Andor v. United Air Lines, Inc.

739 P.2d 18, 303 Or. 505
CourtOregon Supreme Court
DecidedJune 23, 1987
DocketTC A8301-00133; CA A32141; SC S33093
StatusPublished
Cited by32 cases

This text of 739 P.2d 18 (Andor v. United Air Lines, Inc.) is published on Counsel Stack Legal Research, covering Oregon Supreme Court primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Andor v. United Air Lines, Inc., 739 P.2d 18, 303 Or. 505 (Or. 1987).

Opinion

*507 LINDE, J.

Plaintiff was a passenger injured in the crash of a United Air Lines plane near the Portland International Airport on December 28, 1978. In her action for compensatory and punitive damages, a jury awarded her $161,275.32 against United Air Lines, Inc. (United) and its pilot, McBroom, in general and special damages, no punitive damages against McBroom and $750,000 in punitive damages against United. Upon United’s motion, the circuit court found insufficient evidence of the degree of “wanton misconduct” required to justify punitive damages and granted a judgment notwithstanding the verdict on that issue. The Court of Appeals reversed the judgment and ordered reinstatement of the punitive damages. Andor v. United Air Lines, 79 Or App 311, 719 P2d 492 (1986). Having allowed United’s petition for review, we reverse the Court of Appeals.

The dispute concerns the propriety of punitive damages on the facts leading to the crash. We quote the summary of the facts from the opinion of the Court of Appeals:

“Flight 173 was scheduled to arrive from Denver at the Portland International Airport at 5:13 p.m. The flight was normal until McBroom extended the landing gear. He described the ‘abnormal extension’ as ‘a heavy to severe jolt-jolt * * *. This was not the normal slow extension, but immediate and was accompanied by a yaw to the right.’ Fearing a problem with the landing gear, McBroom advised the Portland control tower at 5:12 p.m. that the landing would be delayed. The tower advised the crew to proceed to an area southeast of the airport in which the plane could circle while the crew attended to the situation.
“The crew consulted a manual to diagnose the problem. They visually checked a mechanical indicator on the wing, which showed that the landing gear was in a down and locked position. Uncontradicted testimony established that [the] indicator provides an unerring positive indication that the gear is down and locked. McBroom still did not feel confident about the landing gear’s safety, and at 5:40 p.m. he began consulting with ground personnel in Portland and San Francisco. After relating his situation, McBroom was informed ‘You’ve done everything you can do.’ At 5:42 p.m. McBroom reported that the plane had 7,000 pounds of fuel remaining and that he planned to hold for 15 to 20 minutes while the crew prepared the passengers for an emergency evacuation. *508 The San Francisco dispatcher confirmed a 6:05 p.m. landing with McBroom.
“At 5:49 p.m., with the gauges indicating that 5,000 pounds of fuel remained, the low fuel pressure warning lights illuminated. At 5:52 p.m. McBroom confirmed with United personnel in Portland that he would land at 6:05 p.m. with about 4,000 pounds of fuel. At 6:03 p.m. McBroom advised that he would begin his approach in three to five minutes and that the plane had 3,000 pounds of fuel left. At 6:07 p.m. the number four engine flamed out while the plane circled at 5,000 feet. The crew re-started the engine. At 6:13 p.m. two engines flamed out, and McBroom realized that he could not reach the airport. He crash-landed the plane about six miles southeast of the airport at 6:15 p.m.
“McBroom testified that at the time of the accident he thought, because of his training, that the fuel gauges were completely accurate unless they were obviously erratic or inoperative. Subsequent to the crash, he learned that there was an allowable tolerance in the fuel supply indicator system, to the extent of 426 pounds for each of the eight fuel tanks and an additional 1,000 pounds for the totalizer system. That amounts to a total tolerance, or potential inaccuracy of 4,408 pounds. He testified that, if he had known of those tolerance figures at the time of the accident, he would have taken them into account in deciding how long he could safely stay aloft.
“There was evidence that the initial abnormal extension was due to preexisting corrosion in the plane’s landing gear. The parts of the landing gear which were corroded and failed when the gear was extended were the threads of an eyebolt and a piston. They were part of a hydraulic system which had the function of slowing the extension of the landing gear. Plaintiffs uncontradicted evidence shows that United employes were aware of the corrosion problem on DC-8’s in general and on the right landing gear of this plane in particular. United had detected the corrosion by means of a gamma ray inspection and had attempted to seal the connection to retard the corrosion. United stopped the gamma ray inspections in 1977, when it installed a ‘bungee system improvement,’ which ostensibly guaranteed that the landing gear would come down and lock in the proper position if the hydraulic system failed. Although, as we will discuss below, United argues that its maintenance of the landing gear provides no basis for the jury’s award of punitive damages, it does not dispute that its personnel were aware of the corrosion in the parts, that the parts were not replaced and that the corrosion was not cured.”

*509 79 Or App at 313-15, 719 P2d 492.

Defendants did not dispute liability for compensatory damages based on ordinary negligence, but they moved to take plaintiffs claim for punitive damages from the jury. The circuit court denied the motion and submitted the issue to the jury with instructions that it might award punitive damages “only if defendants’ conduct goes beyond mere carelessness to a willful or wanton disregard of risk of harm to others of a magnitude evincing a high degree of social irresponsibility,” that “wanton misconduct is conduct amounting to a deliberate disregard of the rights and safety of others” and “something worse than negligence but less than intentionally hurting someone.” After the jury returned its verdict of punitive damages against United, however, the circuit court granted United’s motion for judgment notwithstanding the verdict, ruling that the evidence left no jury question on punitive damages.

In reversing the circuit court’s ruling, the majority of the Court of Appeals, in banc, stated its disagreement with United’s position and with the dissent in these terms:

“It is well-established that whether a defendant’s conduct is aggravated or wanton or comes within any of the other characterizations that permit the imposition of punitive damages is for the jury to decide, as long as there is evidence upon which the finding can be based. * * * However, * * * the Supreme Court and this court have periodically succumbed to the temptation to make an impermissible independent normative evaluation of the aggravatedness of a defendant’s conduct in the guise of reviewing for evidentiary sufficiency. * * * That is essentially what United asks us to do here, and that is essentially what the dissent does. We decline to do so. Our function is to determine whether the evidence and the inferences, taken at their strongest, rationally support the jury’s finding; it is not our function to make our own assessment of how defendants’ conduct should be characterized.”

79 Or App at 315-16 (citations omitted).

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Bluebook (online)
739 P.2d 18, 303 Or. 505, Counsel Stack Legal Research, https://law.counselstack.com/opinion/andor-v-united-air-lines-inc-or-1987.