CLAIRE V. EAGAN, District Judge.
In the scheduling order (Dkt. # 18), the Court set a deadline of June 6, 2016 for the parties to file motions in limine.
On March 16, 2015, plaintiffs James Rodgers and Christopher Evans filed this case alleging a manufacturer's products liability claim against Beechcraft and a negligence claim against Beechcraft and HBGCS. Their spouses, Sheryll Rodgers and Jill Evans, also allege claims of loss of consortium against defendants. James Rodgers and Christopher Evans were passengers on a Beech Premier 390 aircraft, manufactured by Beechcraft in 2008, that was flying from Tulsa, Oklahoma to South Bend, Indiana on March 17, 2013, and the pilot of the aircraft was Wesley Caves. During the flight, plaintiffs allege that both engines of the plane were inadvertently shut down and the pilot was unable to restart both of the engines due to a defective electrical bus distribution system. Dkt. # 28, at 5-6. The pilot was unable to successfully land the plane and it crashed near the South Bend Airport, and James Rodgers and Christopher Evans were injured in the crash. Plaintiffs allege that the alternate landing gear system failed to deploy properly during the attempted landing and that the alternate landing gear system was defectively designed.
In June 2016, plaintiffs filed a motion to file a second amended complaint (Dkt. # 93) adding a theory of product defect based on the aircraft flight manual (AFM), and they allege that the AFM contains faulty instructions for restarting the electrical generator following a dual engine shutdown.
In the second amended complaint (Dkt. # 129), plaintiffs allege claims of negligence against Beechcraft and HBGCS, a manufacturer's products liability claim against Beechcraft, and loss of consortium claims against Beechcraft and HBGCS. The second amended complaint alleges three defects with the subject aircraft: (1) HBGCS incorrectly installed a repair kit and created a defect in the electrical bus distribution system that caused intermittent electrical supply to essential systems; (2) the alternate landing gear did not operate as represented in the design specifications; and (3) the AFM included faulty instructions for restarting the electrical generators following a shutdown. Dkt. # 129, at 5-7. In addition, plaintiffs allege that defendants were negligent due to inadequate assembly and inspection practices, substandard wiring practices, and the design of the alternate landing gear.
"`A motion in limine is a request for guidance by the court regarding an evidentiary question,'" which the court may provide at its discretion to aid the parties in formulating trial strategy."
The parties' motions in limine are primarily based on the admissibility of evidence under Federal Rules of Evidence 401 and 403. Under Rule 401, evidence is relevant if "(a) it has any tendency to make a fact more or less probable than it would be without the evidence; and (b) the fact is of consequence in determining the action." Fed. R. Evid. 401. However, a court may exclude relevant evidence if "its probative value is substantially outweighed by a danger of . . . unfair prejudice, confusing the issues, misleading the jury, undue delay, wasting time, or needlessly presenting cumulative evidence." Fed. R. Evid. 403. "Evidence may be unfairly prejudicial if it would likely provoke the jury's emotional response or otherwise tend to adversely affect the jury's attitude toward a particular matter . . . [but] [e]vidence is not unfairly prejudicial merely because it damages a party's case."
Plaintiffs ask the Court to exclude evidence of Caves' training in an Eclipse 500 aircraft, because this is not the type of aircraft involved in the accident and evidence of Caves' pilot training is inadmissible under Rules 404 and 406. Dkt. # 43. Defendants respond that plaintiffs have placed Caves' training, specifically his ability to follow checklists, directly at issue by alleging that the checklists in the AFM were defective and by offering expert testimony that Caves was a skilled pilot who acted reasonably up to the time of the crash. Dkt. # 83.
Caves owned an Eclipse 500 aircraft and he received training from Keith Jones in the Eclipse 500. Dkt. # 83-6, at 4 The training occurred in February and March 2012, or about 13 months before the crash giving rise to this lawsuit. Jones noted on one training flight that Caves failed to follow checklist procedures, and Jones' notes contained a number of comments "that the checklist procedure was not either done or verbalized."
Plaintiffs' motion in limine to exclude evidence of Caves' training in the Eclipse 500 aircraft should be denied. One of plaintiffs' theories of product defect is that the checklist in the AFM for restarting the electrical generators is defective.
