Thomas v. McDonnell-Douglas Helicopter Co.

67 F.3d 308, 1995 U.S. App. LEXIS 33003, 1995 WL 563769
CourtCourt of Appeals for the Ninth Circuit
DecidedSeptember 22, 1995
Docket94-15219
StatusUnpublished

This text of 67 F.3d 308 (Thomas v. McDonnell-Douglas Helicopter Co.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Ninth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Thomas v. McDonnell-Douglas Helicopter Co., 67 F.3d 308, 1995 U.S. App. LEXIS 33003, 1995 WL 563769 (9th Cir. 1995).

Opinion

67 F.3d 308

NOTICE: Ninth Circuit Rule 36-3 provides that dispositions other than opinions or orders designated for publication are not precedential and should not be cited except when relevant under the doctrines of law of the case, res judicata, or collateral estoppel.
John THOMAS, Ethelen S. Thomas, husband and wife; David C.
Cook; Vicki Vaughn-Cook, husband and wife; Homer
Hackworth and Lydia Hackworth, husband
and wife, Plaintiffs-Appellants,
v.
MCDONNELL-DOUGLAS HELICOPTER COMPANY, a Delaware
corporation, Defendant-Appellee.

No. 94-15219.

United States Court of Appeals, Ninth Circuit.

Argued and Submitted Sept. 13, 1995.
Decided Sept. 22, 1995.

Before: CHOY, BEEZER and THOMPSON, Circuit Judges.

MEMORANDUM*

Plaintiffs John and Ethelen Thomas, David C. and Vicki Vaughn-Cook, and Homer and Lydia Hackworth (collectively "Thomas") appeal the district court's grant of judgment as a matter of law in favor of defendant McDonnell-Douglas Helicopter Company ("McDonnell Douglas") following a jury verdict in Thomas' favor. Plaintiffs also appeal the district court's conditional grant of a motion for a new trial. We have jurisdiction pursuant to 28 U.S.C. Sec. 1291, and we reverse.

* Thomas argues that the district court erred in granting judgment as a matter of law in favor of McDonnell Douglas. We review this ruling de novo, Wilcox v. First Interstate Bank, 815 F.2d 522, 524-25 (9th Cir.1987), and we agree with Thomas.

The jury's verdict in favor of Thomas will be upheld if it is supported by substantial evidence. Id. at 525. We are not free to weigh the evidence or disregard the will of the jury if reasonable minds could differ over the verdict. See William Inglis & Sons Baking Co. v. ITT Continental Baking Co., 668 F.2d 1014, 1026 (9th Cir.1981), cert. denied, 459 U.S. 825 (1982). In determining whether the jury verdict in this case was supported by substantial evidence, we examine whether a reasonable person could find, based on the evidence at trial, that the fuel float assembly became tangled in the start pump wire causing the erroneous fuel reading and ultimately the crash.1

We are satisfied that substantial evidence supports the jury's verdict. Most compellingly, the McDonnell Douglas Model 369E helicopter crashed with no fuel in the tank, despite the fuel gauge indicating that 90 pounds of fuel remained. This fact alone is persuasive evidence of some defect in the fuel measuring system. Thomas then offered more specific evidence supporting his position regarding the nature of the alleged defect.

McDonnell Douglas had received various reports from helicopter users indicating that the design of the fuel tank could, if the start pump wire was not properly secured to the fuel hose, result in erroneous fuel gauge readings. Indeed, in a Service Information Notice ("EN-38") sent to owners of Model 369E helicopters in September of 1987, McDonnell Douglas indicated that "[t]here have been recent incidents where the fuel tank start pump wiring interfered with the [ ] fuel float after the start pump and fuel quantity sending unit had been replaced in the field. This interference can result in erroneous fuel quantity indications." The EN-38 also informed users that in order to prevent this problem, "the fuel pump wiring shall be wrapped around or tie-wrapped to the fuel inlet hose per the HMI [Helicopter Maintenance Manual]."

The jury then heard testimony from mechanics who examined Thomas' helicopter both before and after the crash. Roger Gagnon, the mechanic who performed the compliance with the EN-38, indicated that he usually used plastic tie-wraps to secure the start pump wire if the wire could not be wrapped at least twice around the fuel hose. While he could not specifically remember his work on the subject helicopter, he understood the EN-38 to permit the use of tie-wraps in the fuel tank.

Although McDonnell Douglas employee George Murrell testified that the start pump wire was usually wrapped twice around the fuel hose when a helicopter left the factory, the wire on Thomas' helicopter was not wrapped twice at the time of the crash.2 A photograph taken of the inside of the fuel tank after the crash confirms that the start pump wire was wrapped only once around the fuel hose. At trial, McDonnell Douglas mechanic Jim Veal attempted to wrap the start pump wire twice around the fuel hose using an exact replica of the fuel tank, but was unable to do so.

Aircraft mechanic Wayne Ballard testified that, when he examined the helicopter after the crash, although the wire was looped over the fuel line, the EN-38 "was not complied with" at that time by the wrap around method, but rather might have been tie-wrapped at some time. Paul Shepherd, a mechanic, looked inside the fuel tank and noticed that the start wire was "kind of spiraled" and looked "like a piece of that Christmas candy."

Finally, Thomas presented the testimony of two experts. Keith Mackey, an aircraft mechanic, testified that tie-wraps used to secure wires can come loose for a variety of reasons. Mackey indicated that he had never before seen tie-wraps used in a fuel tank. Mackey further testified that if the start pump wire were wrapped twice around the fuel hose, the wire would not interfere with the fuel float assembly. Roger Boisjoly, an engineer, testified that in his opinion the design of the fuel indicating system was defective and the attempted repair of the system through the instructions contained in the EN-38 was negligent. Boisjoly also indicated that tie-wraps were not an acceptable method for securing the start pump wire. Boisjoly conceded that if the start pump wire was wrapped properly around the fuel hose, it would not be in a position to interfere with the float arm.

There was sufficient evidence for the jury to believe that when Gagnon complied with the EN-38, he was only able to wrap the wire once around the fuel hose and then tie-wrapped the slack at the top. Sometime during the helicopter's last flight, the tie-wrap came loose and the wire then was in a position to interfere with the fuel float assembly. A rational juror could find that, more probably than not, an improperly secured start pump wire was the cause of the crash and that McDonnell Douglas was both strictly liable for the design and manufacture of the system and negligent in permitting the use of tie-wraps to secure the start pump wire.3

The district court, in its order granting judgment as a matter of law, discounted much of Thomas' evidence, and credited all of McDonnell Douglas' evidence. It is the jury's role, not the district court's or ours to weigh the evidence. The jury's verdict was supported by substantial evidence, and we will not disturb it.

II

McDonnell Douglas offers two other grounds by which we could affirm the trial court's grant of judgment as a matter of law. Neither has merit.

First, McDonnell Douglas argues that Thomas failed to establish that the product was defective when it left the manufacturer.

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67 F.3d 308, 1995 U.S. App. LEXIS 33003, 1995 WL 563769, Counsel Stack Legal Research, https://law.counselstack.com/opinion/thomas-v-mcdonnell-douglas-helicopter-co-ca9-1995.