Fort Lauderdale-Executive

The flight was a VFR positioning flight from FLL to FXE. Transcripts of the cockpit voice recorder (CVR) showed that while waiting for takeoff from FLL the flightcrew heard the local controller reported to a Delta Airlines flight that was on a seven mile final approach to land on runway 27R that the winds were 250 degrees at 19 knots, gusting to 50 knots. The Delta Airlines flight crew then informed the controller they were making a missed approach. At 1130:05 the captain asks the first officer if "can you see the end of the weather? If we make a hard right turn, can we stay clear of it?" The first officer responded "I believe so." At 1130:06 the local controller reported "wind shear alert. The centerfield wind 230 at 22. Runway 27R departure 25 knot loss one mile departure." The captain stated to the first officer "sweet." At 1132:11 the captain transmitted to the local controller "tower, any chance of Hop-a-Jet 55 getting out of here?" The local controller responded wind 230 at 17, right turn direct FXE approved, runway 27R cleared for takeoff. The captain responded "cleared to go, right turn out." At 1133:10 the captain asks for gear up. At 1133:15 the local controller responded to a Southwest Airlines Flight waiting for takeoff "no, don't look like anyone's gonna go." "The uh, weather is due west moving rapidly to the north. It looks like a few minutes, and you all be in the clear straight out." At 1133:17, the captain stated to the first officer "oh #. Think this was a bad idea." The first officer responded "no airport in sight." At 1133:43 the sound similar to precipitation hitting the windshield is recorded. At 1133:46 the FLL local controller instructs the flight crew to contact FXE Tower. At 1133:54 the CVR records the FXE local controller transmitting "wind 200, variable 250 at 15, altimeter 29.99. Heavy cell of weather to the west moving eastbound. Low level wind shear possible. At 1134:16, the FXE local controller transmits "attention all aircraft, low level wind shear advisories are in effect. Use caution. Wind 240 at 10." At 1134:51, the first officer transmitted to the FXE local controller that the flight was over the shoreline inbound full stop. At 1135:02, the FXE local controller transmitted "Hop-a-Jet 55, Executive tower, wind 210 variable 250 at 35, 35 knots and gusting. Winds are uh, heavy on the field. Low level wind shear advisories are in effect. Heavy rains from the west, eastbound and would you like to proceed inbound and land Executive? Say intentions." The first officer responded "that's affirmative." The local controller responded, "Hop-a-Jet 55 straight in runway three one if able. The winds 230 gusts, correction, winds 230 variable 210 at 25." At 1135:48, the local controller transmitted, "Hop-a-Jet 55, wind 230 variable 300 at 25 gusts 35. Altimeter 30.00. Runways are wet. Traffic is exiting the runway prior to your arrival, a Dutchess. Caution standing water on runways. Low level wind shear advisories in effect, Runway 31. Cleared to land." The first officer responded "cleared to land, Hop-a-Jet 55." At 1136:35, the local controller transmitted "wind 230 at 25, gusts 35." At 1136:58, the CVR records the sound similar to precipitation on the windshield. At 1137:17, the CVR records a sound similar to the aircraft touching down on the runway. At 1137:19, the sound of a repetitive tone similar to the thrust reverser warning starts and continues to the end of the recording. At 1137:23 a loud unidentified roaring sound starts and lasts 8 seconds. At 1137:30, loud rumbling noises similar to the aircraft departing the runway start. At 1137:36, a continuous tone similar to landing gear warning signal sounds and continues to the end of the recording. The rumbling noises stop. At 1137:39 the captain states the thrust reversers didn't stow and at 1138:36, the captain states "I went around and the # TRs stayed. The CVR recording ended. The 1132, Goes-12 infrared image depicts a rapidly developing cumulonimbus cloud between and over the FLL and FXE airports. The top of the cloud over FXE was in the range of 22,000 feet. The top of the cloud southwest of FXE was in the 39,000 feet range. The 1145, Goes-12 infrared image depicts a developing cumulonimbus cloud over FXE with the cloud top in the 42,000 feet range. Data was obtained from the Melbourne, Florida Doppler Weather Radar System, located 118 miles north-northwest of the accident site. The data showed that at FXE, between 1130 and 1145, a VIP Level 1 to 2 echo evolved into a VIP Level 5 "intense" echo at 1135 and a VIP Level 6 "extreme" echo by 1145.