Plaintiffs ask the Court to exclude Caves' statement that he regularly flew the subject aircraft over the recommended weight limit and evidence that the overspeed warning horn was heard twice before the aircraft's engines were shut off by a passenger on March 17, 2013. Dkt. # 44. Defendants respond that evidence that the overspeed warning horn went off is directly relevant to the cause of the crash, and they argue that evidence that the pilot disregarded weight limits is relevant to plaintiffs' claims that the pilot was a skilled pilot who would have followed instructions in the AFM. Dkt. # 80.
The National Transportation Safety Board (NTSB) prepared a transcript after reviewing the cockpit voice recorder (CVR) following the crash. Caves informs his passengers that the landing gear of the aircraft has a weight limit of 13,000 pounds, Caves states that he does not "have any problem with [13,500 pounds]." Dkt. # 80-1, at 12. Caves goes on to say that "so even though the book is that I don't . . . pay a whole lot of attention to it."
Plaintiffs argue that the Caves's statements concerning flying the aircraft over the recommended weight limit and the two overspeed warnings noted in the transcript of the CVR are irrelevant, because neither the aircraft's weight nor speed were the cause of the crash. Dkt. # 44, at 5. Plaintiffs cite Fed. R. Evid. 404 and 406 and argue that evidence that Caves claimed to regularly fly the aircraft over the recommended weight limit is inadmissible.
Plaintiffs ask the Court to exclude evidence or argument that Caves misused the alternate landing gear or that he was contributorily negligent in failing to lock the alternate landing gear in place. Dkt. # 69. Defendants respond that evidence of Caves' failure to properly use the alternate landing gear system tends to show that pilot error, not a product defect, was the cause of the accident, and this evidence should not be excluded merely because the evidence may not eventually support an instruction on a misuse defense.
Plaintiffs' motion in limine is not a true motion in limine to exclude evidence but, instead, an argument that defendants should be prohibited from presenting the evidence in a particular manner at trial. Neither side disputes that evidence of causation is relevant, but plaintiffs object to the possibility that defendants may characterize Caves' allegedly improper deployment of the alternate landing gear as misuse of the aircraft. The Court finds that it would be premature to prevent defendants from raising a defense of product misuse. As plaintiffs point out, the primary defenses available to a defendant in a products liability claim are lack of evidence of causation, product misuse, and voluntary assumption of the risk. Dkt. # 139, at 3. Voluntary assumption of the risk does not appear to be at issue in this case. The Court will not defeat one of the two remaining defenses based only on plaintiffs' summary of the evidence that may be presented at trial. At the jury instruction conference, the Court will consider whether to instruct on a misuse defense. However, defendants will be permitted to argue that Caves was contributorily negligent as a defense to plaintiffs' negligence claim and that any alleged design flaw in the alternate landing gear system did not cause the accident, even if plaintiffs' motion in limine were granted. Plaintiffs' motion in limine (Dkt. # 69) is denied, but plaintiffs may request a limiting instruction at trial concerning the separate defenses of product misuse (as to the products liability claim) and contributory negligence (as to the negligence claim) if defendants argue that Caves was contributorily negligent in his operation of the alternate landing gear.
Plaintiffs ask the Court to prevent defendants from arguing that "FAA approval or issuance of a type, production or airworthiness certificate" means that the subject aircraft was not defective. Dkt. # 70, at 6. Defendants respond that the FAA's issuance of certificates and the FAA's approval of the AFM tend to show that the aircraft was not defectively designed, and plaintiffs' claims that the FAA did not rigorously examine the alternate landing gear design or the AFM can be raised on cross-examination. Dkt. # 115, at 9.
Plaintiffs argue that compliance with FAA regulations concerning the design and manufacture of the subject aircraft is irrelevant, because a product may comply with federal regulations and still be unreasonably dangerous as a matter of Oklahoma law. Dkt. # 70, at 11-12. They claim that FAA regulations concerning the alternate landing gear and the AFM lack specificity, and that a jury could be confused or misled by evidence of compliance with FAA regulations.
