McGee v. Cessna Aircraft Co.

82 Cal. App. 3d 1005, 147 Cal. Rptr. 694, 82 Cal. App. 2d 1005, 1978 Cal. App. LEXIS 1737
CourtCalifornia Court of Appeal
DecidedJuly 20, 1978
DocketCiv. 14920
StatusPublished
Cited by17 cases

This text of 82 Cal. App. 3d 1005 (McGee v. Cessna Aircraft Co.) is published on Counsel Stack Legal Research, covering California Court of Appeal primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
McGee v. Cessna Aircraft Co., 82 Cal. App. 3d 1005, 147 Cal. Rptr. 694, 82 Cal. App. 2d 1005, 1978 Cal. App. LEXIS 1737 (Cal. Ct. App. 1978).

Opinion

Opinion

STANIFORTH, J.

Helen M. McGee sought damages from John Hedger and Cessna Aircraft Company for personal injuries she sustained in the crash of a 1968 model 177 Cardinal Cessna aircraft. The aircraft was manufactured by Cessna and owned by Hedger. McGee settled her claim, dismissed her complaint, as to defendant Hedger before commencement of the trial. As to the remaining defendant Cessna, McGee asserted two theories of liability. First, McGee charged negligence in the design of the aircraft and second design defects of the aircraft renders Cessna strictly liable for injuries caused proximately thereby. More specifically, McGee asserted the fuel system of the aircraft was inherently unsafe; Cessna designed, installed near the cockpit an “accumulator” of gasoline intercepting its flow from the storage tanks in the wings to the carburetor and the engine in the nose of the plane.

McGee complains that Cessna knew the nosewheel strut was susceptible to deformation either in a crash or due to rough handling; the nosewheel strut collapsed, telescoped, upon impact and ruptured the accumulator tank, permitting fuel to escape in an area where combustion would and did in fact occur, thus causing the second accident—a post-crash fire. Cessna denied the allegations and raised the affirmative *1008 defenses of contributory negligence, assumption of risk and misuse of the product. The jury returned a verdict in favor of defendant Cessna. After denial of her motion for a new trial, McGee appealed.

Facts—The Crash

McGee was injured in a crash of the Cessna aircraft which occurred shortly after the aircraft left the ground on takeoff from Warner Springs Airport, San Diego County, March 28, 1971. Four persons were seated in the aircraft at the time of the crash. McGee was in the left front seat; Hedger, the owner of the plane, was in the right front seat; Dorothy Watts and Virginia Renn occupied the two rear seats. Each occupant wore a seat belt; however, no shoulder harnesses were provided in the aircraft.

The weather was clear; the aircraft took off on an easterly course of travel. After a short period of flight, the plane made a left turn to go in a northerly direction. After the turn the aircraft crashed on the hilly terrain. After the aircraft came in contact with the ground, the front of the aircraft burst into flames. The flames quickly entered the cockpit area under the control panel, burned on the left front side of the cockpit, and then spread throughout the entire aircraft.

The two women in the rear seats remained conscious during and after the impact. No occupant suffered major injuries on the original crash. However, McGee and Hedger were rendered unconscious when thrown forward during the crash. The conscious, rear seat passengers quickly evacuated the burning aircraft and pulled the unconscious Hedger and McGee from the burning wreckage.

McGee was the last to be removed from the aircraft and by the time she was extricated, she had suffered extensive third degree burns over both her legs. These burns were of such severity as to require amputation of her right leg three inches below the knee joint and the left leg six inches below the hip joint. McGee’s injuries are almost entirely the result of the post-crash fire.

Facts—The Trial

To support her claim of defective or negligent design of the Cessna aircraft relating to its performance and handling characteristics, as well as its crashworthiness, McGee relied upon the testimony of three expert *1009 witnesses: Norman Horton, formerly associated with the University of Southern California; Dr. James Turnbow of Arizona State University; and Michael Antoniou, a test pilot. Defendant Cessna relied upon the testimony of three other expert witnesses: Prof. Karl Bergey of the University of Oklahoma; Dr. John Swearingen, a retired Federal Aviation Administration employee; and Mr. Bill Robinson, a test pilot, currently employed by Piper Aircraft Company.

Mr. Antoniou testified to numerous deficiencies in the design of the subject aircraft as it relates to its performance and handling characteristics; however he was unable to establish a causal connection between these defects and the crash. Mr. Horton and Dr. Turnbow testified to design defects in the Cessna aircraft as it relates to crashworthiness—the incineration potential after a relatively minor initial crash. Each opined such deficiencies were a proximate cause of McGee’s injuries, though they did not contribute to the original cause of the crash.

Concerning the crashworthiness issue, Horton and Turnbow testified the Cessna 177 aircraft had a fuel system which operated primarily on a gravitational flow principle. Specifically, the fuel in the aircraft was contained in the wings which were affixed to the top of the aircraft fuselage. A fuel line then carried the fuel through a fuel selector valve: This valve could be operated by persons in the cockpit so fuel can be taken from the right wing, the left wing or both at the same time. However, this valve cannot be positioned so as to stop the flow of fuel through the fuel lines as it does not have an offposition.

From the fuel selector valve, the fuel line then proceeds to a fuel reservoir tank, identified during the trial as the “accumulator” tank. This tank is located on the passenger side of the firewall separating the passenger cockpit from the engine compartment. It rests immediately in front of the feet and legs of both the pilot and co-pilot controlling the aircraft. The top of the accumulator tank is part of the floor of the cockpit and is made of thin aluminum sheet metal. The fuel line proceeds from the accumulator through a shut-off valve located on the firewall into the carburetion system of the engine of the aircraft.

The Cessna aircraft had a nonretractable nosewheel attached to the aircraft by means of a tubular metal strut. The nosewheel mechanism and attachments are in the immediate proximity of the engine of the aircraft and specifically the carburetion system on the engine. The same strut and attachments are also in immediate proximity to the firewall separating the *1010 engine compartment from the cockpit and in fact attach near the fuel accumulator tank.

The aircraft had, as standard equipment, lap type seatbelts but did not have shoulder harness as part of the standard equipment present when the aircraft was originally manufactured and sold.

Horton and Turn bow opined when the aircraft struck the ground, it was in substantially level flight and under control. As a result of sliding along the ground the nosewheel strut collapsed dislodging the carburetor and rupturing the accumulator tank. The escaping fuel contacted various sources of ignition in the engine compartment and the fire, the second accident, occurred. They further testified because of the nature and design of the fuel system of this aircraft, all of the fuel in the tanks was available to feed the fire.

On behalf of Cessna expert witness Robinson testified the handling and performance characteristics of the Cessna aircraft were as specified in the Cessna flight test data and in conformity with applicable Federal Aviation Regulations. Prof. Bergey and Dr.

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Cite This Page — Counsel Stack

Bluebook (online)
82 Cal. App. 3d 1005, 147 Cal. Rptr. 694, 82 Cal. App. 2d 1005, 1978 Cal. App. LEXIS 1737, Counsel Stack Legal Research, https://law.counselstack.com/opinion/mcgee-v-cessna-aircraft-co-calctapp-1978.