Private American

Cessna 421C Golden Eagle III

On July 10, 2021, about 0920 mountain daylight time, a Cessna 412C airplane, N66NC, was substantially damaged when it was involved in an accident near Longmont, Colorado. The pilot and three passengers received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. After the airplane lifted off from the runway, the pilot didn’t feel that the engine(s) were making full power. The airplane settled back onto the runway, then exited off the departure end of the runway. The airplane came to rest upright, and a small post-crash fire developed. Substantial damage was noted to the airplane’s fuselage and wings.

Cessna 421B Golden Eagle II

On March 11, 2021, about 1953 eastern daylight time, a Cessna 421B, N80056, was substantially damaged when it was involved in an accident at the Macon County Airport (1A5), Franklin, North Carolina. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, this was a planned local flight. The pilot stated that it was a normal start, taxi, and run-up before takeoff. He initiated the takeoff roll and called out speeds in 10 knot (kts) increments looking for a rotation speed of 100 kts. He said the airspeed reached 90 kts and the aircraft acceleration “lagged” while only reaching a maximum airspeed of around 92 kts. He noticed that the runway length was decreasing and elected to abort the takeoff with the remaining runway. He pulled both throttles to idle and initiated maximum braking. Examination of the runway by a Federal Aviation Administrator inspector, revealed tire skid marks beginning around 1,200 ft from the runway end and continued off into the grass. The airplane continued down a slope, and through a fence before coming to rest. All of the occupants exited the airplane safely and a post-crash fire ensued. The airplane sustained fire and structural damage to the fuselage.

Eclipse EA500

The pilot reported that, while conducting a night landing on a runway contaminated with ice and patchy packed snow, the airplane overshot the touchdown zone. The pilot tried to fly the airplane onto the runway to avoid floating. The airplane touched down firm and the pilot applied moderate braking, but the airplane did not decelerate normally. The airplane went off the end of the runway and collided with several Runway End Identifier Lights (REILs) and a tree. The airplane sustained substantial damage to the left and right wings. The pilot reported that he did not feel modulation in the anti-lock braking system (ABS) and felt that might have contributed to the accident. An examination of fault codes from the airplane’s diagnostic storage unit indicated no ABS malfunctions or failures. An airport employee reported that he saw the airplane unusually high on the final approach and during the landing the airplane floated or stayed in ground effect before it touched down beyond the midpoint of the runway. The airplane’s long touchdown was captured by an airport surveillance video, which is included in the report docket.

BAe 125

After flying over the Yucantan Province and the Cayman Islands, the aircraft entered the Venezuelan Airspace without permission. It was pursued by F-16 fighters over the Lake of Maracaibo until it crashed in unknown circumstances in the Jesús María Semprún municipality. There was no fire and no casualties apparently. The aircraft was destroyed.

