The pilot reported that climbing through 550 feet agl, the engine lost power. He lowered the nose of the airplane, established a glide, checked the engine controls and fuel selector, and pulled the carburetor heat control to no avail. At one point, ‘the engine started but would run at a fast idle, and for only a few seconds.’ he conducted a forced landing in a soybean field. Examination of the wreckage revealed no anomalies. During a test in a production test cell, the engine operated normally and produced maximum rated power.
Category: Non-Fatal
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.
The pilot reported that after the airplane reached an altitude of 10,500 feet msl, the skydivers exited the airplane. The pilot stated that he then began a wings-level, high-rate descent to stay clear of the drop zone. The mixture was at full rich and the carburetor heat was applied as he maintained 150 to 160 knots indicated airspeed.
The pilot lost control of the tailwheel equipped airplane while attempting to land on runway 18 with a crosswind from 290 at 19 knots, gusting to 37. The airplane ground looped and the left wing spar was damaged when the wing impacted the ground.
Two airplanes were converging head-on while taxiing on the same east-west taxiway. The pilot of the cessna 182 was taxiing east and saw the tailwheel equipped great lakes 2t-1ak (biplane) ‘s-turning’ on the taxiway. She assumed the biplane pilot saw her aircraft.
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.
The airplane was descending for a landing when the engine suffered a total loss of power. The pilot stated that he had no memory of the accident. Although personnel who moved the airplane claimed that 15 or 16 gallons of fuel were removed from the accident airplane at the accident scene, only about six gallons could be located.
The airplane took off with four parachutists on board. After reaching an altitude of 11,000 feet, one parachutist exited the airplane. As the second parachutist was exiting, his reserve parachute deployed pulling him toward the rear of the airplane. The parachute canopy went over the top of the horizontal stabilizer and the parachutist went under the stabilizer.
The aircraft was damaged when a sport parachutist collided with the horizontal stabilizer while exiting the aircraft at 13,000 feet msl. According to statements from the pilots and other jumpers on board the aircraft, the injured jumper’s reserve parachute deployed as he exited the door. The parachute momentarily draped over the left leading edge of the horizontal stabilizer,
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.
AFTER FUELING THE AIRCRAFT, THE PILOT OBSERVED ‘A LOT’ OF WATER IN THE FUEL, WHEN CHECKING THE SUMPS. HE SHOOK THE WINGS, AND AGAIN OBSERVED WATER. HE ALLOWED THE AIRCRAFT TO SIT FOR ABOUT AN HOUR, THEN HE CHECKED THE SUMPS AGAIN. HE DRAINED WATER UNTIL NO MORE WATER WAS OBSERVED. AT ABOUT 200 FEET AGL, DURING THE INITIAL CLIMB, THE ENGINE QUIT.
The pilot was performing the initial takeoff, when he observed a loss of power, associated with a torque indication of zero. He force landed the aircraft in a wooded area when he could not make an open field. A post accident inspection of the engine revealed that the fuel control unit arm was loose, and the lock wire was not in place.
The 81-year-old pilot was flying to the glencoe municipal airport to pick up parachutists. The glencoe airport has a grass runway. The pilot landed in a grass field one-half mile south of the airport. Witnesses reported the pilot circled the field before landing. The airplane struck a fence post and nosed over during landing roll.
On final approach to runway 14, a total loss of engine power occurred. Due to construction equipment, transmission lines, and vehicle traffic on a highway, the pilot made a decision to land in a field. During the landing in rough and uneven terrain, the nose gear, left main gear, and left wing were damaged. The pilot reported 15 gallons of fuel at the initial preflight.
A student sport parachutist was preparing for a static line jump. The parachute inadvertently deployed as he was moving into jump position, outside of the airplane. Canopy static lines caught on the horizontal stabilizer, twisting the empennage.
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.
The pilot was conducting a local skydiving flight. During the climb, both engines began to operate intermittently. The pilot instructed the parachutists to bail out at 9,000 feet msl and returned to the airport. The pilot failed to use carburetor heat during the descent. The pilot applied power to both engines while on final approach, but got no response.
During sport parachute operations the aircraft inadvertently stalled when too many jumpers attached themselves on the outside of the aircraft. The jumpers had been briefed on limiting the number to exit at one time to six; however, they ignored these instructions. As they departed the aircraft the pilot regained control and landed without further incident.
The private pilot and four parachutists were on board the airplane as it taxied for takeoff. The wind conditions were reported between 14 and 16 knots. The pilot stated that he added full power, achieved flying speed, rotated, and began to climb out.
The aircraft departed fully topped with 65 gallons of fuel on three 45 nautical mile minimum legs plus a total of five parachute drops involving ascents between 7,500 and 9,500 feet above ground level. During the descent from the fifth parachute drop the engine stopped developing power and the pilot in command executed a forced landing in a field. During the landing roll the aircraft collided with a barb wire fence and impacted a drainage ditch.
The airplane was at 8000 feet, four parachutist had jumped, and the pilot then descended the airplane to the pattern altitude of 1,400 feet. During this descent, carburetor heat was not applied. The pilot then initiated the approach and landing to runway 19. During the approach the pilot applied carburetor heat twice for short periods of time. On final approach the pilot needed additional power to reach the runway.
Shortly after takeoff, both engines lost power. The pilot said he selected different fuel tanks, but could not restart the engines. He subsequently made a wheels-up forced landing in a field below his flight path. The pilot stated that he had performed a preflight inspection and that there was 4.1 gals in both the front left and right main fuel tanks. Examination of the airplane after the accident revealed a combined total of about 5 gals in the forward left and right tanks.
The pilots were completing a parachute/orientation flight. After the parachutists exited, the airplane, with the first pilot at the controls, returned to the airport, descending at the maximum descent rate. The second pilot, a company check pilot, reported that the first pilot touched down simultaneously on the nose and right main landing gears at a high airspeed. The airplane subsequently swerved to the left and struck a bush located about 150 feet from the runway centerline and nosed over.
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.
The airplane was being used to haul skydivers. According to the pilot, after about the third or fourth flight, there was a partial loss of power, due to a fuel tank vent that had been blocked by a mud dauber nest. The pilot noted that when a fuel cap was removed, he heard a ‘hiss’ as differential air pressure was relieved. Maintenance was performed to clear the vent, then the pilot continued hauling skydivers.