Accident Details
Probable Cause and Findings
was an aborted takeoff not performed by the pilot-in-command. Factors related to the accident were the partial power loss for undetermined reasons and the continued operation of the airplane with a deficiency.
Aircraft Information
Registered Owner (Historical)
Analysis
On January 11, 1994, at 1558 central standard time (CST), a Mooney M20F, N6323Q, registered to Gary Trendler of Geneva, Illinois, and piloted by a private pilot, was substantially damaged during a collision with terrain while performing a forced landing. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 flight was not operating under a flight plan. The pilot reported minor injuries. The flight departed Dekalb, Illinois, at 1530 CST.
The pilot stated N6323Q's engine was "...difficult to start due to the very cold weather... ." Once the engine started, it "...made popping sounds similar to backfiring and had difficulty developing full power." According to the pilot, "This same condition was experienced regularly after the airplane had sat in cold weather for extended periods." He said he ran the engine for approximately ten minutes and shut it down to do a preflight inspection.
N6323Q's engine was restarted without difficulty after completion of the preflight inspection according to the pilot. The pilot stated, "Midway into the takeoff roll the engine began to make a soft popping sound similar to before but not severe." After taking off, the pilot said he decided to return to the airport and land. He said the airplane climbed to approximately 200 feet above the ground "...without any apparent decrease in engine output... ." At that point in the initial climb, the pilot said the airplane began to descend.
As the airplane turned onto the downwind leg, the pilot said he believed the airplane was descending toward a bridge. He stated he turned the airplane to avoid hitting the bridge and "...glided onto the ground."
The on-scene investigation revealed N6323Q's last annual inspection was on January 8, 1989. An examination of the engine "... revealed no abnormalities..." according to the Federal Aviation Administration (FAA) Principal Maintenance Inspector (PMI) representing the NTSB. The engine was test run approximately one-and one-half months after the accident. It started immediately with no hesitation in RPM. Within 30 seconds of the engine's starting, a full power increase was made. The POI observed a smooth increase in power, "... no hesitation or power loss was observed."
N6323Q's fuel tanks had ruptured during the crash sequence. The local fire department had sprayed water on N6323Q's wreckage. The interiors of the fuel tanks were filled with water, ice and snow.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI94LA061