What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: malfunction or defect report FAA form 8010-4 submitted. On August 7, 1996 at approximately 1630 cdst a Cessna, C172N, N4949G, made an emergency landing in a hay field on county hwy mm, Cadott, chippewa county, Wisconsin. The aircraft did not sustain any damage. The ATP rated pilot and passenger did not report any injuries. The flight originated at meyers field, rippon, Wisconsin with a gas stop at marshfield (mfi) Wisconsin with destination to be flemming field, st. paul, Minnesota. Visual meteorological conditions prevailed. No flight plan was filed. The pilot stated, he experienced a rough running engine at lever cruise flight followed by degraded power output and was unable to maintain altitude. On site evaluation of the engine revealed the magnetos points were not opening due to excessive wear on the point's cam follower. This wear was accelerated by a heat build-up, on the magneto shaft, generated by a failed rear bearing. A malfunction or defect report, FAA form 8010-4, has been submitted pertinent to this part failure.
As the FAA filed it
NARRATIVE: MALFUNCTION OR DEFECT REPORT FAA FORM 8010-4 SUBMITTED. ON AUGUST 7, 1996 AT APPROXIMATELY 1630 CDST A CESSNA, C172N, N4949G, MADE AN EMERGENCY LANDING IN A HAY FIELD ON COUNTY HWY MM, CADOTT, CHIPPEWA COUNTY, WISCONSIN. THE AIRCRAFT DID NOT SUSTAIN ANY DAMAGE. THE ATP RATED PILOT AND PASSENGER DID NOT REPORT ANY INJURIES. THE FLIGHT ORIGINATED AT MEYERS FIELD, RIPPON, WISCONSIN WITH A GAS STOP AT MARSHFIELD (MFI) WISCONSIN WITH DESTINATION TO BE FLEMMING FIELD, ST. PAUL, MINNESOTA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. NO FLIGHT PLAN WAS FILED. THE PILOT STATED, HE EXPERIENCED A ROUGH RUNNING ENGINE AT LEVER CRUISE FLIGHT FOLLOWED BY DEGRADED POWER OUTPUT AND WAS UNABLE TO MAINTAIN ALTITUDE. ON SITE EVALUATION OF THE ENGINE REVEALED THE MAGNETOS POINTS WERE NOT OPENING DUE TO EXCESSIVE WEAR ON THE POINT'S CAM FOLLOWER. THIS WEAR WAS ACCELERATED BY A HEAT BUILD-UP, ON THE MAGNETO SHAFT, GENERATED BY A FAILED REAR BEARING. A MALFUNCTION OR DEFECT REPORT, FAA FORM 8010-4, HAS BEEN SUBMITTED PERTINENT TO THIS PART FAILURE.
Other reports on N4949G · 1
Matched to the same aircraft by N-number and date.