Airport (less than 10 km from airport)

On May 16, 2005 about 1230EST (1845Z), a Britten Norman Islander aircraft, registration C6-ASA crashed approximately 3nm northeast of the Moss Town International Airport. The Pilot reported, “about 35 minutes south of Nassau International Airport [MYNN] I noticed that my ground speed was very low. I continued with my flight to MYEF because I should have had 1 hour and 30 minutes of fuel. About 10 miles from MYEF my right engine quit then 2 minutes later my left engine quit. I then look a suitable place to land three miles from the airport.” The one (1) pilot and two (2) passengers received no serious injuries. The aircraft was destroyed from impact sustained as it contacted the trees. The accident flight originated from Freeport, Grand Bahama, Bahamas to Moss Town, Exuma, Bahamas with an intermediate stop in South Bimini, Bahamas. Visual Flight Rules Conditions existed at the time of the accident. The aircraft was operated by Flamingo Air Limited, a Bahamian Air Operator Certificate holder. Flamingo Air Limited operated as a Commuter, Unscheduled / On Demand Operator in commercial air transport. Flamingo Air Limited operated under the provision of the Bahamas Aviation Safety Regulations (BASR 2001). Its aircraft are maintained under the provision of Bahamas Aviation Safety Regulations (BASR 2001). The aircraft had flown a total of 2 flights including the accident flight. The pilot flew both flights [the same pilot later flew the accident flight]. The pilot reported no problems with the aircraft prior to the accident. There were no open MEL items. There were no open (uncorrected) mechanical irregularities written in the Technical and Journey Log. On May 15, 2005 the pilot uplifted a total of 130 gallons of fuel, which is the maximum capacity for this aircraft. Prior to the accident flight, the aircraft completed two flights, MYAM to MYGF [flown on May 15, 2005] which lasted 45 minutes and MYGF to MYBS [flown on May 16, 2005] which lasted 30 minutes. No fuel was uplifted prior to the next flight which was MYBS to MYEF, the accident flight [flown on May 16, 2005]. During post accident interviews, the pilot confirmed that he had not noticed anything unusual about the airplane. The pilot later surmised that he had simply run out of fuel.

The DC-9 was taxiing to the gate area when it collided with a company A319 that was being pushed back from the gate. Prior to arriving at the destination airport, the DC-9 experienced a loss of hydraulic fluid from a fractured rudder shutoff valve located in the DC-9's right side hydraulic system. The left side hydraulic system had normal hydraulic pressure and quantity throughout the flight. The flightcrew elected to continue to the scheduled destination and declared an emergency while on approach to the destination airport. After landing, the emergency was negated by the flight crew and the airplane taxied to the gate. Flight data recorder information indicates the left engine, which provides power for the left hydraulic system, was shut down during taxi. The captain stated he did not remember shutting the left engine down, and that if he had, it would have been after clearing all runways. The first officer stated that he was unaware that the left engine was shut down. Upon arrival at the gate with the left engine shut down and no hydraulic pressure from the left system and a failure of the right hydraulic system, the airplane experienced a loss of steering and a loss of brakes. The flightcrew requested company maintenance to chock the airplane since they were unable to use brakes to stop the airplane. The crew said they were going to keep the "...engines running in case we have to use reversers..." The airplane began to roll forward and the captain applied reverse thrust but the reversers did not deploy. The airplane impacted the A319 with a speed of approximately 15.65 miles per hour to 16.34 miles per hour. Evacuation of the DC-9 was completed approximately 5:22 minutes after the collision and evacuation of the A319 occurred approximately 13:08 minutes after the collision. Examination of the left hydraulic system revealed no anomalies and examination of the right hydraulic system revealed a fractured rudder shutoff valve that displayed features consistent with fatigue. Following the accident, the airplane manufacturer issued a service letter pertaining to the replacement of the rudder shutoff valve based upon reliability information that was reported to them. The number of reports was greater than that of the Federal Aviation Administration's Service Difficulty Reports database, and less than the operators records.

erimeter Aviation flight 914, a Metro II with 17 people on board, was on approach at Thompson, MB. The first officer flew the aircraft during the approach, and encountered turbulence and fluctuating airspeed. The captain took control at 200 feet agl. The aircraft was high and left of centreline. The captain added power, continued the approach and landed hard on runway 23 near the intersection with runway 32. After the aircraft arrived at the apron, a fuel leak was noted. The aircraft was inspected and damage was found in the wheel wells, wing leading edge, engine mounts and a wing-fuselage attachment point. No injuries were reported. Reported winds at 1400Z were 010 at 15-20 kts; 1500Z winds were 350 at 9 kts.

