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1999 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Tecumseh, MI August 11, 1999

The aircraft was landing on runway 36 when the right main landing gear separated. The aircraft departed the right side of the runway and came to rest. The pilot and passenger were not injured. Inspection revealed a fracture of the right spring landing gear leg about one inch outobard of the fuselage skin.

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1999 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal East Troy, WI Feb. 21, 1999

The pilot stated that after four parachutists had boarded the airplane, he began to taxi away from the gate. The pilot stated that the airplane traveled about 25 yards on the upward sloping grass terrain when the right main landing gear collapsed. Examination of the landing gear revealed a break approximately 10 inches from the inboard end of the landing gear leg at a point where it is clamped to the fuselage structure.

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1998 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Independence, MO May 19, 1998

The pilot reported that as the airplane was descending through 4,000 feet msl it started loosing power. She leveled off, pulled carburetor heat on, and switched fuel tanks. She reported that, ‘Upon restart the engine backfired and quit.’ She reported that she trimmed the airplane for best glide (80 mph) and flew directly for the airport 2.5 miles away. At .5 miles from the airport she realized she would not make the runway so she decided to land short.

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1997 Beech 65 Queen Air Mechanical Failure Non-Fatal Non-Fatal Multi-Engine

Beech 65 Non-Fatal West Jordan, UT April 19, 1997

The pilot stated that after parachutists egressed from the airplane, he returned to the airport and found that he did not have a green down-and-locked indication for the left main landing gear. He stated that he executed emergency procedures and did two fly-bys over the runway. Ground personnel stated that the landing gear appeared to be down-and-locked.

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1995 Beech 65 Queen Air Mechanical Failure Non-Fatal Non-Fatal Multi-Engine

Beech 65-B80 Non-Fatal Anderson, IN August 20, 1995

Directional control of the aircraft was lost during the takeoff roll. The aircraft skidded sideways, veered off the runway into an agricultural field and both main landing gear assemblies collapsed.

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1995 Helio H-250 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

Helio H-250 Non-Fatal Clarkson, NY May 18, 1995

The pilot departed on a local flight with three passengers. The engine start, taxi, and initial takeoff were normal. As the airplane flew over the end of the runway at 50 to 75 feet, the engine lost power.

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1994 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Worthington, PA Oct. 15, 1994

The pilot was returning from a skydiving drop when he entered the airport traffic pattern, experienced an inflight loss of control, and then struck trees short of the runway.

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1994 C-170 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-170 Non-Fatal Bushnell, FL April 26, 1994

The commercial pilot was about 50 feet agl on initial takeoff climb when the airplane started to vibrate and the engine started running rough. The pilot determined that he could not clear trees at the end of an open field and made a forced landing straight ahead maneuvering around some trees and cattle. The pilot stated he flared a little high, landed hard and the right main landing gear separated.

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1 1993 C-182 Fatal Fatal Single-Engine Mechanical Failure

C-182 Fatal (1) East Moriches, NY August 14, 1993

The passengers(parachutists) reported that after the airplane became airborne they heard ‘backfiring’, a ‘bang’ and ‘….Saw white smoke…’ the jumpmaster reported that the engine quit after the airplane turned downwind. The airplane continued to lose altitude on downwind and during the turn to the runway. It crossed the approach end of the runway at a 45-deg angle and dragged a wing on the runway, coming to rest next to the runway.

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1993 DC-3 Improper/Poor Maintenance Mechanical Failure Non-Fatal Non-Fatal Multi-Engine

DC-3 Non-Fatal Zephyrhills, FL April 20, 1993

The pilot stated that on initial climb, at about 400 ft agl, the crew smelled something burning, followed by light smoke in the cabin. Both engines appeared normal visually. The odor and smoke increased, and the left fire warning light illuminated. The left engine was shut down & the prop feathered. The pilot increased power on the right engine; however, the airplane would not climb or maintain airspeed.

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1991 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Jenkinsburg, GA July 20, 1991

The airplane had landed following a sport parachute flight. During the landing roll the nose wheel separated from the strut. The nose strut dug into the sod runway & the airplane nosed over inverted. An faa inspector examined the airplane & noted that the nut & bolt which secured the nose wheel was absent. It was not located. He stated that there was no evidence that the bolt had broken. No maintenance to the nose wheel had been recorded recently, & the last annual inspection was logged 8 months & 72 flight hours before the accident.

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1987 C-180 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-180 Non-Fatal Carlton, MN December 5, 1987

The plt rprtd that the left main gear collapsed as he started to taxi from the ramp area on a smooth grass surface. When the gear collapsed, the left wing dropped to the ground & was substantially dmgd. The plt rprtd the left gear leg had broken off 2 inches ‘inside the bulkhead.’ an exam of the broken part revealed it had failed from fatigue.

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1985 C-182 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Forest City, IA July 20, 1985

Shortly after the acft took off with 4 skydivers on board, its eng seized at an alt of about 300 to 400 ft. The plt selected the best available area to land which was a field of tall corn on rolling terrain. During the emerg landing, the acft nosed over. Later, the eng was disassembled & aprx 1 qt of finely ground ferreous material was found deposited in the lower oil pan. The main bearings were found scored & discolored, & the main bearing shells showed evidence of overheating. The connecting rods were also discolored from heat. The screen chamber of the oil pump was found full of ferrous metal which shut off the oil supply to the oil pump gears. The faa maint inspector who examined the eng stated that the ferrous material found in the eng & bottom pan was not from the eng. The source of the material was not determined.

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1983 C-206 Turbo-Charged C-U206 Mechanical Failure Non-Fatal Non-Fatal Single-Engine

C-TU206 Non-Fatal Loveland, CO October 23, 1983

The acft lost part of one blade of the propeller during the climb to cruise phase of operation. The passengers were skydivers so they used their parachutes in an exit of the acft as the airframe started to vibrate. The plt made a successful landing on the arpt without power. All the jumpers landed safety. Visual examination of the propeller showed that the blade had separated 10 to 12 inches outboard from the blade root. The fracture exhibited evidence typical of high cycle fatigue and overload stress.

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