam, about 22 km northeast of Kayseri Airbase. The aircraft was totally destroyed and all three occupants were killed.

The twin engine aircraft departed Paris-Le Bourget Airport at 1309LT on a flight to Reims-Champagne with two pilots on board, one instructor and one pilot that should complete a transition program. While descending at an altitude of 2,000 to Reims-Prunay Airport, the crew informed ATC that he would perform an exercise consisting of a go-around procedure with the simulation of an engine failure. On a left downwind approach to runway 25, the crew started the exercise when the aircraft rolled to the left, lost height and crashed in an open field, bursting into flames. The wreckage was found 425 metres short of runway 25 and both pilots were killed.