Pilatus PC-12

On November 6, 2020, about 1600 Pacific standard time, a Pilatus PC-12, N400PW, was substantially damaged when it was ditched in the Pacific Ocean about 1000 miles east of Hilo, Hawaii. The two pilots sustained no injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 ferry flight. According to the pilot-in-command (PIC), who was also the ferry company owner, he and another pilot were ferrying a new airplane from California to Australia. The first transoceanic leg was planned for 10 hours from Santa Maria Airport (KSMX), Santa Maria, California to Hilo Airport (PHTO), Hilo, Hawaii. The manufacturer had an auxiliary ferry fuel line and check valve installed in the left wing before delivery. About 1 month before the trip, the pilot hired a ferry company to install an internal temporary ferry fuel system for the trip. The crew attempted the first transoceanic flight on November 2, but the ferry fuel system did not transfer properly, so the crew diverted to Merced Airport (KMCE), Merced, California. The system was modified with the addition of two 30 psi fuel transfer pumps that could overcome the ferry system check valve. The final system consisted of 2 aluminum tanks, 2 transfer pumps, transfer and tank valves, and associated fuel lines and fittings. The ferry fuel supply line was connected to the factory installed ferry fuel line fitting at the left wing bulkhead, which then fed directly to the main fuel line through a check valve and directly to the turbine engine. The installed system was ground and flight checked before the trip. According to Federal Aviation Administration automatic dependent surveillance broadcast (ADS-B) data, the airplane departed KSMX about 1000. The pilots each stated that the ferry fuel system worked as designed during the flight and they utilized the operating procedures that were supplied by the installer. About 5 hours after takeoff, approaching ETNIC intersection, the PIC climbed the airplane to flight level 280. At that time, the rear ferry fuel tank was almost empty, and the forward tank was about 1/2 full. The crew was concerned about introducing air into the engine as they emptied the rear ferry tank, so the PIC placed the ignition switch to ON. According to the copilot (CP), she went to the cabin to monitor the transparent fuel line from the transfer pumps to ensure positive fuel flow while she transferred the last of the available rear tank fuel to the main fuel line. When she determined that all of the usable fuel was transferred, and fuel still remained in the pressurized fuel line, she turned the transfer pumps to off and before she could access the transfer and tank valves, the engine surged and flamed out. The PIC stated that the crew alerting system (CAS) fuel low pressure light illuminated about 5 to 15 seconds after the transfer pumps were turned off, and then the engine lost power and the propeller auto feathered. The PIC immediately placed the fuel boost pumps from AUTO to ON. The CP went back to her crew seat and they commenced the pilot operating handbook’s emergency checklist procedures for emergency descent and then loss of engine power in flight. According to both crew members, they attempted an engine air start. The propeller unfeathered and the engine started; however, it did not reach flight idle and movement of the power control lever did not affect the engine. The crew secured the engine and attempted another air start. The engine did not restart and grinding sounds and a loud bang were heard. The propeller never unfeathered and multiple CAS warning lights illuminated, including the EPECS FAIL light (Engine and Propeller Electronic Control System). The crew performed the procedures for a restart with EPECS FAIL light and multiple other starts that were unsuccessful. There were no flames nor smoke from either exhaust pipe during the air start attempts. About 8,000 ft mean sea level, the crew committed to ditching in the ocean. About 1600, after preparing the survival gear, donning life vests, and making mayday calls on VHF 121.5, the PIC performed a full flaps gear up landing at an angle to the sea swells and into the wind. He estimated that the swells were 5 to 10 ft high with crests 20 feet apart. During the landing, the pilot held back elevator pressure for as long as possible and the airplane landed upright. The crew evacuated through the right over wing exit and boarded the 6 man covered life raft. A photograph of the airplane revealed that the bottom of the rudder was substantially damaged. The airplane remained afloat after landing. The crew utilized a satellite phone to communicate with Oakland Center. The USCG coordinated a rescue mission. About 4 hours later, a C-130 arrived on scene and coordinated with a nearby oil tanker, the M/V Ariel, for rescue of the crew. According to the pilots, during the night, many rescue attempts were made by the M/V Ariel; however, the ship was too fast for them to grab lines and the seas were too rough. After a night of high seas, the M/V Ariel attempted rescue again; however, they were unsuccessful. That afternoon, a container ship in the area, the M/V Horizon Reliance, successfully maneuvered slowly to the raft, then the ship’s crew shot rope cannons that propelled lines to the raft, and they were able to assist the survivors onboard. The pilots had been in the raft for about 22 hours. The airplane was a new 2020 production PC-12 47E with a newly designed Pratt and Whitney PT6E-67XP engine which featured an Engine and Propeller Electronic Control System. The airplane is presumed to be lost at sea. The investigation is ongoing.

Gulfstream GIII

Probably engaged in an illegal flight, the aircraft crashed in unknown circumstances in an isolated and swampy area located in the Laguna del Tigre National Park. The wreckage was found on November 2 about 7 km south from the Mexican border. Two dead bodies were found and the aircraft was destroyed.

Cessna 340

On final approach to Orléans-Loiret Airport (ex Saint-Denis-de-l’Hôtel), the pilot encountered engine problems and elected to make an emergency landing. The twin engine aircraft crash landed in a wooded area located about 3 km short of runway 23 and burst into flames. Both occupants aged 55 and 60 escaped uninjured while the aircraft was totally destroyed by fire.

Rockwell Sabreliner 75

The aircraft entered the Venezuelan airspace without flight plan and authorisation. While flying over the Paraguaña Peninsula at low altitude, the crew was forced to land when control was lost. The aircraft crashed in shallow water few meters offshore, lost its tail and both wings. Both pilots were killed.

Beechcraft 200 Super King Air

Engaged in an illegal flight, the twin engine airplane landed on a dirt road located about 35 km southwest of Brus Laguna. The nose gear collapsed and the aircraft came to rest, damaged beyond repair. No one was found on site and a load of 806 kilos of cocaine was seized.

Gulfstream GII

The crew was engaged in an illegal trip and elected to land on a remote 'airstrip' located in the region of Machiques. The aircraft crash landed and came to rest, bursting into flames. One pilot was killed and the second was injured.

