Stecyk v. Bell Helicopter Textron, Inc.

295 F.3d 408, 58 Fed. R. Serv. 1330, 2002 U.S. App. LEXIS 13249
CourtCourt of Appeals for the Third Circuit
DecidedJuly 3, 2002
Docket99-2030, 99-2051, 94-CV-1818, 94-CV-4342, 94-CV-4343
StatusPublished
Cited by176 cases

This text of 295 F.3d 408 (Stecyk v. Bell Helicopter Textron, Inc.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Third Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Stecyk v. Bell Helicopter Textron, Inc., 295 F.3d 408, 58 Fed. R. Serv. 1330, 2002 U.S. App. LEXIS 13249 (3d Cir. 2002).

Opinions

ROTH, Circuit Judge.

These wrongful death actions arose out of the July 20, 1992 crash of a V-22 Osprey aircraft near Quantico, Virginia. Plaintiffs are representatives of the estates of two of the seven members of the crew. Defendants designed, manufactured, and tested the Osprey and the components at issue in this case. A jury trial resulted in judgment for defendants. On appeal, plaintiffs challenge several of the District Court’s evidentiary rulings.

' For the reasons stated below, we will affirm the District Court’s final judgment.

I. FACTS

The twin-engine Osprey combines the vertical takeoff and landing capability of a helicopter with the cruising speed and flying capabilities of a fixed wing aircraft. Bell Helicopter Textron, Inc., along with Boeing Vertol Company, designed and developed the Osprey under a contract with the federal government. General Motors Corporation designed and manufactured the engines under a separate contract with [411]*411the government. Macrotech Fluid Sealing, Inc., manufactured the torquemeter shaft seal,'known as the “617 seal,” under a subcontract with the Bell-Boeing team.

On July 20, 1992, the Osprey crashed while in the transition stage from airplane to helicopter flight. The Osprey was attempting to land at the Quantico military field after a two hour and forty-four minute flight from Eglin Air Force Basé.in Florida. The plane’s three U.S. Marine pilots, together with four Boeing engineers, were killed.

The accident was investigated by a U.S. Navy Court of Inquiry. The Court of Inquiry’s findings were then forwarded to a superior Naval authority for review, referred to as the First Endorsement. The Endorsement became part of the Court of Inquiry Report.

At trial, the District Court admitted the Report, including the Endorsement, into evidence. Both the Court of Inquiry and the Endorsement agreed that the crash occurred after a flammable fluid was ingested by the aircraft’s right engine as the craft was attempting to land. The Court of Inquiry stated that the right torqueme-ter shaft seal (the 617 seal) was installed backwards and leaked, providing “the most probable primary causal factor for the mishap.” . However, the Endorsement did “not concur” with this conclusion. The Endorsement stated that improper installation of the 617 seal was only one possible source of the leaked flammable fluid.

Plaintiffs’ theory was that the crash was caused by a transmission oil leak past a 617 seal that had been installed backwards by Boeing mechanics. They contended that Bell and Macrotech were negligent in not designing a “Murphy-proof1' seal which could not be reversed. While such a “two-way” seal has been installed in subsequent versions of the Osprey, the District Court precluded evidence of this post-incident remedial measure.

For the defense, Bell contended that a 617 seal would' not leak even if reversed and presented an alternate theory of causation that the engine failure was caused by hydraulic fluid, not transmission oil.

Bell presented evidence of three separate tests which concluded .that a reversed 617 seal did not leak. The first test (1992 test) had been performed by Bell employee Ken Wilson at the request of the Court of Inquiry. The 1992 test, which was discussed in both the Court of Inquiry’s findings and the Endorsement, concluded that a reversed 617 seal subjected to the same range of RPMs, torque, power, heat, pressure and tilt angles as the 617 seal on the Osprey did not leak. Plaintiffs’ experts criticized the 1992 test in several ways, including challenging the use of “new” seals and contending that the test’s one hour and twenty minute duration was too short. Plaintiffs did not object to the admission into evidence of the 1992 test.

The two other reversed 617 seal tests, conducted in 1997 and 1998, were performed at Bell’s request by Wilson, who had retired from Bell in 1995. These two tests were videotaped, and Bell produced these videotapes to plaintiffs five months before trial.

During the defense case at trial, when Bell attempted to elicit testimony from Wilson about the 1997 and 1998 tests, plaintiffs objected based, inter alia, on “unfair surprise.” The court excused Wilson and ordered him and defense expert Dr. Thomas Eagar to produce supplemental reports for plaintiffs by 5 p.m. that day, a Friday. Shortly thereafter, the court recessed trial until Tuesday to give plaintiffs the opportunity to consult with their own experts and depose Wilson and Dr. Eagar, if appropriate.

[412]*412When trial resumed on Tuesday morning, plaintiffs confirmed that they had received the reports and declined to take any additional depositions. They asked the court to exclude Wilson’s videotaped tests on the ground that they were not substantially similar to the conditions on the Osprey. After hearing argument about substantial similarity, the court admitted the 1997 and 1998 tests. At the close of Wilson’s testimony, plaintiffs moved to strike his testimony regarding the 1997 and 1998 tests, again on grounds of substantial similarity, and the court denied the motion.

After Wilson testified, Dr. Eagar testified as an expert on failure analysis, testing with respect to failure analysis, and materials science. He presented an alternate theory of causation, opining that the Osprey’s engine failure was caused by hydraulic fluid, not transmission oil.

After a six week trial, the jury returned a verdict for the defendants. The District Court denied post verdict motions, and plaintiffs timely appealed to this Court.

II. STANDARD OF REVIEW

The District Court had jurisdiction under 28 U.S.C. § 1332. We have jurisdiction to review the final judgment of the District Court pursuant to 28 U.S.C. § 1291.

We review the District. Court’s evidentiary rulings principally for abuse of discretion. See General Electric v. Joiner, 522 U.S. 136, 146, 118 S.Ct. 512, 139 L.Ed.2d 508 (1997) (decision to admit or exclude expert testimony); Glick v. White Motor Co., 458 F.2d 1287, 1294-95 (3d Cir.1972) (admission or exclusion of tests); see also Inter Med. Supplies, Ltd. v. EBI Med. Sys. Inc., 181 F.3d 446, 464 (3d Cir.1999) (reviewing district court’s admission of evidence for abuse of discretion, but exercising plenary review over evidentiary rulings with legal component); Complaint of Consolidation Coal Co., 123 F.3d 126, 131 (3d Cir.1997) (same), cert. denied, 523 U.S. 1054, 118 S.Ct. 1380, 140 L.Ed.2d 526 (1998). To show an abuse of discretion, appellants must show the district court’s action was “arbitrary, fanciful or clearly unreasonable.” Stick v. United States, 730 F.2d 115, 118 (3d Cir.1984).

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295 F.3d 408, 58 Fed. R. Serv. 1330, 2002 U.S. App. LEXIS 13249, Counsel Stack Legal Research, https://law.counselstack.com/opinion/stecyk-v-bell-helicopter-textron-inc-ca3-2002.