Hottle v. Beech Aircraft Corp.

47 F.3d 106, 1995 WL 55667
CourtCourt of Appeals for the Fourth Circuit
DecidedFebruary 3, 1995
DocketNo. 92-1927
StatusPublished
Cited by55 cases

This text of 47 F.3d 106 (Hottle v. Beech Aircraft 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
Hottle v. Beech Aircraft Corp., 47 F.3d 106, 1995 WL 55667 (4th Cir. 1995).

Opinion

Affirmed by published opinion. Judge WIDENER wrote the opinion, in which Judge RUSSELL and Judge HALL concurred.

OPINION

WIDENER, Circuit Judge:

This appeal presents us with the interesting question of whether a federal court sitting in diversity appropriately deferred to a Virginia rule excluding evidence.1 The jury returned a verdict in favor of defendant Beech Aircraft Corporation in a wrongful death action brought by Sally S. Hottle for the death of her husband in an airplane accident. Mrs. Hottle contends that the district court’s exclusion of internal company documents under a Virginia evidentiary rule, several other evidentiary rulings, and the jury instructions were error. She also challenges the sufficiency of the evidence. Finding no error in the court’s deference to the state exclusionary rule in this case, nor any other reversible error, we affirm.

I. Facts

In the late evening hours of October 25, 1989, a Beech Baron 58P airplane crashed shortly after take-off from Manassas Airport in Virginia, killing its pilot and sole occupant, Douglas A. Hottle. The Beech Baron 58P was a six-passenger, twin-engine propeller plane designed and built by Beech Aircraft Corporation (Beech) in 1981-82. Hottle and a partner bought the aircraft from its original purchaser in April, 1989. The plane was on its first flight following repair and reins-tallation of the actuator trim tabs by a mechanic at Manassas Airport. National Transportation Safety Board investigators determined that the trim tab actuators, an essential component of the aircraft’s flight control systems located on the tail of the plane, had been reversed, which was taken by all to be the cause of the crash. On October 11, 1991, Mrs. Hottle, on behalf of herself and her two children, filed a complaint for the alleged wrongful death of her husband against the Beech Aircraft Corporation on the grounds [108]*108of negligent design, negligent failure to warn, and breach of warranty.

Beech engineers designed the Baron series aircraft using an elevator trim tab control system with dual actuators, left and right, to control the trim tab deflector. The actuators are visually similar and are physically, but not functionally, interchangeable.2 Thus the left one can be mounted on the right side of the aircraft but should not be. Interchanging of the actuators allows the trim tabs to deflect beyond their normal limits, in a direction opposite from that anticipated by the pilot, so that the aircraft becomes uncontrollable. To prevent such an occurrence, there are several safeguards: visually distinguishable physical shape of key internal part, the “actuator screw;” See supra, footnote 2; clear warnings and directions in the Beech Maintenance Manual (to which Federal Air Regulations (FARs)3 require strict compliance) for separate disassembly and repair of left and right actuators, including tagging of parts; post-maintenance visual and functional inspection of crucial flight control systems by the mechanic is mandated under the FARs and the Beech Maintenance Manual; and FARs and Beech’s Pilot Operating Handbook require post-maintenance check of direction and range of travel of crucial flight control surfaces by the pilot.

Evidence established that the mechanic who repaired Hottle’s plane incorrectly installed the left actuator on the right side of the plane and vice versa. Evidence also indicated that in doing the repairs, the mechanic failed to follow FAR-mandated compliance with the procedures set out in Beech’s maintenance manuals and his training. The evidence also suggested that pilot error contributed to the accident, as there was testimony that while Hottle performed a visual inspection of the plane, a prudent pilot would have checked for proper deflection of the trim tabs after any repair of these crucial flight control systems. There was also testimony which indicated that Hottle negligently failed to abort take-off when he noticed, or should have noticed, the enormously increased gear-stick pressure during take-off.

Mrs. Hottle argued that the trim tab actuators could have and should have been designed to prevent their being reversed, and that Beech failed to give adequate warnings to the mechanic and the pilot of risks associated with such a reversal. Mrs. Hottle also introduced testimony of a general industry standard and a FAR requiring design of flight control systems so that they can not be installed incorrectly or interchanged. Her experts gave specific examples of designs that might have eliminated or reduced the risk of reversing the actuators.

Beech argued that it was not negligent in its design of the Baron control system, that the warnings given in the Maintenance Manuals were clear and sufficient, that the act of the mechanic was an intervening cause, and that the pilot was contributorily negligent. Beech further asserted that it could not reasonably foresee that a mechanic would ignore FARs and its installation instructions in light of the warnings in its manuals.

Following a trial from June 1-4, 1992, the jury returned its verdict for Beech on all counts. The court denied Mrs. Hottle’s motion for a new trial, and this appeal followed. Mrs. Hottle claims that the court committed reversible error-in several of its evidentiary rulings and in the jury instructions. She also claims that the jury’s verdict was against the weight of the evidence. We find all of the challenges without merit, and will address at some length only the court’s deference to a Virginia exclusionary rule.

II.

Mrs. Hottle first challenges the district court’s exclusion of the Beech Engineering Manual which she offered on the issues of industry standard for safe flight control design, alternative design feasibility, and [109]*109Beech’s knowledge of industry standards. The district court, relying on a Virginia rule of evidence excluding a party’s internal rules and regulations to show negligence, granted Beech’s pretrial motion to exclude the documents. The court noted that, as a matter of public policy, Virginia courts have held that internal rules of a party “are not admissible to prove negligence or set a standard against which a party’s duties are to be assessed.” Notwithstanding this ruling, Mrs. Hottle offered a page from the Engineering Manual as evidence of the industry standard on safe design known as “Go Right — No Go” during cross-examination of Beech’s engineer expert.4 The court stated that it had already ruled on the admissibility of the manual and did not allow the page to be introduced. Mrs. Hottle argues that admissibility should have been determined under the Federal Rules of Evidence and that the court erred in deferring to Virginia’s exclusionary rule.

As noted, we are presented with the question under the Erie line of cases as to whether the Federal Rule of Evidence, which, for the purpose of argument, we assume would allow the evidence to be admitted,5 or the state rule should control in this diversity case. Although we review some decisions regarding admission of evidence under an abuse of discretion standard, we review de novo the legal analysis underlying this aspect of the district court’s decision.

In Erie R.R. v. Tompkins,

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47 F.3d 106, 1995 WL 55667, Counsel Stack Legal Research, https://law.counselstack.com/opinion/hottle-v-beech-aircraft-corp-ca4-1995.