BAe 125

The airplane landed on an illegal airstrip, lost its nose gear and hit obstacles before coming to rest. No one was found on site. The aircraft was damaged beyond repair.

Cessna 402

According the commercial pilot and a flight instructor rated check pilot, they were conducting their first long-duration, aerial observation flight in the multiengine airplane, which was recently acquired by the operator. They departed with full fuel tanks, competed the 5-hour aerial observation portion of the flight, and began to return to the destination airport. About 15 miles from the airport, the left engine fuel warning light illuminated. Within a few seconds, the right engine stopped producing power. They attempted to restart the engine and turned the airplane toward an alternate airport that was closer. The pilots then turned on the electric fuel pump, the right engine began surging, and soon after the left engine stopped producing power. They turned both electric fuel pumps to the low setting, both engines continued to surge, and the pilots continued toward the alternate airport. When they were about 3 miles from the airport, both engines lost total power, and they elected to land on a highway. When they were a few feet above the ground, power returned briefly to the left engine, which resulted in the airplane climbing and beginning to roll. The commercial pilot pulled the yoke aft to avoid a highway sign, which resulted in an aerodynamic stall, and subsequent impact with trees and terrain. The airplane sustained substantial damage to the wings and fuselage. Although both pilots reported the fuel gauges indicated 20 gallons of fuel remaining on each side when the engines stopped producing power, the flight instructor noted that there was no fuel in the airplane at the time of the accident. In addition, according to a Federal Aviation Administration inspector who responded to the accident site, both fuel tanks were breached and there was no evidence of fuel spillage.

BAe 125

The aircraft crashed in unknown circumstances in a wooded area located near La Libertad and was totally destroyed by impact forces and a post crash fire. Both pilots were killed. Guatemalan Authorities reported the aircraft was engaged in a contraband mission and a load of 762 kilos of cocaine was found.

Cessna 550 Citation II

The pilot was conducting a personal cross-country flight in a turbofan-powered airplane. Shortly after departure, the airplane entered a witness-estimated 90° left bank with the nose parallel to the horizon; as the airplane began to roll out of the turn, the nose remained at or below the horizon before it dropped and the airplane impacted the ground. Flight track data revealed that, shortly after departure, the airplane's ground speed immediately began decreasing from its maximum of 141 knots during takeoff and continued decreasing until the last recorded data point, which showed that the airplane had a ground speed of 100 knots. The surface wind reported about 10 minutes before the accident was from 170° at 9 knots, gusting to 14 knots, which resulted in a 1- to 2-knot tailwind component. Given this information and the airplane's configuration at the time of the accident, the airplane's indicated airspeed (IAS) would have been between about 86 and 93 knots. The airplane's stall speed was calculated to be 100 knots IAS (KIAS) with a bank angle of 45° and 118 KIAS with a bank angle of 60°. Thus, the pilot failed to maintain airspeed or accelerate after departure, which resulted in an aerodynamic stall A pilot who had flown with the accident pilot twice before the accident reported that, during these flights, the pilot had flown at reduced power settings and slower-than-normal airspeeds. During the flight 1 year before the accident, he reached over and pushed the power levers forward himself. He also stated that every time he had flown with the pilot, he was "very behind the airplane." Postaccident examination of the engines revealed no signs of preimpact mechanical failures or malfunctions that would have precluded normal operation, and both engines exhibited circumferential rub marks on all rotating stages, blade tip bending opposite the direction of rotation, and debris ingestion through the gas path, indicating that the engine had power at impact. Further, the right engine full authority digital electronic control (FADEC) nonvolatile memory recorded no faults. (The left engine FADEC could not be downloaded due to damage.) The Airplane Flight Manual stated that the pilot must, in part, advance the throttle lever to the maximum takeoff detent for the FADEC's nonvolatile memory to record a logic trend snapshot 2 seconds after takeoff. The lack of a FADEC logic trend snapshot is consistent with the pilot not fully advancing the throttles during the takeoff and initial climb and is likely why he did not attain or maintain sufficient airspeed. The flight track data, pilot witness account, and airplane damage are consistent with the pilot failing to fully advance the power levers while maneuvering shortly after takeoff, which led to his failure to maintain sufficient airspeed and resulted in the exceedance of the airplane's critical angle of attack and a subsequent aerodynamic stall.

