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NTSB Identification: MIA99LA135. The docket is stored in the (offline) NTSB Imaging System.

Accident occurred Tuesday, April 20, 1999 at S. ROCKLEDGE, FL

Aircraft: Cessna 150M, registration: N66560

Injuries: 1 Serious



Event: 20001205X00536 Status: Final Report Approved On Friday, March 31, 2000



NTSB Preliminary Narrative (6120.19A)



On April 20, 1999, about 1600 eastern daylight time, a Cessna 150M, N66560, registered to Brittania Flight Center, Inc., operating as a 14 CFR

Part 91 instructional flight, crashed while attempting an emergency landing, following a loss of engine power near Rockledge, Florida. Visual

meteorological conditions prevailed and no flight plan was filed. The airplane received substantial damage and the student pilot, the sole

occupant, sustained minor injuries. The flight originated from Winter Park, Florida, about 1 hour before the accident.



According to eyewitnesses, the airplane engine's sound lessened and stopped completely. The engine sounded quiet as the pilot appeared to

look for a landing area. The airplane crashed in a residential area.



According to the student pilot, he was flying his solo cross-country flight from Winter Haven's Gilbert Airport to Cocoa's Merritt Island Airport.

About 10 miles west of Merritt Island, he radioed Merritt unicom for traffic advisories and to relay his intentions. He stated he was in cruise flight

at 1,800 feet msl, 2,300 (engine rpm), and mixture leaned "appropriately". Immediately after his radio transmission, he noticed an uncommanded

reduction in engine rpm, and a loss of power. He got no response to increasing his throttle setting, so he began emergency procedures for an

engine failure, except that he does not remember using carburetor heat. His two options for a forced landing site were a road or a field. The

road contained too much traffic and the field was ringed by high tension wires and contained playing children.



According to an FAA inspector, the airplane struck a tree and came to rest in the front yard of a private residence on its side, right wing up.

The FAA inspector could not estimate the amount of fuel aboard, but stated the left tank contained enough fuel that the fuel line and vent line had

to be plugged to prevent spillage when the wing was removed. The gascolator and carburetor contained fuel. Fire rescue personnel

responding to the accident mentioned they sandbagged the storm sewer drain to prevent a "significant amount" of fuel from entering the storm

drain. The carburetor squirted fuel through the venturi when the throttle linkage was manually pumped. The airplane was equipped with properly

vented fuel tank caps. Testing of fuel for water content was negative. Disassembly examination of the engine and its components revealed no

mechanical failures or malfunctions. Aircraft records revealed an appropriate supplemental type certificate (STC), for automotive fuel use. The

spark plugs and combustion chambers exhibited abnormally dark coloration, and it is the FAA inspector's opinion that the coloration is the result

of, "..a fuel rich mixture which would be consistent with carburetor icing".



Reference to carburetor icing charts reveals that an ambient temperature of 24 degrees C and a dew point of 9 degrees C, as reported by

Titusville (TIX) and Melbourne (MLB) for the time period of the accident, would put the flight's probability within the region labeled, "visible icing at

glide and cruise power." A copy of the chart is included in this report under, "Other Pertinent Forms and Reports".



NTSB Final Narrative (6120.4)



The student pilot stated he was nearing his destination on the first leg of his solo cross-country, still in cruise flight, when the engine suddenly

lost power. He stated that he performed the procedures for engine failure, but does not remember using carburetor heat. He did not regain

engine power, and was forced to make an emergency landing in a residential area, sustaining minor injuries and substantially damaging the

airplane. Examination of the aircraft, engine, fuel system, and all components by an FAA inspector revealed no failures or malfunctions. The

temperature and dew point reported by a station 15 miles from the accident would have put this flight within the region labeled, 'visible icing at

glide and cruise power' using carburetor icing probability charts.



NTSB Probable Cause Narrative



A total loss of engine power while in cruise flight due to the pilot's failure to use carburetor heat during carburetor icing conditions and the

subsequent emergency landing to unsuitable terrain and collision with a tree.



Occurrences and Sequence of Events

Occurrence: 1, LOSS OF ENGINE POWER(TOTAL) - NONMECHANICAL

Phase of Operation: CRUISE



Sequence of Events for Occurrence Number: 1

1 (Finding) WEATHER CONDITION / CARBURETOR ICING CONDITIONS / (0)

2 (Finding) FUEL SYSTEM, CARBURETOR / ICE / (0)

3 ( Cause ) CARBURETOR HEAT / NOT USED / PILOT IN COMMAND



Occurrence: 2, FORCED LANDING

Phase of Operation: EMERGENCY DESCENT/LANDING



Occurrence: 3, IN FLIGHT COLLISION WITH OBJECT

Phase of Operation: EMERGENCY LANDING



Sequence of Events for Occurrence Number: 3

1 (Finding) TERRAIN CONDITIONS / NONE SUITABLE / (0)

2 (Finding) TERRAIN CONDITIONS / RESIDENTIAL AREA / (0)

3 (Finding) OBJECT / TREE(S) / (0)


 

 

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