Loftleidir Icelandic Airlines, Inc. v. McDonnell Douglas Corp.

158 Cal. App. 3d 83, 204 Cal. Rptr. 358, 1984 Cal. App. LEXIS 2290
CourtCalifornia Court of Appeal
DecidedJuly 3, 1984
DocketCiv. 68831
StatusPublished
Cited by5 cases

This text of 158 Cal. App. 3d 83 (Loftleidir Icelandic Airlines, Inc. v. McDonnell Douglas Corp.) 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
Loftleidir Icelandic Airlines, Inc. v. McDonnell Douglas Corp., 158 Cal. App. 3d 83, 204 Cal. Rptr. 358, 1984 Cal. App. LEXIS 2290 (Cal. Ct. App. 1984).

Opinion

*87 Opinion

JOHNSON, J.

This appeal arises out of the crash of a DC-8 airplane operated by plaintiff, Loftleidir Icelandic Airlines, Inc. (Loftleidir), and manufactured by defendant, Douglas Aircraft Company, Inc. (Douglas). The jury returned a verdict in favor of Douglas. Loftleidir appeals raising two claims of error, both relating to trial court orders excluding evidence.

Loftleidir first argues the trial court erred by excluding evidence of three of the six prior airplane accidents Loftleidir sought to have admitted at trial. In the unpublished portion of this opinion we hold that although evidence of those accidents was relevant the trial court could properly exclude it under Evidence Code section 352.

Loftleidir also argues the court erred by excluding the testimony of one of its expert witnesses. The court excluded the testimony on the ground it was prohibited by 49 Code of Federal Regulations, section 835 et seq. Those regulations govern the permissible scope of a National Transportation Safety Board (NTSB) employee’s testimony. In the published portion of this opinion we hold exclusion of the expert’s testimony was prejudicial error. The federal statute prohibits introducing into private litigation evidence of the NTSB’s opinions about the probable cause of an airplane accident. Since Loftleidir’s expert did not investigate the subject accident while employed by the NTSB there was no chance his testimony would reveal the prohibited matter.

I. Statement of Facts and Proceedings Below

On June 23, 1973, a 1966 model DC-8 airplane operated by Loftleidir crashed while on approach to John F. Kennedy International Airport in New York. The accident occurred because the pilot prematurely extended the ground spoilers 1 when the airplane was about 30 feet above the runway. There were no deaths among the 119 passengers and 9 crew members, but 2 stewardesses and 36 passengers were injured. 2 The crash also resulted in heavy damage to the aircraft.

Loftleidir filed this action against Douglas for property damage and loss of use on June 2, 1976. On August 27, 1981, the case proceeded to trial on *88 theories of strict liability and negligence. 3 Loftleidir’s primary contention was the DC-8 should have been designed to preclude in-flight deployment of the ground spoilers. If premature extension of the ground spoilers had been impossible the accident would not have occurred. According to Loftleidir, Douglas was negligent and/or strictly liable for designing a system capable of in-flight deployment.

Much of the testimony at trial concerned the design history and operation of the ground spoiler system on DC-8 airplanes. The DC-8 was originally designed with what was labeled at trial as the Mark I anti-skid system. Although the ground spoilers were not designed to perform any in-flight function, the Mark I system was capable of in-flight deployment. However, in order to deploy the spoilers in-flight, the crew would have to overcome 65 to 70 pounds of resistance in order to move the spoiler handle. When the plane was on the ground there was only about nine pounds of resistance to overcome in order to move the spoiler handle.

In 1962 the Mark II anti-skid system was introduced to improve some of the features of the Mark I system. As a result of design changes, however, Douglas reduced the amount of resistance to overcome in order to move the spoiler handle in-flight from 65 pounds to 35 pounds. The Mark II design also required the addition of an electric actuator to the spoiler system. If on takeoff the actuator did not coast to the full retract position, or if after takeoff the actuator received a spurious signal, the pilot would encounter only nine pounds of spring resistance before the spoiler handle could be moved in-flight.

There were no accidents involving in-flight deployment of the ground spoilers before 1962 while DC-8’s were equipped with the Mark I anti-skid system. However, the record in this case reflects six accidents or incidents involving DC-8’s equipped with the Mark II system. Each of the accidents was caused in some form or fashion by the in-flight deployment of ground spoilers.

Three of the six accidents were caused, as in this case, by crew members inadvertently deploying the ground spoilers. The fourth and fifth accidents were caused by an electrical malfunction which in turn caused deployment of the ground spoilers. The cause of the final accident was in dispute. The trial court ruled evidence of the three accidents where crew members de *89 ployed the spoilers was admissible. However, the court excluded most of the evidence related to the three other accidents.

On August 4, 1981, Douglas filed another motion in limine, this time to exclude the testimony of Charles O. Miller, one of Loftleidir’s expert witnesses and a former employee of the NTSB. Douglas argued Miller’s testimony was prohibited by 49 Code of Federal Regulations, section 835.7. That statute sets forth the permissible scope of testimony of former employees of the NTSB.

Loftleidir intended to call Miller, an expert on human factors and safety engineering in aviation, and the president and principal consultant of System Safety Incorporated, as its primary expert witness. Miller was to testify extensively regarding the design of the ground spoiler system from an engineering and human factors standpoint. Miller also intended to testify with respect to Douglas’ duty to anticipate and to react to safety problems which developed during the design and service life of the DC-8.

Miller was the director of the Bureau of Aviation Safety at the time of the accident. The Bureau of Aviation Safety is responsible for investigating aircraft accidents for the NTSB.

On August 27, 1981, the court indicated it was inclined to permit Miller’s testimony provided no reference was made to the opinions contained in the NTSB report of the Loftleidir accident or to Miller’s former status as director of the Bureau of Aviation Safety. However, after additional argument by Douglas, the court reserved its ruling until an evidentiary hearing could be held. The hearing was held on September 4, 1981, one week after the trial began. After the hearing, the court again reserved its ruling asking for additional argument by counsel. This argument was heard on September 8, 1981, after which the court granted Douglas’ motion to exclude Miller’s testimony.

On September 24, 1981, after approximately three weeks of trial, the jury returned a verdict in favor of Douglas on both the strict liability and negligence counts. In answer to interrogatories the jury found the DC-8 was not defective and Douglas was not negligent.

Judgment was entered in favor of Douglas on September 25, 1981. On November 12, 1981, Loftleidir’s motion for a new trial was denied. Loftleidir filed a timely notice of appeal.

*90 *

II.

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Cite This Page — Counsel Stack

Bluebook (online)
158 Cal. App. 3d 83, 204 Cal. Rptr. 358, 1984 Cal. App. LEXIS 2290, Counsel Stack Legal Research, https://law.counselstack.com/opinion/loftleidir-icelandic-airlines-inc-v-mcdonnell-douglas-corp-calctapp-1984.