Beechcraft 60 Duke

The commercial pilot was relocating the multiengine airplane following the completion of an extensive avionics upgrade, which also included the installation of new fuel flow transducers. As the pilot neared the destination airport, he reported over the common traffic advisory frequency that he had "an engine out [and] smoke in the cockpit." Witnesses observed and airport surveillance video showed fire emanating from the airplane's right wing. As the airplane turned towards the runway, it entered a rightrolling descent and impacted the ground near the airport's perimeter fence. The right propeller was found feathered. Examination of the right engine revealed evidence of a fire aft of the engine-driven fuel pump. The fuel pump was discolored by the fire. The fire sleeves on both the fuel pump inlet and outlet hoses were burned away. The fuel outlet hose from the fuel pump to the flow transducer was found loose. The reason the hose was loose was not determined. It is likely that pressurized fuel sprayed from the fuel pump outlet hose and was ignited by the hot turbocharger, which resulted in the inflight fire.

Piper PA-31-350 Navajo Chieftain

In the morning, the Guatemala Army Forces were informed by ATC that a PA-31 entered the Guatemala Airspace without prior permission. The twin engine airplane crashed in a wooded area located near the farm of Sepens located in the region of Sayaxché, Petén. The aircraft was partially destroyed by impact forces and both occupants were killed. A sticker was set on the fuselage with the registration N2613 which is wrong.

Rockwell Sabreliner 60

The aircraft crashed in unknown circumstances in an isolated and uninhabited area located about 14 km east of Bajamar, Honduras. The airplane was engaged in an illegal mission (drug smuggling flight) as a pack of cocaine and a gun were found in the wreckage. The crew disappeared and was not recovered.

BAe 125

The aircraft was engaged in an illegal flight, carrying two pilots and a load of 200 kg of cocaine. En route, the crew apparently encountered an unexpected situation and was forced to attempt an emergency landing when the airplane crashed in a wooded area located near San Pedro de Peralta. A pilot was killed while the second was seriously injured. Originally registered N299GS, the aircraft was cancelled from the US registered on 15 February 2018 and exported to Mexico. The registration N18BA is false.

Cessna 421 Golden Eagle

The twin engine aircraft crashed in unknown circumstances in an open field located near Génova. The aircraft came to rest upside down and both occupants were killed. It is understood that the registration was false as N113FT is officially attributed to a Piper PA-46 according to the FAA. Thus, it is believed that the flight was illegal.

Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class)

While overflying the Yucatán Province, en route from Monterrey to Cancún, the pilot informed ATC that he was low of fuel and requested the permission to divert to Chichén Itzá Airport for an emergency landing. While approaching the airfield by night, the single engine aircraft descended into trees and crashed few km from the airport. The airplane was destroyed and there was no fire. All five occupants were injured.

Piper PA-31-350 Navajo Chieftain

The twin engine airplane was involved in a smuggling flight within Mexico and was carrying three people. In unclear circumstances, the pilot attempted a belly landing in a swampy area located in El Sacrificio, State of Campeche. The wreckage was found by local authorities few hours later and no trace of the occupant was found or the load was found. The registration N633D is attributed to a Piper PA-31 with MSN 31-7852098 which was not involved in this accident. Thus, it was confirmed by Mexican and US Authorities that the registration was false.

Piper PA-61 Aerostar (Ted Smith 601)

Following an uneventful flight from Bitburg, the pilot was cleared for an approach to Karlsruhe-Baden Baden Airport Runway 21. On final approach, while completing a sharp turn to the left to join the runway, the twin engine airplane stalled and crashed in an open field, bursting into flames. The pilot was seriously injured and the aircraft was destroyed by a post crash fire. The wreckage was found about 500 metres from the runway threshold and 350 metres to the left of the runway extended centerline.

Rockwell Sabreliner 75

The aircraft, a Rockwell Sabreliner 75A (NA-265-80 version) departed Celaya-Capitán Rogelio Castillo Airport shortly before 0700LT on a short flight to Santiago de Querétaro without any flight plan and with an unknown number of people on board. At 0731LT, the crew contacted the destination airport and elected to land about seven minutes later. After landing on runway 27, the crew was instructed to vacate via taxiway for the apron but the aircraft continued, veered off runway after a distance 800 metres, impacted a rocky wall, lost its nose gear and came to rest. When the rescuers arrived on the scene, there was nobody as the occupants left the airplane and disappeared. It appears the flight was illegal and it is believed that the aircraft was stolen at Celaya Airport.

Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class)

According to the pilot, he checked the winds via his onboard weather reporting device during the run-up, and he stated that the 25 knot wind sock was about ¾ full just moments before the takeoff roll. He reported that during the takeoff roll the airplane encountered a significant wind gust from the right. He stated that the wind gust forced the airplane to exit the left side of the runway, the landing gear collapsed, and the airplane collided with metal pylons which surrounded the wind sock. The airplane sustained substantial damage to both wings, fuselage, horizontal stabilizer and elevator. The pilot reported that there were no mechanical failures or anomalies prior to or during the flight that would have prevented normal flight operation. According to the Airport/Facility Directory, the Airport Remarks state: Airport located in mountainous terrain with occasional strong winds and turbulence. Lighted windsock available at runway ends and centerfield. With southerly crosswinds in excess of 15 knots, experiencing turbulence and possible windshear along first 3000´ of Runway 27. The reported wind at the airport during the time of the accident was from 200 degrees true at 22 knots, with gusts at 33 knots, and the departure runway heading was 27. According to the pilot operating hand book the maximum demonstrated crosswind component for this airplane is 17 knots. The crosswind component during the time of the accident was 26 knots.

Rockwell Grand Commander 680

The aircraft was probably engaged in an illegal flight when it crashed under unknown circumstances in a desert area located in Los Hatos, about 5 km northeast of Capatárida, Venezuela. The aircraft was destroyed and both occupants were killed. No flight plan was filed to enter the Venezuelan airspace.

De Havilland DHC-2 Beaver

At 14:01 on August 9th, 2015, a pilot along with a friend, a contracted ferry flight pilot, planned to fly airplane N610LC, which is of the type De Havilland DHC-2 Beaver, under Visual Flight Rules (VFR) from Akureyri Airport to Keflavik Airport in Iceland. The purpose of the flight was to ferry the airplane from Akureyri to Minneapolis/St. Paul in the United States, where the airplane was to be sold. The airplane was initially flown in Eyjafjörður in a northernly direction from Akureyri, over Þelamörk and then towards and into the valley of Öxnadalur. The cloud ceiling was low and it was not possible to fly VFR flight over the heath/ridge of Öxnadalsheiði. The airplane was turned around in the head of the valley of Öxnadalur and flown towards the ridge of Staðartunguháls, where it was then flown towards the heath/ridge of Hörgárdalsheiði at the head of the valley of Hörgárdalur. In the valley of Hörgárdalur it became apparent that the cloud base was blocking off the heath/ridge of Hörgárdalsheiði, so the airplane was turned around again. The pilots then decided to fly around the peninsula of Tröllaskagi per their original backup plan, but when they reached the ridge of Staðartunguháls again the pilots noticed what looked like a break in the cloud cover over the head of the valley of Barkárdalur. A spontaneous decision was made by the pilots to fly into the valley of Barkárdalur. The valley of Barkárdalur is a long narrow valley with 3000 – 4500 feet high mountain ranges extending on either side. At the head of the valley of Barkárdalur there is a mountain passage at an elevation of approximately 3900 ft. About 45 minutes after takeoff the airplane crashed in the head of the valley of Barkárdalur at an elevation of 2260 feet. The pilot was severely injured and the ferry flight pilot was fatally injured in a post crash fire.

BAe 125

The aircraft took off in the day from an airfield located in Venezuela with two passengers, two pilots and a load of 1,3 ton of narcotics, en route to Central America. While cruising over the Caribbean Sea off the Colombian coast, the aircraft was intercepted by a Colombian Air Force fighter. In unclear situation, the right engine of the Hawker caught fire (shot down ?). The crew descended in a low nose down attitude until the aircraft impacted the sea and disintegrated. All four occupants were killed and the load of narcotics was found floating on water. Three dead bodies and some debris of the aircraft were found few days later on a beach located northeast of Puerto Colombia. The aircraft was identified as N917TF which departed Fort Lauderdale-Executive Airport, Florida for Toluca, Mexico on May 1, 2015. It was formally cancelled from the U.S. register on June 2, 2015 as exported to Mexico.

