While landing on runway 3, the airplane’s right wing contacted the runway and the airplane landed hard. A weather observation reported at an airport about 18 miles northeast of the accident site, included winds from 320 degrees at 13 knots. The pilot further reported that he conducted an uneventful flight an hour prior to the accident, with the same wind conditions.
Category: Non-Fatal Single-Engine
The airplane initiated a forced landing after a partial loss of engine power during the takeoff initial climb. During the initial run-up the magneto check was not within acceptable limits; however, approximately 15 minutes later the pilot rechecked the magnetos and they were within acceptable limits. The pilot said he configured and checked the airplane prior to takeoff with 10 degrees of flaps and all gages “in the green.”
The pilot landed long beyond his intended touchdown point. He delayed his decision to initiate a go-around. The airplane struck trees at the end of the runway.
After releasing parachutists, the pilot planned to return to the airport. During the descent, about 2,500 feet msl, the engine began to lose power. The pilot thought that carburetor ice caused the power loss, and performed emergency procedures, which included the application of carburetor heat. The engine did not regain power, and the pilot planned an emergency landing to a field.
On the fourth parachute drop flight of the day for the pilot and aircraft, the pilot detected a reduction in elevator control authority on takeoff. He elected to continue the takeoff and climbed to 3,500 feet agl, where he released the two parachutists. On return to the airport, he used power to control his flare, but landed hard and began a porpoise maneuver.
After the pilot dispatched two parachutists, the pilot commenced his descent to return to the airport. While on final approach, approximately 200 feet AGL, the engine lost power. The pilot attempted to land in a nearby open field rather than to attempt maneuvering around high power lines near the airport.
The certificated commercial pilot was conducting skydiving operations in the vicinity of the accident airport. After the airplane climbed to about 11,500 feet msl, all three of the skydivers aboard exited the airplane, and the pilot began a descent to return to the departure airport. The pilot said that while on approach, all engine power was lost, and emergency engine procedures did not restore engine power.
After the sky divers exited the airplane at 12,000 feet, the engine lost power while the airplane was descending through 10,000 feet. The pilot switched fuel tanks and engine power was reestablished. The engine again lost power at 4,000 feet and the pilot attempted a forced landing at his home base airport.
The pilot stated that as the aircraft descended, the engine was operating at 2000 rpm, and the selected manifold pressure was 15 in Hg, and at 8,000 feet he noticed that the engine had ceased operating. Prior to noticing that the engine had ceased operating he said everything had been normal, but as he maneuvered to land he felt he was too far down the runway to land safely, so he elected to perform a go-around.
The airplane nosed over in a cornfield during a forced landing after a total loss of engine power. The pilot reported he released the parachutists at 10,100 feet msl over the drop zone and started the descent to the south due to better cloud clearances and to keep clear of company traffic. He reported that he applied carburetor heat before descending.
The pilot and 21 jumpers were aboard the airplane for the local skydiving flight. The airplane took off to the north on the wet grass runway. Jumpers reported that during the initial takeoff climb, the aircraft assumed a “very steep angle of attack,” and described the pilot “winding the wheel on the lower right side of the chair clockwise, frantically,” and “busy with a wheel between the seats.”
The pilot of the skydiver dropping aircraft reported that the engine lost power at the end of his descent from the 12,000-foot drop altitude as the airplane approached a landing 3-mile base leg. When the engine lost power, he checked that the fuel selector was in the “both” tanks position, the mixture was in the “rich” position, and checked individual magnetos; all with no effect.
The airplane sustained substantial damage on impact with trees and terrain during a forced landing to a field following an in-flight loss of engine power. Skydivers had been dropped prior to the loss of engine power and the pilot reported no injuries. The pilot stated, “I climbed to 11000 [feet.] Was not getting usual climb rate. Before decent found I could not close cowl flaps. Decended to 6000 feet. Noticed eratic raise on manifold gage.
The flight departed with approximately 20 gallons of fuel in each fuel tank and offloaded skydivers at 10,500 feet, then descended to return with the throttle at idle, the fuel/air ratio leaned; and carburetor heat applied. At 2,000 feet, the pilot began to level off and, “realized I was having engine trouble and began my emergency procedures for an engine failure at altitude….”
After discharging three parachutists into a drop zone from about 12,000 feet mean sea level, the pilot attempted to return to the departure airport. The engine began surging as the airplane descended through 8,000 feet. The pilot continued the descent and entered the departure airport’s traffic pattern. He misjudged his distance from the runway, and when all engine power was lost turning onto the final approach leg he was unable to glide to the runway.
The pilot reported that she taxied the aircraft to the grass covered run-up area in preparation for takeoff. As the aircraft moved over the grass, a ‘snapping’ sound was heard and the aircraft ’tilted back and to the right.’ The right wing and right side stabilizer contacted the ground.
Prior to the day of the accident, the pilot had not flown out of the airstrip. During takeoff, the airplane traveled over a ‘soft spot’, and began to veer to the left. The pilot was unable to correct the turn, the airplane went off the left side of the runway and struck a tree. The runway was 1,515 feet long, 110 feet wide, and consisted of soft turf. Review of the pilot’s weight and balance calculations revealed that the airplane was approximately 300 pounds over the maximum gross takeoff weight.
The pilot stated that while descending through 6,000 feet msl, the engine lost power. The pilot reported that when he enriched the mixture, the engine regained power. He stated that he left the mixture full rich; however, when the airplane was at 600 feet and turning to base, the engine lost power again.
During its takeoff roll from a sod runway, the airplane’s pilot said a deer was running toward the airplane from its right side. The pilot said she ‘…throttled back and hit the brakes…[and the airplane] ground looped.’ Ground scars on the runway confirmed that the airplane made a left-hand, 180 degree turn that resulted in a collapsed right main landing gear and the outboard half of the right wing was bent upward about 20 degrees.
While landing, the nose landing gear collapsed, and the airplane went off the left side of the runway. Four bolts secured the nose landing gear. Two of them were missing, and rust was evident in the slots where the bolts were originally secured. The pilot was able to recover one of the bolts. Examination of the bolt revealed that shearing was evident, consistent with a secondary failure.
The pilot reported that after takeoff he saw an approaching thunderstorm and returned to the airport to land on runway 21. The pilot stated that when he arrived at the airport there was a 90-degree crosswind. He estimated that the wind was 120 degrees at 25 knots, with 5-10 knot gusts. The pilot further reported that as the airplane touched down, ‘a gust of wind kept the wheels from settling so I could not brake effectively,’ and the aircraft ran off the end of the 3,000-foot-long runway and impacted a fence and a ditch.
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.
The pilot said he was landing on runway 25 and encountered a dust devil on touchdown. The airplane veered off the runway and into the dirt area beside the pavement, collapsing the right main landing gear.
While climbing through 600 feet after takeoff, a loud bang was heard and a hole appeared in the top of the engine cowling. Oil leaked from the engine and covered the windshield. The engine did not stop running, but did loose power. A forced landing was landing was made in a field and the nose landing gear collapsed during rollout.
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.