37 Fed. R. Evid. Serv. 225, prod.liab.rep. (Cch) P 13,373 Four Corners Helicopters, Inc., a Colorado Corporation Jenny R. Paton, as Surviving Spouse and as Personal Representative of the Estate of William Paton, Deceased v. Turbomeca, S.A., a French Corporation, and Societe Nationale Industrielle Aerospatiale, a French Corporation Aerospatiale Helicopter Corporation, a Delaware Corporation Avialle, Inc., a Delaware Corporation Roberts Aircraft, Inc., an Arizona Corporation

979 F.2d 1434
CourtCourt of Appeals for the Tenth Circuit
DecidedNovember 17, 1992
Docket91-1295
StatusPublished

This text of 979 F.2d 1434 (37 Fed. R. Evid. Serv. 225, prod.liab.rep. (Cch) P 13,373 Four Corners Helicopters, Inc., a Colorado Corporation Jenny R. Paton, as Surviving Spouse and as Personal Representative of the Estate of William Paton, Deceased v. Turbomeca, S.A., a French Corporation, and Societe Nationale Industrielle Aerospatiale, a French Corporation Aerospatiale Helicopter Corporation, a Delaware Corporation Avialle, Inc., a Delaware Corporation Roberts Aircraft, Inc., an Arizona Corporation) is published on Counsel Stack Legal Research, covering Court of Appeals for the Tenth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
37 Fed. R. Evid. Serv. 225, prod.liab.rep. (Cch) P 13,373 Four Corners Helicopters, Inc., a Colorado Corporation Jenny R. Paton, as Surviving Spouse and as Personal Representative of the Estate of William Paton, Deceased v. Turbomeca, S.A., a French Corporation, and Societe Nationale Industrielle Aerospatiale, a French Corporation Aerospatiale Helicopter Corporation, a Delaware Corporation Avialle, Inc., a Delaware Corporation Roberts Aircraft, Inc., an Arizona Corporation, 979 F.2d 1434 (10th Cir. 1992).

Opinion

979 F.2d 1434

37 Fed. R. Evid. Serv. 225, Prod.Liab.Rep. (CCH) P 13,373
FOUR CORNERS HELICOPTERS, INC., a Colorado corporation;
Jenny R. Paton, as surviving spouse and as
personal representative of the Estate of
William Paton, deceased,
Plaintiffs-Appellees,
v.
TURBOMECA, S.A., a French corporation, Defendant-Appellant,
and
Societe Nationale Industrielle Aerospatiale, a French
corporation; Aerospatiale Helicopter Corporation, a
Delaware corporation; Avialle, Inc., a Delaware
corporation; Roberts Aircraft, Inc., an Arizona
corporation, Defendants.

No. 91-1295.

United States Court of Appeals,
Tenth Circuit.

Nov. 17, 1992.

Mary A. Wells (J. Mark Smith and Stephen J. Baity, with her on the briefs), of Weller, Friedrich, Ward & Andrew, Denver, Colo., for appellant.

James A. Cederberg (Douglas E. Bragg, with him on the brief), of Bragg, Baker & Cederberg, P.C., and Chris A. Mattison (Alan Epstein, with him on the brief), of Hall & Evans, Denver, Colo. for plaintiffs-appellees.

Before LOGAN, HOLLOWAY and BARRETT, Circuit Judges.

BARRETT, Senior Circuit Judge.

Turbomeca, S.A. (Turbomeca) appeals from a judgment entered in favor of plaintiffs Jenny Paton and Four Corners Helicopters, Inc. (Four Corners).

Factual Background

This case arises from a helicopter crash which resulted in the death of pilot William Paton (Paton), husband of Jenny Paton. At the time of the accident, Paton was operating an Aerospatiale SA 315 B "Lama" helicopter for his employer, Four Corners. The helicopter was powered by an Artouste IIIB turbine engine, designed and manufactured by defendant Turbomeca.

The Artouste IIIB is a constant-speed engine which maintains the same revolutions per minute (RPMs) during operational maneuvers by sensing deviations in RPMs and adjusting the amount of fuel delivered to the engine. This process produces additional heat, and if the engine temperature limits are exceeded, the engine will burn itself up.

At the time of the accident, Paton was using the helicopter to transport a compressor by long-line. Although this maneuver placed substantial demands on the engine, it was within the engine's limits. Prior to the accident, this helicopter had been used extensively for this type of mission and, in fact, following the accident, was replaced by a similar aircraft. In the instant case, it is undisputed that the helicopter engine overheated, causing the aircraft to crash. The issue at trial was the cause of overheating.

