Boyle v. United Technologies Corp.

792 F.2d 413, 1986 U.S. App. LEXIS 25322
CourtCourt of Appeals for the Fourth Circuit
DecidedMay 27, 1986
DocketNo. 85-2264
StatusPublished
Cited by15 cases

This text of 792 F.2d 413 (Boyle v. United Technologies Corp.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Fourth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Boyle v. United Technologies Corp., 792 F.2d 413, 1986 U.S. App. LEXIS 25322 (4th Cir. 1986).

Opinion

PER CURIAM:

David Boyle drowned after the Marine helicopter he was flying crashed in the Atlantic Ocean. Boyle’s father, Delbert Boyle, on behalf of himself, Boyle’s mother and three sisters, sued the Sikorsky Division of United Technologies Corporation (hereinafter “Sikorsky”), the manufacturer of the helicopter. Boyle alleged negligence [414]*414and breach of warranty in the design of the co-pilot’s escape hatch and the rework of the helicopter’s control system.

The jury found for plaintiffs. Sikorsky moved for a judgment notwithstanding the verdict, arguing that the military contractor defense shielded it from liability for the alleged design defect, and that plaintiffs had failed to establish Sikorsky’s responsibility for the malfunction of the control system. The district judge denied Sikorsky’s motion.

We reverse and remand with directions to enter judgment for defendant.

I.

On April 27, 1983, a Marine helicopter manufactured by Sikorsky (a CH-53) crashed in the ocean off the coast of Virginia Beach. The four crew members survived the impact. Three of them escaped through emergency exits, but the co-pilot, David Boyle, did not escape, and drowned.

At trial, plaintiffs attempted to show that Sikorsky had defectively repaired the pilot valve of the helicopter’s servo. The servo acts as a sort of power steering to assist the pilot in flying the plane. After the accident, a small chip of wire was found in the pilot valve. Plaintiffs argued that the chip caused the servo to stop functioning, the pilot lost control of the helicopter, and the helicopter crashed into the water.

The metal chip could have been introduced at one of three times: when Sikorsky overhauled the helicopter in late 1981 — early 1982; when the Navy reworked it in late 1982; or during maintenance of the hydraulic system by the Marines. The parties agree that it is least likely that the servo was contaminated during maintenance. Plaintiffs contended at trial that the chip was most likely introduced by Sikorsky.

Plaintiffs also contended that Sikorsky had defectively designed the co-pilot’s escape hatch. Specifically, plaintiffs alleged that when the collective, one of the control sticks, was pulled full up, it interfered with the co-pilot’s access to his escape hatch.

The jury, in a general verdict, found for plaintiffs and awarded them $725,000. Because we believe the military contractor defense precludes any recovery for the design defect, and because there was insufficient evidence to conclude that Sikorsky was the party that introduced the chip, we reverse the decision below.

II.

A military contractor can escape liability for a design defect if it can demonstrate that 1) the United States is immune from liability; 2) the United States approved reasonably precise specifications for the equipment; 3) the equipment conformed to those specifications; and 4) the supplier warned the United States about dangers in the use of the equipment that were known to the supplier but not to the United States. Tozer v. LTV Corp., 792 F.2d 403 (4th Cir. 1986).

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792 F.2d 413, 1986 U.S. App. LEXIS 25322, Counsel Stack Legal Research, https://law.counselstack.com/opinion/boyle-v-united-technologies-corp-ca4-1986.