Brooks v. Beech Aircraft Corp.

902 P.2d 54, 120 N.M. 372
CourtNew Mexico Supreme Court
DecidedJune 28, 1995
Docket21728
StatusPublished
Cited by47 cases

This text of 902 P.2d 54 (Brooks v. Beech Aircraft Corp.) is published on Counsel Stack Legal Research, covering New Mexico Supreme Court primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Brooks v. Beech Aircraft Corp., 902 P.2d 54, 120 N.M. 372 (N.M. 1995).

Opinion

OPINION

RANSOM, Justice.

As personal representative of her deceased husband, Virginia Brooks brought a wrongful death action against Beech Aircraft Corporation in connection with a 1988 plane crash. In relevant part Brooks sued in negligence and strict liability for an alleged design defect, claiming that the absence of shoulder harnesses caused the death of Thomas Brooks. The trial court granted Beech Aircraft's motion for summary judgment and Brooks appeals pursuant to SCRA 1986, 12-102(A)(1) (Repl.Pamp.1992) (warranty count sounding in contract). We hold that a design-defeet claim may be brought in both negligence and strict liability, and we further hold that such claim may be proved without showing that the manufacturer has violated regulations, codes, or standards applicable to the 1968 plane that crashed. Finding disputed issues of material fact precluding summary judgment on the questions of negligence and unreasonable risk, we reverse and remand.

Facts and proceedings. Thomas Brooks died on August 2,1988, when the 1968 Beech Musketeer he was piloting crashed near Cimarron, New Mexico. Mr. Brooks bought his Musketeer used in 1984. Although his plane was equipped with lap belts, it was neither designed nor equipped with shoulder harnesses. When the Musketeer was designed, manufactured, and sold in 1968, Federal Aviation Administration (FAA) regulations did not require the installation of shoulder harnesses in “general aviation” aircraft such as the Musketeer. Further, no aircraft industry standard or guideline applicable at that time required the installation of such harnesses. The FAA did not adopt a regulation requiring the installation of shoulder harnesses in the front seats of general aviation aircraft until 1977, and this regulation applied only to planes manufactured after July 18, 1978. At no time did the FAA require manufacturers to install shoulder harnesses in older planes.

Brooks filed suit in 1990, claiming that a defect in the Musketeer’s engine had caused her husband’s plane to crash. She also claimed that the absence of shoulder harnesses rendered the plane not crashworthy and that, while not causing her husband’s plane to crash, the absence of shoulder harnesses proximately caused enhanced injury resulting in her husband’s death. At the close of discovery Beech moved for summary judgment on all of Brooks’ claims.

In response to the motion for summary judgment, Brooks presented the deposition of Dr. Richard G. Snyder, a forensic anthropologist who testified that Beech Aircraft had developed a workable shoulder harness as early as 1951. Dr. Snyder also testified that Beech had included shoulder restraints as standard equipment on some of its aircraft before 1968. Finally, stating that he had considered the “state of the art” in 1968 and that he had determined shoulder harnesses were available when Mr. Brooks’ plane was designed and manufactured, Dr. Snyder expressed the opinion that the Musketeer was not crashworthy without shoulder harnesses and that Beech was negligent not to include harnesses in the Musketeer’s design.

The trial court entered summary judgment in favor of Beech on Brooks’ warranty claims, claims of misrepresentation under Restatement (Second) of Torts § 402B (1964), and on Brooks’ claim that an engine defect caused her husband’s plane to crash. Brooks does not challenge these judgments on appeal. The trial court also concluded that enhanced-injury claims sound only in negligence and that negligence in design must be proved by showing the product violated the government regulations or industry standards applicable at the time of design, relying for support on Duran v. General Motors Corp., 101 N.M. 742, 744-49, 688 P.2d 779, 781-86 (Ct.App.1983), cert. quashed, 101 N.M. 555, 685 P.2d 963 (1984). Because the undisputed evidence showed that in 1968 none of the applicable government regulations or industry standards required installation of shoulder harnesses in planes like Mr. Brooks’ Musketeer, the trial court entered summary judgment in favor of Beech on Brooks’ design-defect claims. Brooks appeals.

Design-defect liability. — Crashworthiness. The Eighth Circuit Court of Appeals became the first to adopt the “crashworthiness” theory of liability with the landmark decision of Larsen v. General Motors Corp., 391 F.2d 495, 502 (8th Cir.1968). Reasoning that it is readily foreseeable that an automobile will be involved in an accident and that a user will be injured — often as a result of a “second collision” with the interior of the automobile — the court held that a user may recover damages for enhanced injury if, even though an alleged design defect did not cause the injury-producing accident, the victim can show that the defect proximately caused an injury more severe in degree than would have resulted had the defect not been present. Id.

In Duran our Court of Appeals “join[ed] the majority of jurisdictions in adopting ‘crashworthiness’, ‘second collision’ or ‘enhanced injury’ as actionable.” 101 N.M. at 745, 688 P.2d at 782. Citing a fear that case-by-case adjudication of strict design liability for injuries caused or enhanced by what a jury may determine to be an unreasonable risk would impose hopelessly conflicting design requirements on manufacturers, and noting that Larsen (being a negligence case) refrained from commenting on strict liability, the Court of Appeals held that such claims sound only in negligence. Id,, at 745-47, 688 P.2d at 782-84. “In addition to promoting uniformity, the use of negligence principles [based on extrajudicial standards] would relieve the jury of having to second guess what a proper design should have been.” Id. at 747, 688 P.2d at 784. This case presents us with an opportunity to review the soundness of the Court of Appeals’ determinations.

—Crashworthiness as a subdivision both of design-defect and of manufacturing-flaw liability. The Duran Court ruled that crashworthiness claims sound only in negligence regardless of whether the injury in the second collision was caused or enhanced by a design defect or by a manufacturing flaw. In Duran the injury enhancing defects were both a lack of door header rigidity (design defect) and faulty welds (manufacturing flaw). The death of Thomas Brooks is attributed only to a design defect and the issue before us has been briefed and argued not so much as whether all crashworthiness liability should be limited to negligence, but whether all design-defect liability should be so limited. We see no merit in limiting to negligence the liability of a product supplier for a second-collision injury caused by a manufacturing flaw, cf. Duran, 101 N.M. at 749, 688 P.2d at 786; and we agree with the parties that the real issue here is the proper standard of liability for injuries caused by a design defect regardless of whether those injuries occur in a second collision.

— Policies supporting the limitation of design-defect claims to negligence. Brooks contends that whether a product is alleged to contain a manufacturing flaw or a design defect, the standard by which the supplier’s liability is measured should be the same.

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Bluebook (online)
902 P.2d 54, 120 N.M. 372, Counsel Stack Legal Research, https://law.counselstack.com/opinion/brooks-v-beech-aircraft-corp-nm-1995.