Joy v. Bell Helicopter Textron, Inc.

999 F.2d 549, 303 U.S. App. D.C. 1, 1993 U.S. App. LEXIS 19063
CourtCourt of Appeals for the D.C. Circuit
DecidedJuly 27, 1993
DocketNos. 91-7128, 91-7129 and 91-7168
StatusPublished
Cited by174 cases

This text of 999 F.2d 549 (Joy v. Bell Helicopter Textron, Inc.) is published on Counsel Stack Legal Research, covering Court of Appeals for the D.C. Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Joy v. Bell Helicopter Textron, Inc., 999 F.2d 549, 303 U.S. App. D.C. 1, 1993 U.S. App. LEXIS 19063 (D.C. Cir. 1993).

Opinion

Opinion for the court filed by Circuit Judge BUCKLEY.

BUCKLEY, Circuit Judge:

This case arises out of a 1987 helicopter crash in which all three passengers were killed and the pilot, Jack Turley, was seriously injured. After the crash, the passengers’ survivors and Mr. Turley brought suit in district court against Allison Gas Turbine [4]*4Division of General Motors Corporation (“Allison”), the manufacturer of the helicopter’s engine. Allison, in turn, sought contribution from the District of Columbia for its handling of the attempted rescue, and from Mr. Turley for alleged negligence in flying the helicopter. Prior to trial, the court granted the District’s motion for summary judgment on the ground that the “public duty doctrine” rendered the District immune from liability for the actions of the police officers who participated in the rescue effort. A trial was then held, at the conclusion of which the jury returned verdicts for the plaintiffs against Allison. The jury also determined that Mr. Turley was not negligent; accordingly, the court entered judgment in favor of Mr. Turley on Allison’s contribution claim.

Allison now appeals these judgments. Its claims of error may be divided into three categories. First, Allison argues that a retrial on liability is warranted because the district court improperly admitted certain evidence and issued erroneous jury instructions. Second, Allison contends that the district court erred by granting judgment in favor of Mr. Turley and the District on the contribution claims. Finally, it asserts that the damages award to plaintiff Linda L. Joy should be reversed because the district court improperly permitted the jury to award damages for loss of consortium and failed to exclude “speculative” expert testimony concerning her late husband’s earning capacity.

Finding no fault in the district court’s evidentiary rulings or its jury instructions, we affirm the jury’s verdict that Allison is liable to the plaintiffs. We also affirm the judgment that Mr. Turley was not negligent in piloting the helicopter, and hence is not liable for contribution. We reverse and remand, however, the damages award to Ms. Joy. Finally, because the question whether the District may be held liable presents a novel issue of D.C. law, we will certify this question to the D.C. Court of Appeals.

I. Background

A. The Crash

At approximately 7:30 A.M. on August 21, 1987, a helicopter crashed into the Potomac River in Washington, D.C. The aircraft came to rest upside down and partially submerged. Jack Turley, the pilot, freed himself from the wreckage and was rescued almost immediately by civilians on the scene. The three passengers — Victoria N. Hinckley, Robert A. Joy, and William Weems — remained inside the helicopter.

A number of people in the area observed the crash and placed emergency calls to notify the District’s Metropolitan Police Department. In response, the Department immediately dispatched a boat from its Harbor Patrol unit. The boat arrived at the site within approximately three minutes of the crash. Unfortunately, however, the officers on board, at least one of whom was a certified police diver, did not have their scuba diving equipment with them. As a result, they left the scene of the accident to retrieve the equipment.

While the Harbor Patrol officers were gathering their equipment, other Harbor Patrol officers and members of the D.C. Fire Department secured the crash scene. Allison offered an affidavit of a civilian scuba diver who stated that she was present at the scene and had access to diving equipment. She told the officers that she wanted to rescue the passengers, but the officers ordered her not to do so. A second eyewitness reported that “three or four qualified scuba divers” arrived in a boat and offered their assistance. They, however, were also ordered to stay out of the water. Still another eyewitness stated that he began to put on his scuba diving equipment when he saw the crash, but stopped when the Harbor Patrol arrived.

Eventually, the Harbor Patrol divers returned with their gear and commenced rescue operations. The witnesses reported that more than twenty minutes had elapsed between the time of the crash and the time the officers were prepared to dive. Although the police divers were able to remove the passengers from the helicopter, all of them died later in the day. According to Allison’s medical expert, Dr. Michael Baden, the passengers did not die from injuries caused by the impact of the crash, but rather from being submerged for an extended period of time.. [5]*5Dr. Baden testified that if the passengers had been removed within the first ten minutes after the crash, they would have had a greater than 50 percent chance of survival. Dr. Baden also stated that if the passengers had been submerged for more than ten minutes but less than fifteen, it would have been possible, but unlikely, that they would have survived.

B. The Cause of the Crash

The parties agreed that the helicopter engine lost power because a critical part, the spur adapter gearshaft (“SAG”), failed. The SAG, along with its mating part, the compressor coupler adapter, connects the turbine (power producing) section of the engine to its compressor (air intake) section. The failed SAG was a replacement part manufactured by Allison in 1982 and installed in the engine that year. The SAG had an anticipated useful life of 3,500 hours, but it failed after 1,450.7 hours in service.

Plaintiffs contended that the SAG failed because it had been improperly “carburized” (i.e., hardened) during manufacturing, as shown by an unusual “microstructure” (grain pattern) in the part. By contrast, Allison argued that the SAG failed because (1) the SAG and the compressor coupler adapter had been misaligned during an overhaul by a third party, and (2) foreign material in the engine’s oil system blocked the flow of oil through the jet that provided lubrication to the forward spline of the SAG.

In addition to the controversy over the underlying cause of the SAG failure, the parties also disputed whether negligence on the part of Mr. Turley, the pilot, contributed to the crash. A helicopter can be safely landed in the event of an engine failure by performing a maneuver called an “autorotation.” The altitudes and airspeeds from which a safe autorotation can be performed are set forth in what is known as a height velocity (“HA7”) diagram. If, however, a helicopter is flown within a particular region of the HA7 diagram (the “restricted area”), it is extremely difficult to land the helicopter safely in the event of a power failure.

There is little question that, at the time the helicopter lost power, Mr. Turley was flying at an altitude of approximately two hundred feet. The HA7 diagram indicates that at that altitude a helicopter’s airspeed should be no less than 43 miles per hour. Allison, however, presented eyewitness testimony designed to show that Mr. Turley was flying at a slow airspeed, or perhaps even hovering. Accordingly, Allison claimed that Mr. Turley’s negligent piloting was the cause of the crash.

In response, Mr. Turley contended that he was adhering to Federal Aviation Administration restrictions that required him to fly below 200 feet along a specified helicopter route to avoid commercial air traffic coming in and out of National Airport.

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Cite This Page — Counsel Stack

Bluebook (online)
999 F.2d 549, 303 U.S. App. D.C. 1, 1993 U.S. App. LEXIS 19063, Counsel Stack Legal Research, https://law.counselstack.com/opinion/joy-v-bell-helicopter-textron-inc-cadc-1993.