On March 31, 2004, about 1235 eastern standard time, a Cessna 402B, N269JH, registered to and operated by Tropic Air Charters, Inc., experienced collapse of all landing gears at the Walker's Cay Airport, Walker's Cay, Bahamas. Visual meteorological conditions prevailed at the time and a visual flight rules flight plan was filed for the 14 CFR Part 135 on-demand, non-scheduled, international, cargo flight from the Fort Lauderdale Executive Airport, Fort Lauderdale, Florida, to the Walker's Cay Airport, Walker's Cay, Bahamas. The airplane was substantially damaged and the commercial-rated pilot, the sole occupant, was not injured. The flight originated about 45 minutes earlier from the Fort Lauderdale Executive Airport. The pilot stated that after landing, the right wing tipped down in what appeared to be a flat tire. He attempted to maintain control of the airplane using the rudder and was successful until the airplane rolled approximately 1,000 feet. The airplane then veered to the right and collided with a tree. The left wing and fuselage were damaged.

The captain and first officer were conducting a CFR Part 135 on-demand charter flight, returning two passengers to the accident airplane's base airport. The multi-destination flight originated from the accident airport, about 16 hours before the accident. On the final leg of the flight, the flight encountered stronger than anticipated headwinds, and the first officer voiced his concern several times about the airplane's remaining fuel. As the flight approached the destination airport, the captain became concerned about having to fly an extended downwind leg, and told the ATCT specialist the flight was low on fuel. The ATCT specialist then cleared the accident airplane for a priority landing. According to cockpit voice recorder (CVR) data, while the crew was attempting to lower the airplane's wing flaps in preparation for landing, they discovered that the flaps would not extend beyond 8 degrees. After the landing gear was lowered, the captain told the first officer, in part: "The gear doors are stuck down.... no hydraulics." The captain told the first officer: "Okay, so we're gonna do, this is gonna be a ref and twenty...All right, probably not going to have any brakes..." According to a ATCT specialist in the control tower, the airplane touched down about midway on the 6001-foot long, dry runway. It continued to the end of the runway, entered the overrun area, struck a chain link fence, crossed a road, and struck a building. During a postaccident interview, the captain reported that during the landing roll the first officer was unable to deploy the airplane's emergency drag chute. He said that neither he nor the first officer attempted to activate the nitrogen-charged emergency brake system. The accident airplane was not equipped with thrust reversers. A postaccident examination of the accident airplane's hydraulic pressure relief valve and hydraulic pressure regulator assembly revealed numerous indentations and small gouges on the exterior portions of both components, consistent with being repeatedly struck with a tool. When the hydraulic pressure relief valve was tested and disassembled, it was discovered that the valve piston was stuck open. The emergency drag chute release handle has two safety latches that must be depressed simultaneously before the parachute will activate. An inspection of the emergency drag chute system and release handle disclosed no pre accident mechanical anomalies.

The instrument rated pilot received three weather briefings on the date of the accident from the Miami Automated Flight Service Station. The pilot obtained his IFR clearance while airborne, was advised to climb to 9000 feet mean sea level (MSL), then later advised to descend and maintain 2000 feet, and to fly heading 030 degrees. Radar data indicates that following the instruction from the controller, the airplane made a right descending turn to a southeasterly heading, followed by a left turn to an easterly heading where the airplane was lost from radar while at 2,200 feet mean sea level. The crash was located 138 degrees and .38 nautical mile from the last radar target. Between 1631:04, and 1631:16, the airplane descended from 7,600 to 6,100 feet. Between 1631:16, and the last radar target 12 seconds later at 1631:28, the airplane descended 3,900 feet. Weather radar data indicates the airplane encountered video integrator and processor (VIP) Level 2, or "moderate intensity" echoes in the area of the in-flight loss of control. Approximately 10 and 20 miles east-northeast through southeast of the accident site, maximum echoes of VIP Level 5 to 6, or "intends to extreme intensity" echoes were noted. The strongest reflectivities were located 20 miles east of the accident site. Disintegration of the airplane was noted; there was no evidence of in-flight, or post crash fire of any recovered components. The full span of the left wing, left aileron, left horizontal, and left elevator were accounted for. A section of the right wing and right outboard flap was identified; the right wing was fragmented. Examination of the engine and propellers revealed no evidence of preimpact failure or malfunction. No determination was made whether the pilot met the instrument recency of experience requirement of 14 CFR Part 61.57 (c).

