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N41VK accident description

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Crash location 26.591389°N, 82.190555°W
Nearest city Captiva Island, FL
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Tail number N41VK
Accident date 28 Feb 2003
Aircraft type Beech 36
Additional details: None

NTSB description


On February 28, 2003, about 1540 eastern standard time, a Beech 36, N41VK, registered to and operated by a private individual, impacted with the ocean waters of Pine Island Sound, shortly after takeoff from North Captiva Air Inc Airport, Captiva Island, Florida. The personal flight was conducted under 14 CFR Part 91. The airplane was destroyed. The private pilot, the sole occupant, was fatally injured. The flight departed Captiva Island about 1530 and was en route to Page Field Airport, Fort Myers, Florida. According to witnesses, instrument meteorological conditions prevailed. No flight plan was filed.

Page Field Airport is located approximately 19 nautical miles on an easterly heading from Captiva Island. About the first 5 nautical miles of the route are over the open waters of Pine Island Sound.

A witness, who was an instrument rated private pilot, observed the airplane depart. The witness stated that the airplane "was in IMC [instrument meteorological conditions] about 100 feet MSL as he departed over the Gulf of Mexico." The witness further stated that "there was heavy fog everywhere." He listened to the sound of the airplane's engine "for a minute or two after departure to be sure there were no unusual sounds."

Target radar data from the FAA's Fort Myers TRACON was recorded for the flight from 1535:30 to 1537:09. The first radar hit showed the airplane about 1 nautical mile southeast of the departure airport at 400 feet msl. Between 1535:30 and 1536:45, the airplane maintained an east-northeast heading, initially climbing to 700 feet and then descending to 500 feet. The airplane then began to turn left. The airplane had turned approximately 100 degrees and was passing through a northerly heading when the last radar hit was recorded at 1537:09. The last recorded radar hit showed the airplane at 500 feet about 4 nautical miles northeast of the departure airport.

There were no radio communications from the airplane to any air traffic control facility. The pilot had intended to pick up some passengers at Page Field, and when he did not arrive, concerned family members notified authorities. Search and rescue efforts were started, but were called off due to fog and darkness. The next morning, the wreckage was found by a search aircraft at latitude 26:35.29 N and longitude 82:11.26 W, about 2 statute miles on a heading of 117 degrees from the departure airport, in 5 feet of water. The wreckage was recovered from Pine Island Sound on March 1, 2003.


The pilot held a private pilot certificate with airplane single engine land and instrument ratings. His most recent application for a third class medical certificate was made on February 20, 2003, and the application was pending FAA action at the time of the accident. Review of the pilot's logbook by the NTSB investigator-in-charge revealed that the pilot had a total flight time of about 1,240 hours. He had logged 95 hours of instrument flight time of which 40 hours were in actual instrument meteorological conditions.


Examination of the airplane's maintenance records revealed that the 1969 model Beech Bonanza 36 received its most recent annual inspection on March 27, 2002, at an airframe total time of 5,767 hours. As of that date, the engine, a Continental IO-520-BA, S/N 555992, had accumulated 993 hours since major overhaul. The most recent maintenance was an engine oil change completed on August 20, 2002, at which time the airframe had accumulated 5,814 hours and the engine had accumulated 1,040 hours since major overhaul.


A fisherman on the water in the area of the accident site, did not hear or see the accident, but did report that about 1530, fog rolled in over Pine Island Sound, reducing visibility to 0 feet for about 15 minutes. The visibility then increased to 50 feet.

At 1553, the reported weather conditions at Page Field Airport, Fort Myers, Florida, located approximately 19 nautical miles east of the accident site, were wind from 230 at 9 knots, visibility 10 statute miles, few clouds at 2,000 feet agl, temperature 27 degrees C, dewpoint 23 degrees C, and altimeter 29.95 inches.

At 1553, the reported weather conditions at Southwest Florida International Airport, Fort Myers, Florida, located approximately 25 nautical miles east of the accident site, were wind from 240 at 10 knots, visibility 10 statute miles, few clouds at 2,500 feet agl, temperature 28 degrees C, dewpoint 21 degrees C, and altimeter 29.95 inches.


The wreckage was examined on March 2, 2003, by the NTSB investigator-in-charge and representatives from Raytheon Aircraft Company and Teledyne Continental Motors. The salvage crew reported that the engine, firewall and instrument panel were found separated from the fuselage. All major components of the airplane were recovered from the accident site except the propeller and the elevator counterweights. Examination of the crankshaft fracture surface revealed evidence consistent with the propeller separating as a result of impact forces. The fuel selector was on the right fuel tank. The landing gear actuator was found in the extended position.

Both wings separated from the fuselage. The right wing remained intact, and the right tip tank and approximately 8 feet of the outboard upper skin panel exhibited fire damage. The paint was bubbled, but the fire did not penetrate the skin panel. There was a gouge in the right wing leading edge approximately 5 feet from the wing root measuring 16 inches in depth. The right bladder fuel cell was breached in this area. The right flap was found in the retracted position, and the right aileron was attached. The left wing was found in several pieces. The left aileron bell crank and some of the upper skin panels were not located. The left tip tank separated from the wing, and the left main landing gear separated from the gear mounts. Flight control continuity was confirmed from the ailerons to the control yoke.

The empennage remained attached to the fuselage. The rudder and elevators remained attached. Flight control continuity was confirmed from the elevator and rudder to the floor panel under the left pilot seat.

The engine was intact with the fuel pump, right magneto, fuel metering unit and the majority of the intake and exhaust pipes separated. The valve covers and top spark plugs were removed, the crankshaft was rotated, and continuity was confirmed to all of the cylinders and to the rear of the engine. Compression was confirmed on all of the cylinders. The top spark plugs showed moderate to heavy wear when compared to the Champion Check A Plug card. The vacuum pump was in place, undamaged and full of water. The drive shaft was free to rotate. The vacuum pump was disassembled, and no internal damage was observed. The fuel pump was separated and intact; the drive shaft was missing. The unit was disassembled, and no internal damage was observed. The fuel manifold was disassembled and water was found in the interior; the diaphragm and spring were intact and undamaged, and a small amount of debris was noted on the screen. The oil filter was opened, and the element was clean and clear with no metal deposits. Heavy corrosion was observed on both magnetos; the cases were beginning to disintegrate. The left magneto was free to rotate, and the right magneto would not rotate. Both magnetos were disassembled, and they had heavy interior corrosion.


An autopsy was performed by the Office of the District Medical Examiner, Fort Myers, Florida. Toxicological testing by the FAA's Toxicology and Accident Research Laboratory detected no carbon monoxide, cyanide or ethanol. The tests detected diphenhydramine in blood and urine.


The wreckage was released to a representative of the owner on March 3, 2003.

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