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| NTSB Identification: MIA97LA224. The docket is stored in the (offline) NTSB Imaging System. |
| Accident occurred Friday, August 01, 1997 at CAPE CORAL, FL |
| Aircraft: Cessna 152, registration: N93011 |
| Injuries: 1 Uninjured |
| Event: 20001208X08702 Status: Final Report Approved On Friday, April 10, 1998 |
| NTSB Preliminary Narrative (6120.19A) |
| On August 1, 1997, about 0802 eastern daylight time, a Cessna 152, N93011, registered to Alternative Flying Club Inc., operated by Fort Myers |
| Airways, as a 14 CFR Part 91 instructional flight, experienced a reported loss of engine power in cruise flight, and crashed during a forced |
| landing in the vicinity of Cape Coral, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was destroyed |
| by a postcrash fire. The student pilot reported no injuries. The flight originated from Page Field, Fort Myers, Florida, about 42 minutes before the |
| accident. |
| According to personnel on duty at Page Field Control Tower N93011 departed from runway 5 at about 0720. At about 0801, the pilot informed |
| them that he was 5 miles south of the airport and seemed to be losing power. The tower operator asked the pilot to ident on the transponder, |
| and asked what was the nature of his emergency. The pilot stated he was losing power and altitude. The pilot was instructed to proceed direct |
| to the airport and asked to verify that he did not have an instructor pilot on board the airplane. The pilot stated at 0801:59, "I dont have an |
| instructor, " followed by " 011 I dont know." There was no other recorded conversation with the pilot. |
| Examination of the airframe and flight control system revealed no evidence of a precrash mechanical failure or malfunction. Continuity of the |
| flight control system was confirmed for pitch, roll, and yaw. |
| The engine assembly was shipped to the engine manufacture for further examination in the presence of the FAA. Textron Lycoming concluded |
| that, "The engine disassembly did not reveal any precrash anomalies or discrepancies that would indicate that this engine was not capable of |
| running and producing power prior to the accident." For additional information see Textron Lycoming Accident Investigation Engine Disassembly |
| Report. |
| The engine assembly and accessories were released to Mr. Donald Carter, President, Alternate Flying Club Inc., on September 30, 1997. |
| NTSB Final Narrative (6120.4) |
| The pilot was in cruise flight between 1,000 feet to 1,200 feet when he experienced a partial loss of engine power followed by a total loss of |
| engine power. He made a forced landing to the only available forced landing area which was nonsuitable. The airplane collided with wires and |
| terrain and a postcrash fire ensued. Examination of the airframe and flight controls revealed no evidence of a precrash mechanical failure or |
| malfunction. Disassembly of the engine assembly revealed no precrash anomalies or discrepancies that would indicate the engine was not |
| capable of running and producing power before the accident. |
| NTSB Probable Cause Narrative |
| Loss of engine power for undetermined reasons resulting in a forced landing to unsuitable terrain. |
| Occurrences and Sequence of Events |
| Occurrence: 1, LOSS OF ENGINE POWER |
| Phase of Operation: CRUISE |
| Sequence of Events for Occurrence Number: 1 |
| 1 ( Cause ) REASON FOR OCCURRENCE UNDETERMINED / / |
| Occurrence: 2, FORCED LANDING |
| Phase of Operation: EMERGENCY DESCENT/LANDING |
| Occurrence: 3, IN FLIGHT COLLISION WITH OBJECT |
| Phase of Operation: EMERGENCY DESCENT/LANDING |
| Sequence of Events for Occurrence Number: 3 |
| 1 ( Factor ) TERRAIN CONDITIONS / NONE SUITABLE / (0) |
| 2 (Finding) OBJECT / WIRE,TRANSMISSION / (0) |
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