Fort Lauderdale-Executive

The airplane had not flown since June 1989. The flight had made 2 high speed taxi operations before takeoff. Immediately after takeoff the flight called to land. The airplane was observed on downwind 200-800 feet agl, 15-25° nose high. The airplane then stalled. The compressor surge valves for the left and right engines were found in the open position. Both occupants were killed.

On June 20, 1990, at 04:51 Atlantic standard time (AST), a Piper PA-31, YV2200P, registered to and operated by Juan A. Zeley, crashed near New Town, Andros Island, Bahamas, while on a business flight from Fort Lauderdale, Florida, to Caracas, Venezuela. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The Venezuelan registered airplane was destroyed. The pilot, the sole occupant of the airplane, who held a Venezuelan commercial pilot certificate was fatally injured. The flight originated at Fort Lauderdale Executive Airport, Fort, Lauderdale, Florida, on June 20, 1990 at 04:05 AST.

While level after descending, the right engine quit. Pilot feathered the propeller, advised ATC, and was diverting to alternate when left engine quit. He positioned the left engine boost pump to high and low with negative results, but did not feather the propeller. Position of boost pumps, when engines quit, was not determined. Aircraft landed on overpass that was under construction. There was fuel leakage after accident due to aircraft damage. Fuel quantity was sufficient. Examination of aircraft revealed right engine flexible duct from turbocharger to plenum chamber separated due to loose clamp. Hose was installed and club prop installed for each engine run. Both engines operated normally. Induction air hose was pulled during right engine run. Engine ran rough due to excessive rich mixture. No determination could be made for the reason of the left engine power loss.

The pilot reported to ground personnel at Fort Lauderdale that he was experiencing an avionics problem and the passenger entry door was sprung the day before when it was slammed; however, the pilot elected to depart. The aircraft wreckage was located on June 19 in the Everglades near Coral Springs, Florida. The aircraft impacted in a nose low attitude. Wreckage was scattered over an area 211 feet long by 55 feet wide. Investigation revealed no preimpact mechanical malfunctions/failures. The pilot, sole on board, was killed.

After takeoff from Staniel Cay Airport, while climbing, the twin engine aircraft went out of control and crashed in the sea. All three occupants were killed.

The flight departed Fort Lauderdale, FL, on 8-2-84 at approximately 0815 edt for Cincinnati, OH. The aircraft wreckage was found on 11-17-84 on an up slope of big Fodderstack Mountain. The aircraft had contacted a 25 feet tall tree located 200 feet west of the main wreckage. The only known radio contact was recalled by the Monroe County airport manager who stated the pilot radioed to exchange the day's greeting. Exact weather at the accident site could not be determined. However, the airport manager recalled the high terrain being obscured with poor visibility. Both occupants were killed.

The aircraft disappeared from radar coverage while in cruise flight at 10,000 feet msl near Orangeville, FL. The ATC transcript revealed that the pilot had been inquiring about the weather ahead of him and was cleared to descend to 6,000 feet in order to get below strong headwinds. One minute later he transmitted that he was going to stay at 10,000 feet because he did not have any choice (strong turbulence). His last transmission stated the weather was getting worse. The aircraft has not been located.

The aircraft crashed while maneuvering at low airspeed and altitude right after takeoff. The pilot said the left engine started losing power intermittently at 90 knots. The pilot had rotated the aircraft and tried to continue the takeoff. He was cleared to land on any runway and in attempting a turn with landing gear and partial flaps extended control was lost and a crash occurred. The aircraft flight manual states that if an engine fails below 105 mph the takeoff should be aborted. An on scene examination revealed no evidence to suggest a pre-impact failure or malfunction. Both propellers showed evidence of torsional overload damage. When the engines were further examined the left engine fuel strainer was partially clogged with dirt. During a run-up test the left engine would not develop more than 23 inches hg. At 2,750 rpm and magneto rpm drop was erratic. The engine would not run with the aux fuel boost pump off. The reason for the low power output was a disconnected pressure line for the turbocharger which appeared to have been disconnected for some time. All five occupants were injured, two of them seriously.

The aircraft crashed at night near a private strip in marginal weather conditions. The gear was found in the up position, the right engine was broken off, the nose section was crushed back to the windshield, and both propellers were bent and twisted. About 1,300 lbs of marijuana was found on board.

On a night approach to Claxton-Evans County (Clayton) Airport, both engines flamed out due to fuel exhaustion. The aircraft lost height and while the pilot was attempting an emergency landing, the airplane struck trees and crashed. Both occupants were seriously injured.