Beechcraft 80 Queen Air

Aviation Technology Innovators

On December 10, 2011, BE-65-80QA (Queen Air) with Registry RP-C824 took off from RWY 13, Manila Domestic Airport on/or about 0610 UTC (1410H) southbound for San Jose, Mindoro. There were three (3) persons on board, the PIC and two (2) other persons; one was seated at the right-hand cockpit seat and the other one at the passenger seat. After airborne, the ATC gave instructions to the pilot o turn right and report five (5) miles out. After performing the right turn, the pilot requested for a reland which was duly acknowledged but the ATC with instructions to cross behind traffic on short final Rwy 06 (a perpendicular international runway) and to confirm if experiencing difficulty. However, there was no more response from the pilot. From a level flight southward at about 200 feet AGL, three (3) loud sputtering/burst sounds coming from the aircraft were heard (by people on the ground) then the aircraft was observed making a left turn that progressed into a steep bank and roll-over on a dive. After about one complete roll on a dive the aircraft hit ground at point of impact (Coordinates 14.48848 N 121.025811 E), a confined area beside a creek surrounded by shaties where several people were in a huddle. Upon impact, the aircraft exploded and fire immediately spread to surrounding shanties and a nearby elementary school building. The aircraft was almost burned into ashes and several shanties were severely burned by post-crash fire. A total of thirteen (13) persons were fatality injured composed of: the 3 aircraft occupants who died due to non survivable impact and charred by post-crash fire, and ten (10) other persons on the ground, all residents at vicinity of impact point, incurred non-fatal injuries and were rushed to a nearby hospital for medical treatment. About 20 houses near the impact point were completely burnt and the adjacent Elementary School building was severely affected by fire.

Transportes Aéreos Don Carlos

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.

Aero Condor - Servicio de Transporte Aéreo Turistico - STAT

The twin engine aircraft crashed in unknown circumstances in the region of Maracaibo while completing a flight from Maracaibo to Boa Vista. No trace of the crew was found and it is believed that the flight was illegal.

Cotercon Comercial

Shortly after takeoff from Belo Horizonte-Pampulha Airport, while in initial climb, the left engine failed. The pilot lost control of the aircraft that rolled to the left, lost height and crashed onto four houses located in the district of São Bernardo near the airport. The aircraft and four houses were destroyed. All three occupants were killed and two other people on the ground were injured.

Private Spanish

Shortly after takeoff from Valdepeñas Airport runway 08, while in initial climb, both engines lost power. The pilot elected to make an emergency landing when the aircraft crashed in an open field located 3 km from the airfield. Both occupants escaped uninjured while the aircraft was damaged beyond repair.

Two Engines and a Prayer

After a 4.7 hour flight, while turning onto final, the airplane landed short. The pilot did not mention engine problems during a police interview. He subsequently told an FAA Inspector that the left engine failed, then later, that the right engine failed. He told the Safety Board that both engines failed. Adequate fuel was confirmed. The previous day, the right engine failed approaching another airport. The pilot performed a single-engine go-around, with landing gear and flaps down. He refused assistance and performed his own maintenance. He cleaned the fuel filters of both engines. During a ground runup, the right engine was hard to start, and required a high fuel flow to remain running. After the pilot re-cleaned the right fuel filter the engine ran fine. The flight was uneventful until the accident. Post-flight examination revealed all propeller blades bent back 90 degrees, with significant chordwise scoring on one blade per engine. The left engine fuel filter was relatively clean, with some brown residue which contained ferrous material. The right engine fuel filter was heavily coated with a white residue which contained aluminum, and brown material which contained ferrous material. The pilot received his multi-engine rating on April 22, 1998.

Viproca

At 1759LT, while descending to Caracas-Maiquetía-Simón Bolívar Airport by night, the pilot informed ATC about an engine failure. Six minutes later, the aircraft crashed in the sea about 22 km north of the airport. A passenger was rescued at 2205LT. The following night, two dead bodies were found while seven other occupants were never found. The aircraft sank and was lost. Crew: Ricardo Batija. † Passengers: Francesco Porco, Fernando Guasamucare, † Ileana González, † Víctor Ruiz, † Yelitza Arenas, † Juan Cabezas, † Ledda Martínez, † Edwin Núñez, † Paola de Guasamucare. †

Falcon Airlines

The aircraft was engaged on a charter flight for the BHP Cannington mine, and departed from Townsville at 0630 EST. The flight was uneventful and the aircraft landed at Cannington at 0840. The aircraft was refuelled and at about 0945 seven passengers and baggage were loaded. The aircraft was started and taxied for runway 36. During this time the necessary checks were completed. The takeoff was commenced, and after the aircraft became airborne and was accelerating with a positive rate of climb, the landing gear was selected up. While the gear was still in transit, there was a sudden power loss from the left engine. The pilot described a simultaneous height loss, roll, pitch, and yaw accompanied by a sound similar to a buzz saw from the left engine. The pilot immediately recognised that the left engine had failed and attempted to maintain speed and directional control. Power was reduced on the right engine to maintain directional control, and it was the pilot's intention to land the aircraft with gear retracted beyond the end of the runway. However, the left wingtip struck a steel fence post, and this spun the aircraft to the left. The aircraft struck a low earth bank while travelling sideways and rearwards. When the aircraft came to rest, all windows were obscured and the pilot believed the aircraft was on fire. The pilot tried unsuccessfully to open the main cabin door, and the passengers were then evacuated through the emergency exit.

Talon Air Service

Witnesses observed the airplane contact the water while buzzing a lake, 'emerge from a cloud of water,' and enter a climb trailing white vapor. As the airplane approached the lake shore, the right propeller 'quit turning,' then the airplane entered a steep right bank and impacted the ground. The right propeller lever was found in the feather position. Propeller teardowns revealed signatures indicating the right propeller was feathered and the left propeller was operating in the low pitch range at impact. Disassembly of the engines revealed no evidence of any pre-impact mechanical anomalies, and, in the opinion of the manufacturer, 'both engines appeared capable of producing power prior to impact.' Toxicological tests showed 178.000 mg/dl (0.178%) ethanol in vitreous fluid, 90.000 mg/dl (0.09%) ethanol in blood, 114.000 mg/dl (0.114%) ethanol in brain fluid, 3.000 mg/dl acetaldehyde in brain fluid, 22.000 mg/dl acetaldehyde in blood, and 4.000 mg/dl 2-propanol in brain fluid. The levels of ethanol found indicate ingestion of alcohol, and the levels of acetaldehyde and 2-propanol (metabolites of ethanol) detected support ingestion of alcohol.