Plaintiffs ask the Court to exclude evidence that Caves was trained in the aircraft itself, rather than by use of a flight simulator, because this method of pilot training is approved by the FAA and Caves received the proper certification to fly the subject aircraft, regardless of the training method. Dkt. # 71. Defendants respond that evidence of Caves' pilot training is admissible to rebut plaintiffs' argument that Caves was a skilled pilot who could have restarted both engines and generators following a dual-engine shutdown. Dkt. # 113, at 14-17. Defendants claim that plaintiffs intend to offer evidence that Caves took FAA-approved training and held the necessary type rating to operate the subject aircraft as undisputable evidence that Caves was a skilled pilot. Evidence that Caves' training was inadequate is relevant to show that pilot error caused or contributed to the accident.
Plaintiffs characterize their motion in limine as a request to exclude evidence of the type of training Caves used to obtain his type rating certification to fly the subject aircraft. The parties agree that there are two acceptable methods under FAA regulations. A prospective pilot can receive training under 14 C.F.R. Part 61, and this training occurs only in the aircraft without the use of a simulator. Dkt. # 71, at 2; Dkt. # 113, at 11. Training can also be acquired pursuant to 14 C.F.R. Part 141/142, and the training occurs in the classroom and in a simulator.
The Court finds that plaintiff's motion in limine (Dkt. # 71) should be denied. Although styled as a motion to exclude evidence of the type of training, plaintiffs' motion is part of a broader dispute between the parties and their experts as to the admissibility of evidence concerning Caves' pilot training. It is a fair reading of plaintiffs' motion in limine that plaintiffs will assert that Caves must have been qualified pilot simply because he obtained the necessary certification to operate the subject aircraft. Defendants have cited evidence that the method of training selected by Caves did not include training as to a dual engine shutdown, and this would be relevant to show that pilot error was the sole cause of the crash. Dkt. # 113, at 11-12. Plaintiffs have placed Caves' piloting skills at issue, particularly his ability to follow checklists and respond to a dual engine shutdown. Depending on the manner of the plaintiffs' presentation of evidence at trial, the method of Caves' training may have less relevance, but it would be premature for the Court to exclude this evidence on an
Plaintiffs ask the Court to exclude evidence that their experts Donald Sommer and John Bloomfield placed a wager on the results of a pull force test of the alternate landing gear of an exemplar aircraft. Dkt. # 72. Defendants argue that evidence that plaintiffs' experts placed a wager on test results is relevant to defendants's arguments that testing was improperly performed and that Sommer and Bloomfield may have had a motive to inflate the pull force necessary to deploy the alternate landing gear. Dkt. # 102.
Plaintiffs state that Sommer and Bloomfield placed a $10 bet on the amount of pull force that would be needed to deploy the alternate landing gear in an exemplar aircraft. Dkt. # 72, at 3. Plaintiffs allege that a third-party, Jay Jones, actually pulled out the handle to deploy the alternate landing gear, and they claim that no money ever changed hands as a result of the bet.
The Court finds that plaintiffs' motion to exclude evidence of betting on the test results by Sommer and Bloomfield should be denied. There is a dispute as to whether Sommer or a third-party conducted the testing at issue, and defendants have challenged the methodology employed by Sommer and Bloomfield in conducting testing on exemplar aircraft. Evidence that Sommer and Bloomfield had an incentive to inflate the pull force needed to deploy the alternate landing gear is relevant, because a key issue in this case is whether Sommer and Bloomfield conducted testing on exemplar aircraft in a manner that improperly increased the pull force for using the alternate landing gear. Plaintiffs argue that any minimal relevance of evidence of betting on test results would be outweighed by the unfair prejudice that would result from admission of this evidence. However, plaintiffs argued in response to defendants'
Plaintiffs asks the Court to prevent defendants from arguing that Frank Graham, plaintiffs' expert sound analyst, "destroyed evidence" in a prior case, because this evidence would be irrelevant and offered for the sole purpose of embarrassing Graham. Dkt. # 73. Defendants respond that Graham has made contradictory statements about his conduct in a prior case, and this evidence goes to his truthfulness and credibility. Dkt. # 114, at 6. Defendants also argue that Graham's past conduct is consistent with his unwillingness to fully explain the basis for his opinions in this case.
