Mooney M20K accident near Swanton, OH

On May 17, 1994, a Mooney M20K (airplane) was involved in an accident near Swanton, OH. 2 people died. Damage to the aircraft: destroyed.

Date
May 17, 1994
Place
Swanton, OH
Aircraft
Mooney M20K · Airplane
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
41.580°N, 83.891°W
NTSB ID
20001206X01365

NTSB summary

HISTORY OF FLIGHT On May 17, 1994, at 1937 eastern daylight time, a Mooney M-20K, N1007A, owned and piloted by Raymond J. Homa, was destroyed when it impacted trees during a forced landing near the Toledo Express Airport, Toledo, Ohio. The pilot and passenger were fatally injured. Visual meteorological conditions prevailed and a instrument flight rules (IFR) flight plan had been filed for the flight operating under 14 CFR 91. Mr. Homa was the owner of an electronics firm in Atlanta, Georgia, and the passenger was an employee. According to air traffic control records, Mr. Homa obtained a weather briefing from the Macon, Georgia, Automated Flight Service Station (AFSS), and filed an IFR flight plan from Dekalb-Peachtree Airport (PDK), Atlanta, Georgia, to Detroit City Airport (DET), Michigan. Mr. Homa was issued an IFR clearance to DET by the PDK Clearance Delivery, and at 1651 was cleared for takeoff by the PDK Tower. The pilot contacted Atlanta (ATL) departure control and was issued a climb to 11,000 feet, followed by a communications handoff to ATL Center. At 1701, N1007A requested a climb to Flight Level (FL) 190, and 3 minutes later was issued a climb to that altitude. The flight proceeded uneventful with several frequency changes over the next 130 minutes. Cleveland Center issued N1007A a descent to 11,000 feet, followed by a frequency change to the Toledo Approach (TOL) Control. The Toledo controller issued N1007A a descent to 5,000 feet, and a frequency change to another Toledo controller. At 1930:08, N1007A contacted the new Toledo controller and stated, "Ah, Toledo

Probable cause

FAILURE OF AN ENGINE CYLINDER WHICH RESULTED IN THE LOSS OF ENGINE POWER AND THE PILOT'S FAILURE TO ESTABLISH THE PROPER DESCENT PATH TO AN AIRPORT THAT WAS WITHIN THE GLIDE DISTANCE OF THE AIRPLANE. A FACTOR WAS THE OVERGROSS WEIGHT CONDITION OF THE AIRPLANE.

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