Cessna 208B Grand Caravan

The pilot reported that, during the postmaintenance test flight, the turboprop engine lost power. The airplane was unable to maintain altitude, and the pilot conducted a forced landing, during which the airplane was substantially damaged. The engine had about 9 total flight hours at the time of the accident. A teardown of the fuel pump revealed that the high-pressure drive gear teeth exhibited wear and that material was missing from them, whereas the driven gear exhibited little to no visible wear. A metallurgical examination of the gears revealed that the damaged drive gear was made of a material similar to 300-series stainless steel instead of the harder specified M50 steel, whereas the driven gear was made of a material similar to the specified M50 steel. Subsequent to these findings, the airplane manufacturer determined that the gear manufacturer allowed three set-up gears made from 300-series stainless steel to become part of the production inventory during the manufacturing process. One of those gears was installed in the fuel pump on the accident airplane, and the location of the two other gears could not be determined. Based on the evidence, it is likely that the nonconforming gear installed in the fuel pump failed because it was manufactured from a softer material than specified, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power. The manufacturer subsequently inspected its stock of gears and issued notices to customers that had engines with fuel pumps installed with the same part number gear set as the one installed on the accident airplane. The manufacturer also issued a service information letter and service bulletins regarding the fuel pump gear set for engines used in civilian and military applications. As of the date of this report, the two remaining gears have not been located.

Piper PA-61 Aerostar (Ted Smith 601)

The pilot's friend reported that the pilot planned to fly his recently purchased twin-engine airplane over his friend's home to show it to him and another friend. The pilot's friends and several other witnesses reported observing the pilot performing low-level, high-speed aerobatic maneuvers before the airplane collided with trees and then terrain. A 1.75-liter bottle of whiskey was found in the airplane wreckage. A review of the pilot's Federal Aviation Administration medical records revealed that he had a history of alcohol dependence but had reportedly been sober for almost 4 years. Toxicological testing revealed that the pilot had a blood alcohol content of 0.252 milligrams of alcohol per deciliter of blood, which was over six times the limit (0.040) Federal Aviation Regulations allowed for pilots operating an aircraft.

Cessna 303 Crusader

Following an uneventful flight from Cannes-Mandelieu Airport, the pilot initiated the approach to Barcelonnette-Saint-Pons Airport Runway 27. Following an unstabilized approach, the aircraft landed hard, causing the left main gear to collapse. The aircraft veered off runway to the left, lost its right main gear and came to rest. There was no fire. All five occupants escaped uninjured and the aircraft was damaged beyond repair.

Piper PA-31-310 Navajo

The twin engine aircraft was engaged in a local post maintenance test flight at Monterrey-Del Norte Airport. Shortly after takeoff, the airplane encountered difficulties to gain height when it stalled and crashed in a field located 500 metres past the runway end, bursting into flames. The aircraft was destroyed by fire and both occupants were killed.

Piper PA-31-350 Navajo Chieftain

The pilot stated he experienced a high temperature in the right engine and a partial loss of engine rpm while at 9,000 feet mean sea level in cruise flight. He requested and received clearance from air traffic control to descend and divert to another airport. He leveled the airplane at 2,500 feet and both engines were operating; however, the right engine experienced a loss of rpm which made it difficult to maintain altitude. The pilot reduced power in both engines, turned the fuel boost pump on, opened the cowl flaps and the engine continued to run with a low rpm. The pilot elected to ditch the airplane in the ocean, instead of landing as soon as practical at the nearest suitable airport, as instructed in the Pilot's Operating Handbook (POH). Additionally, he shut down the right engine before performing the troubleshooting items listed in the POH. He attributed his decision to ditch the airplane to poor single-engine performance and windy conditions. The wind at the destination airport was from 060 degrees at 6 knots and runway 8 was in use at the time of the accident. The airplane was not recovered.