The National Transportation Safety Board (NTSB) investigated the accident at the scene, during engine dismantling, and at Turbomeca's facility in France. The NTSB discovered that a loose labyrinth screw had backed out of position and contacted the compressor impeller. In its report, the NTSB noted that an abnormal squeal, caused by the screw rubbing the diffuser-holder plate, had been witnessed prior to the crash of the aircraft. The NTSB's report also documented twenty-one previously reported instances where, during the course of engine repair or maintenance, it was discovered that the labyrinth screw had rubbed the impeller. In each instance, the engine was removed either because of abnormal noise which occurred during engine rundown, later discovered to be the screeching of the screw on the impeller, or because of a slightly slower rundown time.

Turbomeca also participated in the investigation, conducting loose screw tests upon a similar engine and then transmitting the results to the NTSB and the Federal Aviation Administration (FAA). In its report, Turbomeca reviewed the same twenty-one prior loose screw incidents but concluded that the friction between the screw and the impeller was a minor anomaly which had no effect on the correct operation of the engine. Turbomeca had previously issued Service Bulletin TU133, labelled "URGENT," which outlined a modification procedure to "improve locking of front labyrinth fastening screws on diffuser cover." The company recommended that the modification be performed as soon as possible on both the production line and when repairing engines. The modification consisted of "staking" the screw heads to the surrounding metal, and was performed on the subject engine in 1979 at Turbomeca's factory in France. During Turbomeca's final testing of the engine in question, the engine "seized" during rundown. This seizure was the subject of a second report by Turbomeca which was never provided to the NTSB, the FAA, or Four Corners.

Plaintiffs proceeded to trial on strict liability in tort and negligence theories. They asserted that the helicopter engine failed when a loose labyrinth housing screw backed out of position and contacted the rear face of the compressor impeller. They claimed that this contact reduced the engine's RPMs, causing additional amounts of fuel to be injected into the engine. The additional fuel produced an increase in temperature beyond the engine's limits, resulting in the engine's destruction.

Turbomeca asserted that the loose labyrinth screw could not have caused the engine failure. Turbomeca presented evidence that when a helicopter is required to hover and place a load in a confined area, a collective pitch change results, increasing the engine's temperature, over which the pilot has control. Turbomeca argued that in the instant case, the pilot's demands on the aircraft, namely pulling up too much on the collective pitch control, caused the engine to overheat and ultimately fail. Although Turbomeca's accident reconstructionist opined that no mechanical failure caused the accident, he nevertheless conceded that if there had been a mechanical problem, his theory on pilot error would not be appropriate.

The jury found Turbomeca liable under strict liability only. The district court entered judgment on the jury's verdict, including interest and costs, in favor of Paton in the amount of $959,926.20 and in favor of Four Corners in the amount of $306,204.37.

On appeal, Turbomeca contends that the district court erred in: (1) instructing the jury on a rebuttable presumption that the decedent acted with reasonable care at the time of the accident which caused his death; (2) admitting evidence of sixteen incidents involving labyrinth seal screw backouts; (3) excluding evidence of an experiment conducted by Turbomeca's expert; (4) permitting recovery of economic damages under a strict liability theory; and (5) awarding prejudgment interest on future damages, discounted to the date of trial rather than the date of the decedent's death.

Discussion

I. PRESUMPTION OF REASONABLE CARE INSTRUCTION

Turbomeca contends that the district court erred in instructing the jury on a rebuttable presumption that the decedent acted with reasonable care at the time of the accident which caused his death.

Free access — add to your briefcase to read the full text and ask questions with AI

Related

Cupp v. Naughten
414 U.S. 141 (Supreme Court, 1973)
Larry J. Brandt v. Marvin W. French
638 F.2d 209 (Tenth Circuit, 1981)
Vera Randall v. Warnaco, Inc., Hirsch-Weis Division
677 F.2d 1226 (Eighth Circuit, 1982)
Clifford R. Bannister v. Town of Noble, Oklahoma
812 F.2d 1265 (Tenth Circuit, 1987)
United States v. Alan S. Agnew
931 F.2d 1397 (Tenth Circuit, 1991)
United States v. Robert O. Denny
939 F.2d 1449 (Tenth Circuit, 1991)
Myron Durtsche, Jr. v. American Colloid Company
958 F.2d 1007 (Tenth Circuit, 1992)
Telecky v. Yampa Valley Electric Ass'n
837 P.2d 253 (Colorado Court of Appeals, 1992)
Simpson v. Anderson
517 P.2d 416 (Colorado Court of Appeals, 1974)
City and County of Denver v. DeLong
545 P.2d 154 (Supreme Court of Colorado, 1976)
Union Insurance Co. v. RCA Corp.
724 P.2d 80 (Colorado Court of Appeals, 1986)
Seely v. White Motor Co.
403 P.2d 145 (California Supreme Court, 1965)
Christian v. Randall
516 P.2d 132 (Colorado Court of Appeals, 1973)

Cite This Page — Counsel Stack

Bluebook (online)
979 F.2d 1434, Counsel Stack Legal Research, https://law.counselstack.com/opinion/37-fed-r-evid-serv-225-prodliabrep-cch-p-13373-four-corners-ca10-1992.