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.
Category: Severity
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.
A commercial pilot was returning to land after dropping parachutists in the local area. While on short final, the airplane impacted a fence, nosed over, and came to rest in the inverted position. The operator stated that the airplane encountered a downdraft created by a hangar adjacent to the runway. The wind at the nearest observation facility, eight miles north of the site, was from 300 degrees at 6 knots.
The pilot stated after the third parachute jumper exited the aircraft, he ‘…Continued at reduced power and started to glide down…For landing. As i was starting a long final approach i saw that i would need power to maintain the glide slope. There was no response when i advanced the throttle.’ attempts to restart the engine were unsuccessful and the pilot made a forced landing.Â
After takeoff, the airplane was seen at low altitude trailing smoke from the left engine. Witnesses saw the wings ‘tipping’ back and forth, then a wing dropped and hit the ground. Examination revealed that a supercharger bearing had failed in the left engine. The left engine had been recently installed by non-certificated personnel after being inactive for 18 yrs without preservation.
During a vfr final approach, following a parachute jumping flight, to a private airstrip the engine lost all power. The pilot made a forced landing into a field. The owner/operator reported that the flaps remained in the up position at the accident site and that the pilot had stated the flaps remained in the up position during the approach and landing. The manufacturers’ procedures list full flaps for a shortfield landing. During the flare/touchdown the nose gear collapsed and the airplane came to rest in an inverted position. The cause of the power loss was not determined.
During takeoff roll while hauling parachute jumpers from a private airstrip, the aircraft failed to become airborne, departed the runway and collided with a ditch. The aircraft came to rest upright partially extending onto a country road which bordered the airstrip. Weight of the aircraft was computed to be 250.5 pounds over maximum certified gross weight.
The ground loader had fueled the airplane from the airport fuel truck. He stated that the flight crew did not sump the fuel tanks after they were fueled. Immediately after takeoff the right engine lost power, the right wing lowered to about 90 deg, and the airplane impacted the ground adjacent to the runway. Then forward fuel tank, which provides fuel to the right engine, was found to contain about 8 gals of a heavily contaminated mixture composed of water,
The beech e18s ground looped during the takeoff ground run. The pilot stated that before lift off the airplane encountered a ‘dust devil.’
The pilot had taken a newlywed couple up on a ceremonial ‘mile high’ local pleasure flight as a wedding gift. He reported that during a maneuver he felt a ‘shudder’, and elected to make a low pass over an airport taxiway, by some friends on the ground with a hand-held radio, for a ‘landing gear check’. During the second pass the pilot asked the couple to ‘look to the right where the moon shines over barnwell.’ the airplane collided with a spectator on the taxiway. A pax stated that the pilot then ‘freaked out’ and was in no condition to fly the airplane. During a subsequent landing attempt, a pax prevented a go-around by forcing the yoke forward and pushing on the brake pedals with his hands. The pax stated the pilot ‘wanted to keep flying and he was going nuts.’ the pilot fled the scene after the accident but returned later. The pilot had arranged to have the people on the ground ‘moon’ the airplane during the low pass.
After the parachutists exited the airplane, the flight returned to the airport and entered the downwind leg at 750 feet. Flaps were extended and when turning to final approach, the pilot stated that the airplane encountered a high sink rate. Before the pilot could correct the situation, the airplane collided with 20 foot tall trees approximately 300 feet short of the runway.
During a daytime flight, maneuvering at 8,500 feet msl, a parachute jumper exited the airplane to position on the right wing strut in preparation for the jump. The jumper’s reserve parachute inadvertently opened and the jumper was pulled from the strut and impacted the leading edge of the right horizontal stabilizer bending the spar. The airplane landed safely without further incident.
Pilot was flying a group of sport parachutists on a jump run, and noticed a pilot parachute out of its pack. The pilot yelled at parachutist but he stepped onto the aircraft wing strut. The parachute deployed and pulled the parachutist off the strut. The parachute became momentarily entangled with the horizontal stabilizer. The pilot landed the aircraft safely. The parachutist landed safely.
With the door open and preparing to jump, a skydiver had premature deployment of his main parachute. He jumped out the door and his parachute became entangled in the elevator of the airplane. The pilot said the airplane pitched down and the other skydivers immediately exited the airplane. The skydiver whose parachute was entangled with the tail, cut away his parachute and used his reserved chute for landing.
Engine quit on final approach while returning from dropping parachutists. A forced landing was made in a field and the aircraft collided with a ditch on rollout. Post crash examination of the aircraft by faa inspectors indicated the left fuel tank contained one pint of fuel and the right fuel tank contained 1 gallon of fuel. Aircraft information indicated 1.5 gallons of fuel is unusable in each tank. The engine operated normally after the accident and there was no pre or post crash fuel leakage from the aircraft.
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.
As the jumpmaster and student jumper backed into the door of the airplane in preparation for a tandem jump, he had a uncommanded deployment of his reserve parachute, that dragged them out the door. The jumpers went under the left horizontal stabilizer while the canopy went over the top. After a few seconds, the parachute shroud lines cut through the horizontal stabilizer and deformed the left elevator
As the first parachutist was preparing to jump from the wing at an altitude of 12,000 feet, his reserve parachute release handle became attached to some part of the airplane. Before he could react, the parachute opened and pulled him from the wing. The partially deployed chute wrapped around the right horizontal stabilizer, slamming him against the aircraft. The right stabilizer broke away and the jumper descended to a safe landing under the deployed canopy..
The pilot lost control of the airplane after a parachute line from a student jumper became entangled with the horizontal stabilizer and elevator trim tab. According to the pilot, the airplane became uncontrollable and entered a flat spin. Unable to arrest the spin, the pilot and other jumpers parachuted out the airplane; the airplane crashed in the woods unattended.
The flight was in level cruise and 3 of the 4 jumpers were positioned on the step ready to jump. The reserve chute on one of the jumpers accidently deployed and was sucked forward and over the right wing leading edge. The jumper was pulled forward and over the wing, and in the process, hit his head on the wing leading edge and substantially damaged the internal wing structure. As the jumper’s chute deployed over the wing, the aircraft was rolled inverted. The other jumpers jumped and parachuted to the ground safely.
The airplane had departed the airport on a local area flight in order to drop two skydivers. After the departure of the parachutists a total loss of power was experienced during approach. The airplane collided with 60 foot high pine trees one half mile from the approach end of the runway. Subsequent investigation revealed that the left tank was empty; the right tank contained approximately 11 gallons, and the fuel selector handle was missing.
The pilot reported that shortly after takeoff on a parachute jumping flt the left engine lost power, but a second later power was restored. Soon afterwards a total power loss occurred. According to the pilot, the propeller stopped rotating and did not windmill. He did not feather the left propeller. He made a shallow left turn toward an open field, while trying to return to the airport. He was unable to maintain adequate airspeed or altitude, and in order to maintain aircraft control, he reduced power on the right enggine. He made a forced landing in a wheat field. The airplane came to a stop and all occupants escaped the airplane before it caught fire. The examination of the airplane did not disclose evidence of mechanical malfunction.