Casualties unknown

2004-12-25: Cessna 150C (N7857Z) — East Moriches, NY

East Moriches, NY, US

On December 25, 2004, a Cessna 150C (registration N7857Z) was involved in an aviation accident near East Moriches, NY. Investigators recorded the probable cause as: Several mechanical deficiencies which either independently or collectively resulted in a subsequent loss of engine power. A factor in the accident was the obstruction in the forced landing area. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane experienced a partial loss of engine power after departing Spadaro Airport in East Moriches, New York. The pilot attempted to restore power using carburetor heat but executed a forced landing on a road and then a field, where it struck an obstruction and nosed over, resulting in substantial damage.

Accident Details

The accident occurred during departure from Spadaro Airport (1N2) in East Moriches, New York. Shortly after takeoff, the airplane's engine experienced a partial loss of power. The pilot attempted to regain full power by activating the carburetor heat control, but the effort was unsuccessful. Consequently, the pilot performed a forced landing on a road. The airplane bounced upon initial contact and subsequently touched down in an adjacent field. During the rollout in the field, the airplane struck an obstruction and nosed over, sustaining substantial damage.

Post-Accident Examination

Following the accident, investigators examined the wreckage. The fuel tanks were found to be nearly full, and fuel drained from the system showed no signs of contamination. An examination of the engine was conducted, revealing that crankshaft and camshaft continuity was confirmed. The magnetos produced spark at all spark plugs. A differential pressure test was performed, during which air could be heard discharging at the oil filler/crankcase breather. Cylinders #1 and #3 exhibited readings below the specified leakage limits. An internal inspection of those cylinders revealed heavy carbon deposits on both the cylinder heads and valves. Additionally, wear was visually observed on the cylinder walls, and both rod end bearings exhibited excessive play. The airplane had received an annual inspection 55 flight hours prior to the accident, and the engine was 164 flight hours short of the recommended overhaul time.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041229X02040. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.