Emory v. McDonnell Douglas Corp.

148 F.3d 347, 42 Cont. Cas. Fed. 77,342, 1998 U.S. App. LEXIS 13211, 1998 WL 327264
CourtCourt of Appeals for the Fourth Circuit
DecidedJune 22, 1998
Docket97-2577
StatusPublished
Cited by15 cases

This text of 148 F.3d 347 (Emory v. McDonnell Douglas 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
Emory v. McDonnell Douglas Corp., 148 F.3d 347, 42 Cont. Cas. Fed. 77,342, 1998 U.S. App. LEXIS 13211, 1998 WL 327264 (4th Cir. 1998).

Opinion

Affirmed by published opinion. Chief Judge WILKINSON wrote the opinion, in which Judge LUTTIG and Senior Judge BEEZER joined.

OPINION

WILKINSON, Chief Judge:

Rosemary Emory was killed when an F/A-18 jet fighter crashed and slid into her truck. Appellant Harold Emory, her husband, sued the manufacturer of the aircraft, the McDonnell Douglas Corporation (MDC), under myriad strict liability and negligence theories. The district court granted MDC’s motion for summary judgment, holding that the government contractor defense barred Emory’s design defect and failure to warn claims. Emory appeals only with respect to his negligent failure to warn claim, arguing that the government contractor defense applies only to design defect claims. Because we find that Emory has failed to satisfy the basic state-law requirements for his failure to warn claim, we affirm the judgment of the district court.

I.

This appeal arises from an October 1, 1992 crash of an F/A-18 jet fighter at the Patux-ent River Naval Air Station (Pax River) -in Maryland. Prior to its arrival at Pax River, the crash aircraft was. kept at the Naval Air Station at Cecil Field, Florida as a “hangar queen” — a plane cannibalized to provide parts for the. repair of other plapes in the squadron. The Navy reassembled the, aircraft and transferred it to Pax River in August 1992. In accordance with normal procedure, a Navy maintenance crew performed an acceptance inspection of the aircraft upon its delivery at Pax River. While conducting a flight control check during the course of that inspection, the maintenance crew discovered a problem. The flight computer displayed codes indicating a failure in the aircraft’s flight control system (FCS).

The F/A-18’s flight computer performs a variety of built-in tests (BITs) to identify FCS failures. Periodic BITs are run automatically by the flight computer to check limited aspects of the FCS. In addition, the flight and maintenance crews may initiate distinct BITs on their own. For example, pilots run a preflight BIT to check the aircraft’s FCS before takeoff. The FCS fail *349 ures detected by these BITs are indicated in a number of ways, including the display of BIT Logic Inspection (BLIN) codes and X’s on the cockpit screen. BLIN codes correspond to different types of FCS failures. When used in conjunction with the F/A-18 maintenance manuals, BLIN codes direct specific procedures for identifying and fixing FCS failures. The display of an X on the cockpit screen indicates the failure of a computer channel connected to one of the flight control surfaces.

In this case, the BLIN codes discovered during the acceptance inspection indicated a failure related to the aircraft’s rudders. Working alongside Michael Kidder, MDC’s Contract Field Service Representative, the Navy maintenance crew attempted numerous repairs to eliminate the BLIN codes. Despite such attempts, the BLIN codes could not be eliminated. ‘ Neither the Navy maintenance crew nor Kidder could determine the cause of the codes. Yet because no X’s had appeared on the cockpit screen, and because repeated checks and functional tests of the rudders uncovered no problems, the aircraft was not placed in a down status. Kidder testified that, although his final advice was to identify and fix whatever problem was causing the BLIN codes, he did not believe the aircraft was unsafe for flight. The Navy too concluded the aircraft was safe to fly and thereafter flew it in approximately ten missions.

On October 1, 1992, the aircraft was assigned to another mission. Major Douglas Yurovich and Lieutenant Colonel Troy Pennington served as the pilot and copilot respectively of the crash aircraft that day. Sometime before takeoff, the cockpit screen displayed X’s and BLIN codes with respect to the aircraft’s rudders. Yurovich responded by activating the FCS reset to clear the displays. Because the X’s and BLIN codes did not reappear, the pilots decided the plane was safe to fly and took off.

Almost immediately upon leaving the ground, however, the X’s reappeared. The aircraft simultaneously experienced a mild left yaw — a side-to-side, fishtailing movement. Yurovich gained control of the aircraft and then reset the FCS. The response seemed successful, as the flight proceeded without incident for a period of between forty-five and eighty minutes. At that point, though, the X’s and BLIN codes reappeared and the aircraft experienced another mild yaw. Yurovich again activated the FCS reset, but the X’s and BLIN codes returned. In light of these repeated indicators of FCS failures, Yurovich and Pennington decided to discontinue the mission and to return to Pax River.

As the aircraft approached the runway, it experienced yet another yaw. Fearing a potentially fatal crash landing, Yurovich aborted the approach, reset the FCS, and began to prepare a second landing attempt. Soon thereafter, however, the aircraft experienced a significant yaw, rolled to the right, and pitched down. Believing a crash to now be a certainty, Pennington pulled his ejection handle, causing both himself and Yurovich to eject safely. Sadly, however, the aircraft crashed and slid into Mrs. Emory’s truck, resulting in her death.

Mr. Emory filed this suit on behalf of himself and as the administrator of his wife’s estate. Emory sued the United States and MDC, stating a negligence claim against the government and both negligence and strict liability claims against the contractor. The United States settled its claims with Emory for $800,000. The district court later granted MDC’s motion for summary judgment, finding that the government contractor defense barred both Emory’s design defect and failure to warn claims. The district court also concluded that Emory’s manufacturing defect claims were not supported by the evidence. Emory now appeals only the dismissal of his negligent failure to warn claim.

II.

The district court dismissed Emory’s negligent failure to warn claim on the basis of the government contractor defense recognized in Boyle v. United Technologies Corp., 487 U.S. 500, 108 S.Ct. 2510, 101 L.Ed.2d 442 (1988). Emory claims that dismissal on this ground was error. He argues that Boyle bars only a design defect claim and that the defense adopted in that decision should be held inap *350 plicable to a failure'to warn claim. While it is true that the Court in Boyle adopted the government contractor defense in the design defect context, many circuits have since held that the defense should also apply to failure to warn claims. See, e.g., Tate v. Boeing Helicopters (Tate II), 140 F.3d 654 (6th Cir.1998); Snell v. Bell Helicopter Textron, Inc., 107 F.3d 744, 749-50 (9th Cir.1997); Oliver v. Oshkosh Truck Corp., 96 F.3d 992, 1003-04 (7th Cir.1996), cert. denied, — U.S. -, 117 S.Ct. 1246, 137 L.Ed.2d 328 (1997); Butler v. Ingalls Shipbuilding, Inc.,

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148 F.3d 347, 42 Cont. Cas. Fed. 77,342, 1998 U.S. App. LEXIS 13211, 1998 WL 327264, Counsel Stack Legal Research, https://law.counselstack.com/opinion/emory-v-mcdonnell-douglas-corp-ca4-1998.