The twin engine aircraft was completing a charter flight from San Juan to Córdoba with seven passengers and two pilots on board. On approach to Córdoba-Ambrosio Taravella Airport by night, the crew encountered limited visibility due to poor weather conditions. The aircraft descended below the glide and collided with the inner marker antenna located about 700 metres short of runway 18 and crashed. Both pilots and four passengers were killed while three other passengers were seriously injured. Among those killed were the Argentinian racer Nicolas Vuyovich and Gustavo Ramonda, Director of the Toyota Corolla Racing Team who just won a race at the San Juan's autodrome.

Shortly after takeoff from Barradas Airport located near Tanauan (Batangas), while in initial climb, the aircraft suffered an engine failure. It stalled and crashed in a coconut grove located in the village of Santor, near the airfield. The pilot and three passengers were killed while two others were seriously injured. All occupants were completing a local skydiving mission. Witnesses reported that the engine emitted white smoke shortly after rotation.

The passenger flying the airplane made a hard landing after the pilot had experienced an incapacitating cardiac event. Shortly after takeoff the pilot turned the plane around to return to the departure airport. He started coughing and then went unconscious. The passenger in the right seat, who had no piloting experience, took control of the airplane and made several landing attempts. During the fourth landing attempt he stalled the airplane at a low altitude. The airplane impacted terrain, landing flat on its belly a few hundred feet short of the runway. The autopsy report attributed the pilot's cause of death to arteriosclerotic cardiovascular disease.

Widerøe flight WIF 921 took off from Tromsø airport (ENTC) at time 1401 with an estimated landing time at Hammerfest airport (ENHF) 1442. On board the aircraft, a DHC-8-103 with registration LN-WIK, were a crew of two pilots and one cabin attendant, 26 fare paying passengers and one passive cabin attendant. The crew had taken off from ENHF earlier in the day, when the weather and wind did not cause any problems. During the approach to ENHF the crew was informed about variable and occasional gusty wind from south-east. The wind direction favoured runway 23 and the crew planned the landing accordingly. The copilot was Pilot Flying (PF) and the commander was Pilot Not Flying (PNF). The copilot was newly hired and was flying under supervision. The crew was kept updated on the wind conditions by the AFIS operator, and at times the gusty wind conditions favoured runway 05. The copilot left the control to the commander who continued the approach to runway 05. Just before landing the wind direction veered to the right and increased in strength, resulting in a significant tail wind component. This resulted in a marked increase in the descent rate which the commander tried to stop by advancing to full power. However, the altitude was too low and the airplane touched down hard just inside the runway edge on runway 05. At touch down the right main landing gear leg failed. The airplane slid on the belly, right partly retracted main wheel and wing tip for some 650 m, and stopped just after the second (TWY B) turnoff to the apron. The fire and rescue vehicles were quickly at the scene and sprayed foam on the plane to prevent fire. The cabin attendant calmed the passengers who wanted to get out of the plane quickly due to smoke and burned smell in the cabin. It took 33 seconds from the commander ordered evacuation until this was initiated. The delay was mainly caused by the fact that the order did not get through the cabin’s Public Address (PA) system.

While executing an instrument approach to land on runway 25, the airplane collided with the runway, and collapsed the right main landing gear. The airplane subsequently burst into flames after the pilot and passenger exited the airplane. Post-accident examination of the engines found both the left and right engine fuel controls in a low power setting. Examination of the propeller control found both propellers at 30-degrees. The pilot did not report any flight control or mechanical problems during flight.

After landing at Kabul Airport, following an uneventful cargo flight from Dubai, the aircraft became uncontrollable. It veered off runway to the left and came to rest. A small fire erupted near the undercarriage and was quickly extinguished. All six crew members were rescued but slightly injured. The aircraft was damaged beyond repair.

The single engine aircraft was engaged in a crop spraying flight in the Sennoi area. During the takeoff roll, the left wheel separated. The aircraft went out of control, veered off runway to the left and collided with a parked truck, bursting into flames. Both pilots were injured, the captain seriously. The aircraft was destroyed by fire.