Beechcraft 65 Queen Air

Shortly after takeoff for a repositioning flight for the airplane’s upcoming annual inspection, numerous witnesses, including the two air traffic controllers, reported observing the airplane climbing out normally until it was about 1/2 mile beyond the runway. The witnesses stated that the airplane then underwent a short series of attitude excursions, rolled right, and descended steeply into a lagoon. All radio communications between the airplane and the air traffic controllers were normal. Ground-based radar tracking data indicated that the airplane's climb to about 500 feet was normal and that it was airborne for about 40 seconds. Postaccident examination of the airframe, systems, and engines did not reveal any mechanical failures that would have precluded continued normal operation. Damage to both engines’ propeller blades suggested low or moderate power at the time of impact; however, the right propeller blades exhibited less damage than the left. The propeller damage, witness-observed airplane dynamics, and the airplane’s trajectory were consistent with a loss of power in the right engine and a subsequent loss of control due to airspeed decay below the minimum control speed (referred to as VMC). Although required by the Federal Aviation Administration (FAA)-approved Airplane Flight Manual, no evidence of a cockpit placard to designate the single engine operating speeds, including VMC, was found in the wreckage. The underlying reason for the loss of power in the right engine could not be determined. The airplane's certification basis (Civil Air Regulation [CAR] 3) did not require either a red radial line denoting VMC or a blue radial line denoting the single engine climb speed (VYSE) on the airspeed indicators; no such markings were observed on the airspeed indicators in the wreckage. Those markings were only mandated for airplanes certificated under Federal Aviation Regulation Part 23, which became effective about 3 years after the accident airplane was manufactured. Neither the Federal Aviation Administration (FAA) nor the airplane manufacturer mandated or recommended such VMC or VYSE markings on the airspeed indicators of the accident airplane make and model. In addition, a cursory search did not reveal any such retroactive guidance for any twin-engine airplane models certificated under CAR 3. Follow-up communication from the FAA Small Airplane Directorate stated that the FAA has "not discussed this as a possible retroactive action... Our take from the accident studies is that because of the accident record with light/reciprocating engine twins, the insurance industry has restricted them to a select group of pilot/owners…" Toxicology testing revealed evidence consistent with previous use of marijuana by the pilot; however, it was not possible to determine when that usage occurred or whether the pilot might have been impaired by its use during the accident flight.

Cessna 650 Citation III

The aircraft departed Valencia-Arturo Michelana Airport on a private flight to Puerto Ordaz, carrying one passenger and two pilots. While cruising at an altitude of 30,000 feet, the aircraft entered an uncontrolled descent and crashed in a near vertical attitude. The aircraft disintegrated on impact and all three occupants were killed.

Cessna 340

During the landing approach, a witness saw the twin-engine airplane slow and stall. The airplane crashed short of the runway, in a residential backyard. An airport manager flew with the pilot 8 days before the accident. The manager reported that during his flight the pilot flew the approach and landing with the aural stall warning horn activated. The manager advised the pilot of the aural warning, however no corrective action was taken by the pilot during that flight. An on-scene investigation revealed no preimpact mechanical anomalies. The pilot had about 12.6 hours of flight time in the accident airplane, of which 7.7 hours were dual instruction. Due to the lack of any mechanical problems with the airplane, the pilot's minimal experience in twin-engine airplanes, and his history of flying the airplane too slow, it is probable that he allowed the airspeed to decay below a safe speed, and inadvertently stalled it.

Cessna 401

For unknown reasons, the twin engine aircraft made a wheels up landing at Narsarsuaq Airport and came to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair. They were completing a flight from Goose Bay. The exact date of the occurrence remains unknown, somewhere in January 2007.

Learjet 25

The crew landed with the landing gear in the retracted position. While the airplane was on the base leg of the traffic pattern, the pilot heard a helicopter pilot make a transmission over the common radio frequency. As he completed the before landing checklist the pilot searched for the helicopter that he heard over the radio. During the landing flare he realized something was amiss and looked down at the instrument panel. He noticed that the landing gear lights were illuminated red. Just prior to contacting the runway surface he reached for the landing gear handle and manipulated it in the down position. The airplane made a smooth touchdown with the landing gear in the retracted position. The pilot stated that he did not make the proper check for the gear extension due to the timing of the helicopter distraction. The pilot reported no preimpact mechanical malfunctions or failures with the airplane or engine, stating that the accident was the result of pilot error.

Rockwell Grand Commander 690

The twin engine aircraft was completing an illegal flight from Colombia to the US with three people on board. While flying at low height, it collided with trees and crashed in a wooded and hilly terrain near El Gallito. The aircraft was destroyed and all three occupants were killed. On scene were found one ton of cocaine in several boxes, large sums of money and guns. The registration N572L was probably a false one.

Piper PA-61 Aerostar (Ted Smith 601)

The pilot attempted a night landing on a taxiway in front of the control tower, which was closed at the time. The airplane overran the end of the taxiway, rolled down an embankment and struck trees. The pilot, whose identity was not confirmed, was believed to have incurred minor injuries. He subsequently paid a passerby to take him to a local hotel, and after a night's rest, he left the area. Ownership of the airplane could not be determined due to a recent sale. Approximately 250 kilos of cocaine were found onboard the airplane. Further investigation was being conducted by federal authorities and local law enforcement.

