Voohries-Larson v. Cessna Aircraft Co.

241 F.3d 707, 2000 WL 33180467
Court of Appeals for the Ninth Circuit·Decided February 22, 2001·No. No. 99-15916·Published·Cited by 57 cases

Opinions

Opinion by Judge BRUNETTI; Dissent by Judge REINHARDT

BRUNETTI, Circuit Judge:

Appellants Linda Voohries-Larson, Betsy Keilen, and Charlene Townsend, the mothers of three individuals killed in the crash of an airplane manufactured by the appellee Cessna Aircraft Company, appeal the judgment entered following a jury verdict for Cessna in their diversity action alleging wrongful death and product liability. Appellants contend that the district court erred in its instructions to the jury regarding superseding cause and wilful and wanton conduct. We have jurisdiction under 28 U.S.C. § 1291, and we dismiss in part and affirm in part.

I.

On July 4, 1993, a twin-engine Cessna airplane crashed in Prescott, Arizona, killing all five people on board. The three men who died in the crash were subsequently identified as Brad Keilen, Tor-rence Voohries, and Ronald Townsend, children of the three appellants. The two women on board, Megan Campbell and Stacy Stephenson, met the men the night of the crash and had accepted an offer to ride in the airplane. Because there were no eyewitnesses to the crash, the wreckage and bodies were discovered after five hours had elapsed.

During the course of the sixteen-day trial, the parties presented starkly different theories as to the cause of the crash. The appellants claimed that the crash was caused by a defect or defects in the Cessna airplane, whereas Cessna claimed the accident was solely due to pilot error and negligence. The jury heard from twenty-six witnesses, including ten experts, and had to analyze the relative merits of two competing accident reconstruction theories.

The appellants presented evidence at trial to prove that the type of airplane in which the decedents crashed, a Cessna T-303, is defectively designed and unreasonably dangerous. This evidence included expert testimony that the T-303’s fuel tank is constructed in a manner that permits air to enter the fuel lines in some circumstances, causing an unexpected interruption in the flow of fuel to an engine despite the presence of fuel in the tank. When the airplane’s rate of turn and angle of bank are not balanced (a condition called “uncoordinated flight”), the construction of the T-303’s fuel tank creates a risk not present with other airplanes. If gravity pushed the fuel outboard, as it would during uncoordinated flight, air would be drawn into the fuel system and interrupt the flow of fuel to the engine. According to the appellants’ theory, the pilot must have flown in uncoordinated flight for at least one minute and forty seconds, the amount of time sufficient to interrupt the flow of fuel. This interruption would then have caused the pilot to shut down the left engine; this, in turn, caused the plane to experience asymmetrical thrust which eventually began a spin to the left from which the plane could not recover.

The appellants supported their theory with a demonstration by an expert witness, in which he filled a T-303 wing tank with 30 gallons of liquid, set the wing (no longer attached to the aircraft) on two sawhorses, tilted it downward and timed how long it would take for the inboard fuel inlets to unport as the liquid ran downhill. The test was performed with 30 gallons of fuel, although the National Transportation Safety Board found the left wing tank of the accident aircraft contained approximately 38 gallons of fuel at the time of the accident. The demonstration had a force of one G, or the force of gravity, operating on the liquid. Cessna repeatedly challenged the demonstration as not representative of what actually occurred in flight.

On cross-examination, the appellants’ expert acknowledged that, not only was flying in uncoordinated flight for the length of time suggested by their demonstration a violation of Federal Aviation Regulations and the Cessna Pilots’ Operating Handbook for the T-303, but also such uncoordinated flight resulting in a 1 G force out[711]*711board would cause the passengers and crew to be pressed toward the left side of the airplane and, if seated on the left side, they would be forced against the bulkhead.

Appellants’ experts further acknowledged that a stall caused by fuel interruption would only affect one engine and that the T303 was designed and certified by the Federal Aviation Administration (FAA) as capable of being flown on one engine. Vo-ohries and Keilen were required to demonstrate their ability to fly and land the aircraft on one engine in order to obtain the pilot certificates they held. Appellants’ experts testified that they knew of no reason why the pilots could not have completed the flight on one engine.

Cessna also presented expert testimony regarding the design of the Cessna airplane. Cessna’s expert conducted a test to disprove the uncoordinated flight theory, in which he actually flew the T-303 in uncoordinated flight for the length of time that the decedents were alleged to have flown it that night, to mimic the forces of actual flight. Cameras were mounted inside the fuel tank showing the fuel inlets and on the cockpit instruments indicating the extent of uncoordinated flight. He also used a force gauge to measure the amount of pressure he placed on the right rubber pedal with his leg in order to achieve and maintain uncoordinated flight. The gauge measured approximately 100 pounds, demonstrating to the jury the unreasonableness of flying the aircraft in this manner.

Cessna also presented the testimony of the primary test pilot for the FAA certification of the T-303. The FAA required certain test flights be performed on the T-303 to demonstrate unusable fuel. During these tests, the FAA mandated that the pilot fly the plane in uncoordinated flight to attempt to intentionally uncover the fuel ports in the wing of the plane. In one demonstration, the aircraft was flown in uncoordinated flight for one minute, then coordinated for one minute, then uncoordinated for one minute, and so on until the first sign of fuel interruption. When fuel interruption occurred, the engine was shut down and the plane returned to the ground on one engine. Then the fuel was measured to determine how much remained. The fuel remaining in the tank, following these tests was .79 gallons, as compared to the 38 gallons in the tank of the airplane at the time of the crash. This evidence demonstrated how extreme the uncoordinated flight would have to have been to unport the fuel inlets with 38 gallons in the tank.

Cessna theorized that the stall was attributable solely to pilot error, due to fatigue and sleep deprivation, alcohol, night flying, the airport environment, failure to wear corrective lenses, and the cockpit circumstances. First, Cessna presented evidence that it could have been either Voohries or Keilen flying the plane, as both men were commercial multi-engine pilots and both had licenses that would allow them to fly a T-303. Although Keilen rented the aircraft and was pilot in command for purposes of FAA regulations, this alone did not mean that Keilen actually piloted the aircraft. The T-303 had dual controls and could be operated from either the left front or right front seats, which were occupied by Keilen and Vooh-ries respectively. Evidence pointed to the possibility that Voohries may have assumed some pilot responsibilities during flight, as one of the horns was broken off on Voohries’ yoke, indicating his hand may have been on it at the time of the crash.

Cessna introduced evidence that showed both Keilen and Voohries had consumed alcohol during the evening prior to the accident.

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Voohries-Larson v. Cessna Aircraft Co., 241 F.3d 707, 2000 WL 33180467 (9th Cir. 2001).

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