The pilot stated that he and his wife were en route to a medical conference which was to be held aboard a cruise ship that was departing from Fort Lauderdale, Florida, at 1700. He stated that both tanks were full of fuel when he departed the Canton Regional Airport, Canton, Ohio, en route to Fort Lauderdale Executive Airport. According to the pilot, the inboard tanks had been selected for the first hour and a half and the outboard tanks for the following two hours. He said the flight was vectored around thunderstorms, and during the descent, when about 12 miles to the north of Palm Beach International Airport, Palm Beach, Florida, the left engine ceased operating. He said that at this time he noticed that both inboard fuel indicators showed the tanks to be empty, and he switched to the outboard tanks, both of which were shown to be a quarter full. The pilot stated that two minutes later both engines began to surge, and after making an emergency radio communications call, he was advised by the FAA Air Traffic Controller that Tailwinds Airport was located 4 miles to the west. Unable to reach the runway at Tailwinds Airport, the pilot said he made a forced landing in an orange grove. the pilot also said that prior to the accident, there had not been any mechanical failure or malfunctions to the airplane or any of its systems. Examination of the accident site revealed that the airplane had incurred substantial damage, and there was little or no fuel present at the scene. Follow-on examination of the airplane, its fuel system and both engines revealed no anomalies.

On August 12, 2000, about 1115 eastern daylight time, a Beechcraft B200, N3199A, registered to and operated by Great Texas Food Inc. as a Title 14 CFR Part 91 personal flight, ran off the side of the runway during landing in Spanish Cay, Bahamas. Visual meteorological conditions prevailed at the time and a visual flight rules flight plan was filed. The private-rated pilot and the two passengers received no injuries. The flight originated from Fort Lauderdale, Florida, the same day, about 1030. The pilot stated that he made an uneventful landing and as he applied the brakes, the left brake did not respond. He stated that he lost control of the aircraft and exited the runway from the right side and impacted a berm. The right landing gear collapsed, the left wing and the front fuselage incurred substantial damage.

While enroute from Pueblo, Colorado, to Columbia, South Carolina, the captain's windshield delaminated, and the flight diverted to Fort Lauderdale, Florida, for repairs. The flight crew stated the first officer was flying the airplane and had been instructed by the captain to make a firm landing at Fort Lauderdale to get the airplanes weight on the wheels, due to the airplane being light. The landing was firm and the first officer activated the engine thrust reversers. As the nose landing gear touched down, the airplane began veering to the left. Attempts to control the veer to the left were unsuccessful and the airplane ran off the left side of the runway. The airplane then ran over a taxiway and collided with a taxiway sign and the concrete base for the sign. The nose landing gear collapsed and the airplane came to rest. Examination of the runway showed alternating dark and light marks from the left main landing gear tire were present on the runway about 160 feet before marks from the right main landing gear tire are present. Post accident examination of the airplanes landing gear, tires, wheels, bakes, spoilers, and engine thrust reversers, showed no evidence of pre-accident failure or malfunction. At the time of the accident the flight crew had been on duty for about 17 hours 45 minutes.

While on approach to land the left engine surged and lost power. The pilot switched the left engine fuel selector to another fuel tank and the engine restarted. A short time later the left engine surged and lost power again. The pilot switched the left engine fuel selector to the right main fuel tank and the engine again restarted. A short time later the left engine quit again and he shutdown the engine and feathered the propeller. A short time later the right engine surged and lost power. He shut down the right engine and feathered the propeller. He then made a forced landing in a field and during landing rollout the aircraft's left wing collided with a tree. A fire erupted in the left wing area. Post crash examination showed the right main fuel tank was empty. The right auxiliary fuel tank contained 2.5 gallons. The left main fuel tank contained one half gallon of fuel and the left auxiliary tank was ruptured. The pilot operating handbook stated that the main fuel tanks had one gallon unusable fuel and the auxiliary fuel tanks had one half gallon of unusable fuel.

During departure, the rubber connector for the fuel supply line to the right engine oil dilution valve split at the dilution valve on the aft side of the firewall. The engine would not operate unless the electric boost pump was turned on. While returning to the departure airport, a fire erupted in the right wheel after the landing gear was extended. The cockpit filled with smoke during the landing rollout, and the pilot lost directional control do to not being able to see. The aircraft rolled into a canal and came to rest. The split rubber fuel line connector was dry and brittle and did not have any fire damage. No other sources of fuel leakage was found.

Pilot reported level at 6,000 feet; no further transmissions were received. Radar data shows that after 5 minutes at cruise flight ground speed began to slow, and as speed reached 85 knots (VMC is 83 knots) aircraft made a rapid turn to the left and the speed dropped to 74 knots. Radar contact was then lost. Witnesses reported hearing and seeing aircraft with an engine sputtering and quitting, at which time no engine noise was audible. Engine would then restart, and at one point aircraft was observed initiating a climb after engine start. Engine restarted and obtained near full power, and a short time later sound of impact was heard. The left engine fuel servo was found contaminated with corrosion and dirt, and would not allow fuel flow to the engine. The fuel strainer for this engine was installed backwards allowing unfiltered fuel to enter the engine. The left propeller was not feathered and had no signs of rotation under power. Right engine fuel servo also contained corrosion and contamination. The aircraft did not have a current annual inspection. All five occupants were killed.