Socata TBM-700

After an uneventful flight from Edinburgh the pilot made a visual approach to Runway 28 (landing distance available 1,400 metres) at Dundee. The pilot reported that the aircraft floated down the runway in the flare and bounced lightly on touchdown. During the bounce the aircraft initially yawed left and then rolled left in a normal pitch attitude with no stall warning. Full right rudder was applied but this was unable to correct the yaw. Power was applied to initiate a go-around, whilst maintaining full right rudder, but the pilot was unable to prevent the left wing from hitting the ground. This caused the aircraft to yaw rapidly to the left bringing one of its wheels into contact with a low wall. The pilot then reduced power and ditched in the River Tay, approximately 10 metres from the shore. The air traffic controllers on duty reported that the aircraft achieved a high nose attitude during the go-around before the left wing dropped and the aircraft veered to the left. The aircraft came to rest with the top of the fuselage out of the water and the pilot and passengers were able to evacuate though the main door and stand on the wing to await rescue by the airport's hovercraft. The hovercraft could only carry two passengers at a time thus the process was delayed resulting in the pilot and passengers suffering from mild hypothermia.

Curtiss C-46 Commando

The aircraft was probably involved in an illegal flight when it crashed and burnt while trying to land in a remote area located near Huetamo de Núñez. No one was found in the wreckage and it was later confirmed that the registration N1442V was false.

Douglas DC-6

Crashed in unknown circumstances in a desert area while engaged in an illegal contraband flight. There were no casualties. Any correlation with N72522 (DC-6A/B) MSN 44697/598 that may crash in Tlahualilo de Zaragoza, Durango on Feb 17 1992 ?

Cessna 402

Flight departed and upon reaching a point approx 35 miles north of airport pilot requested return to airport from ATC. Pilot did not declare emergency or report an engine problem. Upon entering traffic pattern at uncontrolled airport pilot stated he would follow a Cessna 152 for landing. On short final aircraft was seen making s turns to maintain spacing behind 152. Pilot then declared he had an engine shutdown and needed to land. 152 was in landing flare and landed. With 152 on runway pilot attempted a go around with full flaps extended, gear down, left engine shutdown, and at a slow airspeed. Aircraft rolled to left upon application of right engine power and nosed down from which it crashed. The number two cylinder of the left engine had suffered separation of the head from the barrel. Pilot logbook did not reflect pilot having current biennial flight review. The pilot, sole on board, was killed.

De Havilland DHC-3 Otter

The aircraft was on its way from Phoenix to Gustavus, AK, to be delivered to its new operator Glacier Bay Airways. On the leg from Port Hardy to Prince Rupert, while cruising at an altitude of 4,000 feet, the engine exploded and oil spread on the windscreen. The crew ditched the aircraft in the Grenville Channel and was quickly rescued. The aircraft sank and was not recovered.

Cessna 421B Golden Eagle II

Crashed in unknown circumstances while landing at Hoffmans Cay Airport. The pilot, sole on board, was killed.

Piper PA-31-350 Navajo Chieftain

The aircraft was completing an illegal flight from Santa Marta to Cat Island, Bahamas, carrying two pilots and a load of 500 kilos of cocaine. After entering illegally the Dominican Republic Airspace, the aircraft was shot down by the pilot of a Dominican Air Force A-37 and crashed in the sea off Cabo Rojo. Both occupants were killed.

Beechcraft 200 Super King Air

Stolen at Tomball Airport, Texas, then crashed in unknown circumstances somewhere in North Mexico while engaged in an illegal mission. Occupant fate unknown.

Cessna 411

The pilot reportedly did an unusual amount of engine run-up before pulling onto the runway. He then performed another run-up before departing. This is evidence that he was aware of a problem with his aircraft. The engine(s) were popping and puffing black smoke during the ground run. Yet, the takeoff was continued. The popping and smoke puffing continued after liftoff. A noticeable loss of airspeed occurred during the climbout. The aircraft started the third roll (into the bad engine) before finally going inverted. The aircraft's allowable gross weight was exceeded by at least 205 pounds at takeoff, however, the center of gravity remained within its specified limits. Internal examination of the right engine exhibited evidence that it had operated at sometime on a mixture of gasoline and jet fuel. All six occupants were killed.

Piper PA-61 Aerostar (Ted Smith 601)

The aircraft was involved in illegal activity when it was intentionally landed in an open pasture. During the landing, the aircraft veered left and struck a 30 inches high concrete culvert. The gear collapsed on contact with the culvert. Unknown personnel subsequently drug the aircraft with a vehicle to a barn. When they attempted to drag the aircraft into the barn, they tore the wings off and damaged the barn.

Cessna 411

Crashed following an engine failure at takeoff. The pilot, sole on board, was killed.