Charter/Taxi (Non Scheduled Revenue Flight)

The aircraft departed Goma on a charter flight to Kongolo with an intermediate stop in Kindu, carrying 22 passengers and five crew members for the Maniema Union Company. About 30 minutes into the flight, the aircraft crashed in a mountainous terrain. The wreckage was found the following day some 10 km from Biega. All 27 occupants were killed.

Witnesses observed the aircraft perform a rolling takeoff and it was airborne by the crossing runway (1,300 feet down the 6,600 foot runway). The aircraft entered an approximate 40 degree nose high climb rate to about 1,000 feet. The aircraft then entered a steep left hand banking turn. The nose dropped and the aircraft rotated up to about 4 times before colliding with the flat terrain adjacent to the departure end of the runway threshold. On site documentation of the airframe found no evidence of a flight control malfunction. An engine examination and teardown found that the gearbox section of the left engine experienced a high cycle fatigue failure of the high speed pinion journal bearing oil supply tube and subsequent degradation of the high speed pinion journal bearings. This failure resulted in a partial power loss to the left engine. The pilot had recently purchased this aircraft and he had accumulated approximately 11 hours since the purchase. The pilot had stated to personnel at the place where he purchased the aircraft that he had not received, nor did he need recurrent training in this aircraft as he had several thousand hours in the aircraft. Flight logs provided by the family indicated that the pilot had accumulated about 551 hours in a Mitsubishi, however, the last time that the pilot had flown this make and model was 14 years prior to the accident. Logbook entries indicated that only a few hours of flight time had been accumulated in all aircraft during the approximately 2 years prior to the accident. Personnel that flew with the pilot in the make and model aircraft involved in the accident described the pilot as "proficiency lacking." Normal takeoff calculations for the aircraft with the flaps configured to 5 degrees, indicated a ground run of 2,900 feet, with a rotation speed of 106 KCAS, and 125 KCAS for the climb out. A maximum pitch attitude of 13 degrees maximum is indicated. Performance calculations indicated that the aircraft was capable of lifting off where the witnesses observed and climbing to 1,000 feet agl by the end of the runway. To achieve this performance the aircraft would have rotated at approximately 84 KCAS and climbed at an airspeed below Vmc (100 KCAS) and close to power-off stall speed (86 KCAS) with 5 degrees of flaps. The airplane's flight manual indicated that if an engine failure occurs in the takeoff climb and the landing gear is fully retracted, the emergency procedures is to maintain 140 KCAS, flaps to 5 degrees, the failed engine condition lever to EMERGENCY STOP, and failed engine power lever to TAKEOFF. On site documentation found the left side condition lever in the takeoff/land position and the power lever was found half-way between takeoff and flight idle.

Aircraft lost power on both engines while on approach to Moscow-Vnukovo airport. The crew decided to divert to Sheremetievo Airport when the undercarriage collapsed on landing. The aircraft veered off runway and slid in a grassy area before coming to rest. Nobody was injured but the aircraft was damaged beyond repair.

The twin engine aircraft was completing a charter flight from Coyhaique to Chile Chico with an intermediate stop in Balmaceda where six additional passengers boarded. The airplane departed Balmaceda Airport runway 27 at 1310LT for the second leg to Chile Chico. About 16 minutes into the flight, while cruising in marginal weather conditions, radar contact was lost after the airplane crashed in an uninhabited area. The wreckage was found in the late afternoon in Meseta del Guenguel. The aircraft was totally destroyed and all 10 occupants were killed.

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 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.

The aircraft was completing a charter flight from Ufa to Naryan Mar with intermediate stops in Perm, Usinsk and Varandey under contract of Naryanmarneftyegaz, a sister company of Lukoil. On final approach under VFR mode in good weather conditions, at a speed of 170 km/h, the aircraft stalled, causing the left wing to struck a sand dune (3 metres high). The aircraft crashed 4,217 metres short of runway, bursting into flames. The captain, the navigator and 26 passengers were killed while 24 other people were injured. The aircraft was totally destroyed by impact forces and a post crash fire. OAT was -24° C. at the time of the accident and the visibility was good.

The pilot failed to lower the landing gear prior to touching down on the runway. The pilot said that during the approach into the airport, the flaps would not lock into the 20-degree extended position. The pilot decided to execute a no-flap landing and referred to the emergency checklist. The checklist advised the pilot to extend the landing gear; however, the pilot skimmed over the information thinking that the gear was already down and locked, and focused on the stabilized approach into the airport. The airplane touched down with the gear in the retracted position. No mechanical malfunctions were noted with the landing gear system on the airplane and a ground test run of the flaps did not reproduce the failure encountered during flight.

The single engine aircraft departed Campbell River on a night flight to Knight's Inlet with four passengers and one pilot on board. As it failed to arrive at destination, SAR operations were initiated by RCAF & RCMP but no trace of the airplane and its occupants was found. On 15 of July 2005, the wreckage was found at a depth of 260 metres of Quadra Island by the families of the victims. TSB did not proceed to any investigations for this occurrence.

The non-Spanish speaking commercial pilot was preparing for a Title 14, CFR Part 135 on-demand charter flight in a twin-engine airplane with gasoline engines. A non-English speaking fuel truck operator inadvertently serviced the accident airplane with 120 gallons of Jet-A turbine fuel. In the pilot's written statement he reported that just after takeoff, with six passengers aboard, both engines began to lose power, and the airplane subsequently descended and collided with tree-covered terrain at the departure end of the runway. An on-site examination of the fuel vender's Jet-A fuel truck disclosed that the dispensing nozzle installed on the truck was the same nozzle as a typical gasoline nozzle. An examination of the accident airplane's fuel caps and fueling ports disclosed that the accident airplane was equipped with round, fuel tank inlet restrictors, that would prevent fueling from a jet fuel nozzle of the appropriate size, but the fueling ports were not placarded with the required statement indicating that only gasoline (av-gas) should be used.