# Accident 19991018045359A: Cessna 150M, Bunnell, FL, October 18, 1999

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: October 18, 1999, 10:00 local time
- Place: Bunnell, FL
- Damage: Substantial damage
- Phase of flight: Normal Cruise
- Operating rules: General operating rules (Part 91)
- Location: 29.4591° N, 81.2500° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=29.4591&lon=-81.2500&mi=10
- Aircraft: N3240V, registered now (https://openairdocs.org/aircraft/N3240V) (OpenAirDocs)
- Registry model: Cessna 150M (registry code 2071830, https://openairdocs.org/model/cessna-150m) (OpenAirDocs)
- Registry engine: Continental 0-200 series (registry code 17020, https://openairdocs.org/engine/continental-0-200-series) (OpenAirDocs)
- Reported make and model: CESSNA 150M
- Reported engine: CONT O200A
- People aboard: 1
- Fatal injuries: 0
- Pilot flight hours: 368 total, 200 in this make and model, 3 in the last 90 days
- NTSB investigation: [NTSB MIA00LA010](https://openairdocs.org/ntsb/MIA00LA010) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19991018045359A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(.4)DURING CRUISE FLIGHT, THE ENGINE BEGAN TO RUN ROUGH. THE PILOT INITIATED A 180-DEGREE TURN TO RETURN THEN 1-2 MINUTES LATER, THICK WHITE SMOKE WAS 'POURING' FROM UNDER THE LEFT SIDE OF THE INSTRUMENT PANEL IN THE AREA OF THE MAGNETO SWITCH.  ALL ELECTRICAL EQUIPMENT WAS TURNED OFF INCLUDING THE MAGNETO SWITCH.  THE AIRPLANE NOSED UP BRIEFLY AFTER TOUCHDOWN IN A FIELD DURING THE FORCED LANDING.  HEAT DAMAGE TO ELECTRICAL WIRES IN THE ENGINE COMPARTMENT WAS NOTED. THE AFT END PLATE P/N 0450338-18 OF THE RIGHT MUFFLER WAS NOT IN PLACE AND WAS NOT LOCATED; ONLY A PERIPHERAL FLANGE REMAINED.  EXAMINATION OF THE RIGHT MUFFLER P/N 0450400-26 REVEALED PERFORATION OF THE TUBE AND THINNING OF THE MATERIAL NEAR THE FRACTURE SURFACE OF THE END PLATE.  THERE WAS NO RECORD INDICATING THAT THE RIGHT MUFFLER HAD BEEN REPLACED OR REPAIRED SINCE THE AIRPLANE WAS MANUFACTURED.  FOUR DAYS AFTER THE ACCIDENT, THE FAA FOUND A MECHANIC MAKING AN ENTRY IN THE MAINTENANCE RECORDS INDICATING COMPLETION OF AN ANNUAL INSPECTION THAT HE PERFORMED APPROXIMATELY 8 MONTHS EARLIER.  THE MECHANIC REPORTED USING 14 CFR PART 43, APPENDIX D AND HIS OWN CHECKLIST AS A REFERENCE.  THE AIRPLANE HAD ACCUMULATED APPRO XIMATELY 37 HOURS SINCE THE LAST ANNUAL INSPECTION, AND 3,781.4 HOURS SINCE MANUFACTURE, AT THE TIME OF THE ACCIDENT. CESSNA RECOMMENDS INSPECTION OF THE EXHAUST SYSTEM EVERY 50 AND 100 HOURS, AND ALSO A SUBMERGED PRESSURE TEST OF THE MUFFLER WHEN FUMES ARE DETECTED IN THE CABIN OR FOR A THOROUGH INSPECTION.                                                                 (-23)AIRCRAFT MADE EMERGENCY LANDING OFF AIRPORT IN A SOFT WATER SOAKED FIELD AFTER THE PILOT DECLARED AN EMRGENCY FOR A POWER LOSS AND SMOKE IN THE COCKPIT.  THE RIGHT WING LEADING EDGE CONTACTED THE GROUND CAUSING SUBSTAINTIAL DAMAGE TO THE AIRCRAFT RIGHT WING.  THERE WERE NO INJURIES.AN FAA INSPECTION OF THE AIRCRAFT FOUND BURNED AND MELTED WIRE INSULATION BEGINNING AT THE BATTERY CABLES TO THE BATTERY CONTACTER, (CESSNA PART #S1579A-2) AND BEYOND THROUGH THE HARNESS TO THE MASTER SWITCH.  THE CONTACTER INSULATORS WERE DETERIORATED, CRACKED AND MELTED. THE CONTACTER IS ARCHED, AND IS RUSTED AROUND THE LEADS.  THE CONTACTER WAS REMOVED FOR FURTHER TESTING.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA00LA010](https://openairdocs.org/ntsb/MIA00LA010), Oct 18, 1999: Cessna 150M (N3240V), Bunnell, FL, substantial damage. Probable cause: The erosion and separation of the aft end plate P/N 0450338-18 of the right muffler resulting in exhaust gas contact to electrical wires in the engine compartment. Also, unsuitable terrain…

## Other reports on N3240V (1)

Matched to the same aircraft by N-number and date.

- [Incident 19950805032259I](https://openairdocs.org/incident/19950805032259I), Aug 5, 1995: Cessna 150M (N3240V), Wimauma, FL. Engine miss en route. Put on carb heat. Lost power. Landed. Carb heat valve broke in closed position.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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