Schneider v. Cessna Aircraft Co.

722 P.2d 321, 150 Ariz. 153, 1985 Ariz. App. LEXIS 865
CourtCourt of Appeals of Arizona
DecidedAugust 8, 1985
Docket1 CA-CIV 7172
StatusPublished
Cited by8 cases

This text of 722 P.2d 321 (Schneider v. Cessna Aircraft Co.) is published on Counsel Stack Legal Research, covering Court of Appeals of Arizona primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Schneider v. Cessna Aircraft Co., 722 P.2d 321, 150 Ariz. 153, 1985 Ariz. App. LEXIS 865 (Ark. Ct. App. 1985).

Opinion

OPINION

KLEINSCHMIDT, Judge.

This appeal arises from a jury verdict against plaintiff-appellant in a wrongful death action that arose out of the crash of a Cessna aircraft. The plaintiff is the widow of the deceased pilot. She brought an action against Cessna in strict liability. She also sued Northland Aviation. North-land had trained the pilot and rented the Cessna aircraft to him. Her action against Northland was based on negligence. The case against Cessna centered on the plaintiff’s theory that the airplane was designed in such a way as to make it difficult to drain water from a critical point in the fuel line, and that when the water froze in the line it caused the plane to crash.

The jury returned a verdict in favor of the plaintiff against Northland Aviation, and in favor of Cessna against the plaintiff. This appeal involves only the verdict in favor of Cessna.

The appellant has raised the following issues:

1) Whether the trial court erred in failing to instruct the jury on Cessna’s duty to warn about the potential danger of operating the aircraft in freezing weather;
2) Whether the trial court erroneously admitted a Federal Aviation Administration (FAA) videotape entitled “Stalling for Safety;”
3) Whether it was error for the trial court to admit the following items of evidence:
a) evidence that the Cessna aircraft had a good safety record with few crashes attributable to the accumulation of ice in the fuel system;
b) testimony of certain of Cessna’s expert witnesses whose identities were disclosed to plaintiffs only 28 days before trial;
4) Whether the trial court erroneously precluded the plaintiff from introducing the following items of evidence:
a) an FAA publication circulated in the southwestern part of the United States which warned Cessna operators of the problems of draining water from the fuel system;
b) rebuttal evidence offered by the plaintiff in order to show that the FAA “approval” of the Cessna fuel system was predicated upon an erroneous summary by the FAA of its own data;
c) the formal response of the National Transportation Safety Board to the published call for comment by the FAA which showed problems with the Cessna plane;
d) a Cessna interoffice communication which was purportedly evidence that the FAA withdrew its proposed rule in exchange for Cessna’s installation of a quick drain.

FACTS

On November 27, 1979, Gary Schneider and a friend were killed when their Cessna Model 152 aircraft crashed. As the pilot, Schneider had rented the plane from North-land Aviation, which was in the business of renting and maintaining aircraft. Schneider had previously been trained by North-land.

Schneider rented the plane for the purpose of spotting elk. The two men left the Flagstaff Airport sometime before 7:30 a.m.; the exact time is unknown because there were no witnesses who saw them depart. Around 8:50 that morning, the plane crashed in a clearing eight miles south of Flagstaff.

Shortly before the crash, three eyewitnesses saw and heard the aircraft flying low over a forested area with the engine cutting in and out, heading toward the only clearing in the area. A fourth eyewitness heard a plane with engine trouble and watched it as it circled the clearing once or twice, before it suddenly went into a nose *156 dive. The testimony reveals that Schneider was flying from anywhere between 200 and 500 feet above the ground. All the experts who testified described the plane as having had a stall-spin accident. A subsequent investigation by the National Transportation Safety Board (NTSB) discovered no mechanical malfunctions or defects.

It was appellant’s contention that this particular model, the 152, had a fuel system which was hazardous in freezing weather because it permitted water to accumulate at the lowest point in the fuel system. The water would then freeze and clog the fuel line either by expanding or by moving to a point where it impeded the flow of fuel.

The plaintiff’s experts expressed the opinion that Schneider had a blockage in the fuel line and was trying to get the engine to function while he was circling the clearing. According to the experts, he stalled because of insufficient air speed and went into the ground in a stall-spin.

The ground temperature at the time of Schneider’s takeoff from Flagstaff was 27 degrees Fahrenheit, while the temperature at the time of the crash was 32 degrees.

The plaintiff had three different theories upon which she based her case against Cessna: 1) the defective design of the fuel system; 2) improper instructions as to how to drain water from the fuel line; and 3) Cessna’s failure to warn of the hazards of flying the plane in freezing weather.

To understand the claims and defenses raised on appeal, it is necessary to understand the relationship between the claim against Cessna and the claim against Northland Aviation. The plaintiff’s case against Northland was based on negligent conduct: 1) the negligent failure to properly maintain the plane by draining the fuel system at the fuel line tee-fitting after every 100 hours of flight; and 2) teaching Schneider an improper method of recovering from a stall-spin. As we have already observed, the jury found Northland negligent, but found in favor of Cessna against Schneider. Northland has not appealed.

THE FUEL SYSTEM

The Cessna 152 fuel system, and whether it was defective, is at the heart of plaintiff’s claim against the manufacturer of the airplane. All aviation fuel contains water in small amounts, and there are standard safeguards to avoid the problems it creates. When the water is unfrozen, it is heavier than fuel and it separates and accumulates at the low point in the fuel system. Generally, then, proper safety procedure requires that the fuel system be drained at the low point in the system before flying. A drain is usually provided at the low point in the system to accomplish this. In the model 152, the low point in the fuel system is a tee-fitting which projects about Vi of an inch below the fuselage of the aircraft, where it is exposed to the outside air temperature. If water freezes in the fuel line, it can block or impede the flow of fuel and cause engine failure. Plaintiff’s experts hypothesized that water accumulated at the tee-fitting and formed an ice pellet which loosened during flight due to the heat from the exhaust, bobbed up into the fuel line and impeded the flow of fuel. A partially restricted fuel line results in the engine cutting in and out which is consistent with what witnesses on the ground said they heard.

The plane that crashed did not have a quick drain at the tee-fitting, the low point in the fuel system. As the name implies, a quick drain is a device which permits easy, quick drainage without resort to disassembly of the fuel system. Rather, this airplane had quick drains at three other points in the system: one on each wing fuel tank and one at the “gascolator” or fuel strainer.

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Cite This Page — Counsel Stack

Bluebook (online)
722 P.2d 321, 150 Ariz. 153, 1985 Ariz. App. LEXIS 865, Counsel Stack Legal Research, https://law.counselstack.com/opinion/schneider-v-cessna-aircraft-co-arizctapp-1985.