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| NTSB Identification: MIA97LA083. The docket is stored in the (offline) NTSB Imaging System. |
| Accident occurred Monday, February 10, 1997 at WESTON, FL |
| Aircraft: Cessna 210L, registration: N115WL |
| Injuries: 1 Uninjured |
| Event: 20001208X07439 Status: Final Report Approved On Monday, August 25, 1997 |
| NTSB Preliminary Narrative (6120.19A) |
| On February 10, 1997, about 0500 eastern standard time, a Cessna 210L, N115WL, registered to Flight Express Inc., was substantially |
| damaged during a forced landing, near Weston, Florida. The commercial-rated pilot was not injured. Instrument meteorological conditions (IMC) |
| prevailed in the vicinity, and an IFR flight plan had been filed. The on-demand, cargo flight was being conducted in accordance with Title 14 CFR |
| Part 135. |
| The flight had departed Opa-Locka, Florida, en route to Tampa, when the pilot heard noises coming from the engine, and elected to make a |
| forced landing, in foggy weather conditions, and impacted in a swampy area. |
| The pilot stated that before departure he performed a preflight inspection. He noted "47 gallons" total fuel onboard, with "22 gallons" in the left |
| wing fuel tank and "25 gallons" in the right wing fuel tank. He stated, "when I found out that the FBO [fixed base operator]...ran out of fuel, I |
| decided to refuel in Tampa since I had plenty of reserve." |
| The flight departed about 0436, and at a location about 25 miles northwest of Opa-Locka, at an altitude of 5,000 to 6,000 feet the pilot said he |
| heard a "thud." He said, "...I realized that I was experiencing a mechanical problem...it seemed at first that I lost a cylinder." He turned southeast, |
| and notified ATC that he was having engine problems. The pilot stated, "my gauges were showing normal indications: 23 inches of manifold |
| pressure, 2500 RPM, 120 pounds of fuel flow." He then attempted to "restart," by "switch[ing] fuel to the left side, turned on [the] fuel pump to |
| prime lines, checked the magnetos on left and right, verified mixture rich, with no re-start successful." |
| On February 18, 1997, the engine from N115WL was test run at the facilities of Certified Engines Inc., Opa-Locka, Florida, under the |
| supervision of the NTSB. The engine was run with all the parts that were on the engine at the time of the accident, with the exception, of the |
| magnetos, and no discrepancies were noted. |
| On March 4, 1997, both magnetos from N115WL's were examined at Continental Motors, Magneto Division, Atlanta, Georgia, under the |
| supervision of the FAA. The magnetos were tested through 3500 rpm, with no discrepancies observed. |
| NTSB Final Narrative (6120.4) |
| After the flight departed, the pilot heard noises coming from the engine and elected to make a forced landing in a swampy area. The pilot stated |
| that before departure he performed a preflight inspection, and had 47 gallons total fuel onboard, with 22 gallons in the left wing tank and 25 |
| gallons in the right wing tank. He elected not to refuel because the FBO had run out of fuel, and decided to refuel at the destination airport since |
| he had 'plenty of reserve.' About 25 miles northwest of the departure airport, at an altitude of 5000 to 6000 feet, the pilot heard a 'thud.' He said, |
| '...I realized that I was experiencing a mechanical problem...it seemed at first that I lost a cylinder.' He turned southeast and notified ATC that he |
| was having engine problems. The pilot stated 'my gauges were showing normal indications: 23 inches of manifold pressure, 2500 RPM, 120 |
| pounds of fuel flow.' He then attempted to restart by 'switch[ing] fuel to the left side, turned on [the] fuel pump to prime lines, checked the |
| magnetos on left and right, verified mixture rich, with no re-start successful.' The engine was test run under the supervision of the Safety |
| Board. The engine was run with all the parts that were on the engine at the time of the accident, with the exception of the magnetos, and no |
| discrepancies were noted. Both magnetos were examined under the supervision of the FAA. The magnetos were tested through 3500 RPM |
| with no discrepancies observed. |
| NTSB Probable Cause Narrative |
| a loss of engine power for undetermined reasons. A factor was thew lack of suitable terrain for the forced landing. |
| 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 |
| Sequence of Events for Occurrence Number: 2 |
| 1 (Finding) WEATHER CONDITION / FOG / (0) |
| Occurrence: 3, IN FLIGHT COLLISION WITH TERRAIN/WATER |
| Phase of Operation: EMERGENCY DESCENT/LANDING |
| Sequence of Events for Occurrence Number: 3 |
| 1 ( Cause ) TERRAIN CONDITIONS / NONE SUITABLE / (0) |
| 2 (Finding) TERRAIN CONDITIONS / SWAMPY / (0) |
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