Graham was an expert witness in
In light of the Court's ruling concerning the admissibility of Graham's testimony, the Court finds that plaintiffs' motion in limine to prevent defendants from cross-examining Graham about his conduct in a prior case is moot if he complies with the requirement that he appear for a supplemental deposition. The primary reason that defendants would introduce evidence of Graham's conduct in
Defendants ask the Court to exclude evidence of electrical defects in the subject aircraft and other aircraft of the same model if the alleged defects did not cause the accident in this case. They also ask the Court to exclude lay opinion testimony concerning the cause of the accident. Plaintiffs respond that Rick Frie should be permitted to testify about electrical problems he observed on a flight on the subject aircraft about two weeks before the crash, and that plaintiffs' experts should be permitted to opine as to electrical defects in other aircraft of the same model and poor workmanship in the subject aircraft.
Admission of evidence "regarding prior accidents or complaints is `predicated upon a showing that the circumstances surrounding them were substantially similar to those involved in the present case.'"
The Court finds that Frie should be permitted to testify about his observations when he was a passenger on the subject aircraft, but he may not offer lay opinion testimony as to the cause of any electrical malfunctions. Frie was a passenger on the subject aircraft on March 5, 2013, just twelve days before the accident, and he reports that the aircraft suffered electrical problems during a thunderstorm. Dkt. # 62-3, at 2. Plaintiffs' electrical expert, John Bloomfield, opines that there was a loose electrical connection on the pilot's essential bus, and he claims that the loose connection would cause electrical problems and voltage spikes. Dkt. # 52-6, at 13, 33-34. During his deposition, Frie offered unsolicited opinions that the aircraft had electrical problems and that there may have been a loose wire. Dkt. # 62-3, at 3, 6. Frie can testify as a fact witness as to his observations of possible electrical malfunctions, because this goes to the condition of the aircraft and the existence of possible electrical problems.
Defendants also ask the Court to exclude evidence that Bloomfield observed other loose screws and missing lock washers in the aircraft wreckage, because plaintiffs have not identified any interruption with the electrical supply that could have been caused by these loose screws. Dkt. # 62, at 10-11. Plaintiffs respond that Bloomfield testified in his deposition that the number of loose screws and missing lock washers was evidence of poor workmanship, and evidence of poor workmanship is relevant to their negligence claim. Dkt. # 119, at 15-16. The Court finds that defendants' request to exclude evidence of loose screws and other alleged poor workmanship should be denied, because this evidence could be relevant to plaintiffs' negligence claim and this evidence would not be unfairly prejudicial to defendants.
Defendants ask the Court to exclude any argument as to legal theories not alleged in plaintiffs' original or amended complaints, from offering cumulative expert testimony, and from offering expert testimony outside the scope of the expert reports and depositions. Defendants also ask the Court to exclude evidence concerning damages for lost income as to plaintiff James Rodgers past the age of 60, because Rodgers testified in his deposition that he planned to retire at 60. Defendants' argument as to exclusion of legal theories not alleged in the original and amended complaints is moot, because plaintiffs have been permitted to file a second amended complaint (Dkt. # 129).
Defendants argue that plaintiffs should be prohibited from offering cumulative expert testimony. Plaintiffs do not object to defendants' request, but they do claim that it will be necessary for their experts to testify about different aspects of the same alleged product defect. The Court has reviewed the reports of plaintiffs' experts in the context of ruling on defendants'
Defendants argue that plaintiffs should be prohibited from offering expert testimony that was not disclosed in plaintiffs' expert reports or deposition testimony. Plaintiffs do not object to defendants' argument but they argue that they should be permitted to rely on an opinions disclosed in a supplemental report prepared by an expert.
Defendants' final argument is that plaintiffs should be prohibited from offering expert testimony concerning lost income of Rodgers beyond the age of 60, because Rodgers testified in his deposition that he intended to retire at that age. Plaintiffs object to defendants' request and argue that Ralph Scott, Ph. D, should be permitted to testify as to Rodgers' income if he had been able to work to the age of 70. Dkt. # 121. The Court finds that defendants' motion in limine should be denied, because Rodger's deposition merely suggests that he had contemplated retiring at 60. The deposition testimony is not so conclusive that it can be treated as a binding admission that Rodgers would have retired at age 60. However, before plaintiffs can offer Dr. Scott's testimony concerning Rodgers' lost income, plaintiffs must lay a foundation that Rodgers could have and would have been likely to work up to the age of 70.