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12 1992 Beech 45 (Beech 18 military) Fatal Fatal Multi-Engine Improper/Poor Maintenance Loss of Aircraft Control

Beech C-45 Fatal (12) Hinckley, IL Sept. 7, 1992

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.

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1992 C-182 Non-Fatal Non-Fatal Single-Engine Undetermined

C-182 Non-Fatal Beeville, TX June 6, 1992

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.

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1992 C-182 Non-Fatal Non-Fatal Single-Engine Preflight

C-182 Non-Fatal Frederick, CO May 10, 1992

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.

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16 1992 DHC-6 Twin Otter Fatal Fatal Multi-Engine Fuel Contamination Preflight

DHC-6 Fatal (16) Perris, CA April 22, 1992

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,

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1992 Beech 18 Loss of Aircraft Control Non-Fatal Non-Fatal Multi-Engine

Beech 18 Non-Fatal Eloy, AZ April 15, 1992

The beech e18s ground looped during the takeoff ground run. The pilot stated that before lift off the airplane encountered a ‘dust devil.’

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1 1992 Barnwell C-182 Collisions Other Fatal Single-Engine SC

C-182 Fatal (1) Barnwell, SC March 21, 1992

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.

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1991 C-182 Loss of Aircraft Control Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Toledo, WA December 28, 1991

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.

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1991 C-182 Non-Fatal Non-Fatal Single-Engine Tail Strike

C-182 Non-Fatal Carlisle, AR December 15, 1991

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.

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1991 C-182 Non-Fatal Non-Fatal Single-Engine Tail Strike

C-182 Non-Fatal Bowling Green, MO November 10, 1991

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.

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1991 C-182 Non-Fatal Non-Fatal Single-Engine Tail Strike

C-182 Non-Fatal Hadley, MA September 29, 1991

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.

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1991 C-182 Fuel Exhaustion Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Titusville, FL Sept. 7, 1991

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.

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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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1991 Beech King Air 90 Non-Fatal Non-Fatal Multi-Engine Tail Strike

Beech 90 Non-Fatal Waynesville, OH July 20, 1991

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

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1991 C-182 Non-Fatal Non-Fatal Single-Engine Tail Strike

C-182 Non-Fatal Hartwood, VA July 14, 1991

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..

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1991 C-210 Non-Fatal Non-Fatal Single-Engine Tail Strike

C-210 Non-Fatal Hazel Green, AL July 13, 1991

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.

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1 1991 C-182 Collisions Other Fatal Fatal Single-Engine

C-182 Fatal (1) Wailua, HI July 11, 1991

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.

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1991 C-182 Fuel Exhaustion Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Farmerville, LA June 13, 1991

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.

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1991 Beech 65 Queen Air Non-Fatal Non-Fatal Multi-Engine Undetermined

Beech 65 Non-Fatal California, MD June 2, 1991

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.

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1991 C-182 Carburetor Icing Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Mead, WA May 16, 1991

At the beginning of a flight for the purpose of dropping parachutists, the pilot reported that everything was normal for the start, taxi, and take off. When the airplane reached an altitude of 150 feet agl, the engine lost power. The pilot set-up for a forced landing in a field with the engine producing partial power and regaining full power, then back to partial power, until touch down. During the landing roll, the airplane collided with a fence. The carburetor icing chart indicates that the flight was being operated in serious icing at cruise and climb power. The pilot had not utilized carburetor heat for the flight.

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1991 C-185 Loss of Aircraft Control Non-Fatal Non-Fatal Single-Engine

C-185 Non-Fatal New Hanover, PA May 12, 1991

During the takeoff on runway 31, the pilot did not maintain directional control, because of the cross wind from the left. The airplane exited the grass runway and struck a ditch. The pilot had 12.6 hours total flight time in the cessna 185c. The wind was reported to be from 200 to 220 degrees at 12 knots.

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1991 C-182 Improper/Poor Maintenance Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Fentress, TX May 4, 1991

Subsequent to the departure of the skydivers, the airplane entered a spiral descent. The jump door, not the sky motive jump door listed on the airplane’s form 337, which had been approved by an faa inspector, entered a flutter condition. The pilot door, windshield and pilot door window separated during the descent. This flutter condition and separation of components resulted in the pilot being unable to control the airplane. Impact occurred in a 20 to 30 degree nose low attitude in approximately a 65 degree left angle of bank.

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1991 C-182 Fuel Exhaustion Non-Fatal Non-Fatal Single-Engine

C-182 Non-Fatal Madera, CA April 12, 1991

Before departing on the initial parachute jumping flight the pilot dipped sticked both tanks and determined that they contained 23 gallons of fuel. The pilot inaccurately calculated that there would be enough fuel to conduct the initial and second flight before fueling would be required. After the parachute jumper departed the airplane on the second flight and during the normal descent to the airport the airplane sustained a total loss of power. The pilot elected to land in a grape vineyard because the airplane’s altitude was insufficient to negotiate the airport. The airplane struck a unmarked transmission wire and crashed during the emergency landing. The airplane contained about 8 gallons of fuel, the unusable amount for all attitudes.

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1991 7 C-182 Collisions Other Fatal Fatal Single-Engine

C-182 Fatal (7) Osceola, WI Feb. 3, 1991

The plts of 2 cessna 182 acft took off from rwy 10 in formation. One of these, n6384a, had 4 skydivers aboard. After takeoff, the plt of n6384a discontinued formation flt & depd to the se, while the otr cessna depd ne. At about the same time, a piper pa-28, n4676r, was apchg the arpt with a dual student & instructor (cfi) aboard. Subsequently, the 2 acft converged & collided about 1-1/2 mi se of the arpt. No known witness saw the collision; the altitude & headings of the acft were not verified. During impact, the 2 acft became entangled & they impacted the ground at the same location. An investigation revealed evidence that the high wing cessna & the low wing pa-28 converged laterally, while on flt paths that angled toward each other.

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1990 2 C-182 Carburetor Icing Fatal Fatal Single-Engine

C-182 Fatal (2) Estacada, OR December 31, 1990

The engine lost power as the pilot made a power reduction shortly after takeoff. During a forced landing in a christmas tree crop, the airplane stalled about 90 ft agl. Investigation revealed that the muffler cones were missing. Witnesses and the pilot stated that the temperature was 40 deg f and the dew point aprx 36 deg. That combination is within the range favorable to induction system icing.

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1 1990 Beech H50 Twin Bonanza Collisions Other Fatal Fatal Multi-Engine

Beech 50 Fatal (1) Snohomish, WA Dec. 15, 1990

During a skydiving operation, the aircraft was slowed to slow cruise flight for a parachute jump. As skydivers were moving to the exit door for a group jump, the d-ring of one skydiver’s reserve parachute became entangled on a protruding cabin door support bracket. The reserve chute deployed & was caught in the slip stream. The skydiver was then pulled from the open door. He impacted the right horizontal stabilizer, fell 4000 ft to the ground & was fatally injured. Most of the right stabilizer was torn from the aircraft. After its separation, the aircraft entered a dive & the remaining skydivers jumped from the plane.

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