Ramey v. Martin-Baker Aircraft Co.

874 F.2d 946, 1989 U.S. App. LEXIS 14536, 1989 WL 47044
CourtCourt of Appeals for the Fourth Circuit
DecidedMay 9, 1989
DocketNos. 87-1716, 87-1765
StatusPublished
Cited by27 cases

This text of 874 F.2d 946 (Ramey v. Martin-Baker Aircraft Co.) 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
Ramey v. Martin-Baker Aircraft Co., 874 F.2d 946, 1989 U.S. App. LEXIS 14536, 1989 WL 47044 (4th Cir. 1989).

Opinion

ERVIN, Chief Judge:

Gary E. Ramey (“Ramey”) and his wife, Amanda C. Ramey, appeal from orders of summary judgment in favor of Quinten Rix, Ramey’s supervisor, and Martin-Baker Aircraft Co., Ltd. (“Martin-Baker”), the manufacturer of an aircraft component Ra-mey believes injured him through its defective design. The district court held Rix immune from suit under a provision of the Maryland Workers’ Compensation Act, Md. Ann.Code art. 101, § 58 (1985). The court also held that the military contractor defense insulated Martin-Baker from liability. We affirm.

[947]*947I.

A.

Ramey, an Air Force-trained aircraft mechanic, worked for Kirk-Mayer, Inc. Kirk-Mayer supplied skilled workers, among them Ramey, to the McDonnell Douglas Corporation for service at the Navy’s Pa-tuxent River Naval Air Test Center (“Pa-tuxent”). McDonnell Douglas, the prime contractor for the Navy’s F-18 fighter aircraft, assigned Ramey to its F-18 full-scale development (FSD) program.

On October 27, 1981, Quinten Rix, Ra-mey’s supervisor and a McDonnell Douglas employee, instructed Ramey to help Thomas E. Waller, another aircraft mechanic, remove the SJU-5 ejection seat1 from an F-18. The F-18 was one of seven, apparently the first seven produced, then undergoing tests at Patuxent.2 While the two were trying to remove the seat from the F-18’s cockpit, they inadvertently triggered one of the seat’s explosive charges. Ramey fell from the F-18’s wing to the hangar floor when the charge exploded, injuring his left leg and foot.

The immediate cause of Ramey’s accident is not in dispute. Because the cranes that mechanics ordinarily used to lift ejection seats from aircraft were not suitable, Ramey and Waller tried to manhandle the seat out of the cockpit. Ramey realizing the seat was too heavy to lift, dropped the seat back into the cockpit. The drop jarred one of the seat’s explosive charge trigger mechanisms and began the charge’s detonation sequence. An audible alarm gave Ramey enough warning to allow him to move from a position straddling the cockpit to the wing before the charge exploded.

Ramey had no specific training on the F-18 ejection seat. Waller had about one hour of instruction on the seat. The two worked from McDonnell Douglas Quality Planning Instruction Sheet No. 74-82-02 (QPIS). Instruction 9 of the QPIS recites “Disconnect ejection seat aircraft grounded maintenance pin set for seat bucket removal.” Waller and Ramey interpreted the instruction to command removing the seat’s safety pin set.3 The set would have prevented the seat’s explosive charges from detonating.

Martin-Baker manufactured the ejection seat as a subcontractor to McDonnell Douglas. Ramey believes Martin-Baker “underdesigned” a component of the seat so that the anticipable, and perhaps inevitable, movements and collisions the seat undergoes during maintenance could trigger the seat’s explosive charges. Ramey also believes Martin-Baker appreciated but failed to apprise the Navy of the risk the seat posed to mechanics, and that the Navy had not otherwise learned of the risk.

Ramey specifically directs our attention to the design of the seat’s drogue firing lever initiator sear assembly (“assembly”), the component Ramey believes was defectively designed. The assembly controls de[948]*948ployment of the seat’s drogue parachutes. The drogues deploy under the impulsion of explosive cartridges in the seat’s drogue “gun.” It was these cartridges that Ra-mey and Waller triggered.

Three components, the timing release mechanism (TRM), the trip rods, and the safety pins, ordinarily prevent accidental detonation of the seat’s explosive charges. As we have observed, Ramey and Waller had removed the safety pins before trying to lift the seat. Ramey and Waller had also disconnected the trip rods, which ordinarily attach both to the seat and the aircraft’s hull and prevent charge detonation until the seat separates from the hull during ejection. The TRM, the component that directs the sequential firing of the seat’s various charges and rocket motors, was also ordinarily restrained from operating by a trip rod. The men left the seat’s trip rods dangling from the seat’s firing sears, the actual explosive triggers.

Navy and McDonnell Douglas investigators concluded that when Ramey dropped the seat back into the cockpit, the TRM trip rod caught on the F-18’s hull. The effect was just as if the trip rod had registered separation during ejection. The force on the trip rod removed the assembly sear, which in turn triggered the drogue gun charge.

Having discussed the role of the various members of the civilian cast, we now review the Navy’s role as it relates to Ra-mey’s allegations. McDonnell Douglas, with Navy approval, chose Martin-Baker to develop the seat. The Navy specified that the design of the seat should comply with its specification 18471, prepared by ejection seat specialists from the Navy Air Systems Command (“NAVAIR”) Airborne Equipment Group.4 NAVAIR evaluated and approved the original seat design as well as all subsequent design modifications.5

B.

The Rameys commenced this action in the Maryland Circuit Court for St. Mary’s County. The Rameys asked damages from Martin-Baker, McDonnell Douglas, Rix and Waller for Mr. Ramey’s injuries and for harm to their marital relationship. The complaint alleged negligence on the part of all defendants and included strict liability and warranty claims against Martin-Baker and McDonnell Douglas. The circuit court shortly ordered summary judgment in favor of McDonnell Douglas, holding it immune from suit as Ramey’s statutory employer under the Act.6 The remaining defendants then removed the suit to the federal district court.

The district court granted Rix’s motion for summary judgment. The court found Rix immune from suit under Athas v. Hill, 300 Md. 133, 476 A.2d 710, 711 (1984), which held that a supervisory employee is not liable under the Act for conduct in furtherance of a nondelegable duty of the employer.

The district court also dismissed Martin-Baker on its motion for summary judgment. The court held that the military contractor defense protected Martin-Baker from claims based on its role in designing the seat.

[949]*949II.

Resolution of this appeal requires us to apply the government, or more precisely the military, contractor defense. We first recognized and applied the defense in Tozer v. LTV Corp., 792 F.2d 403 (4th Cir.1986), cert. denied, — U.S. -, 108 S.Ct. 2897, 101 L.Ed.2d 931 (1988), a wrongful death action brought by the family of a Navy pilot killed in the crash of his reconnaissance aircraft. We promptly relied upon the defense in two more actions stemming from the deaths of military airmen, Dowd v. Textron, Inc., 792 F.2d 409 (4th Cir.1986), cert. denied, — U.S. -, 108 S.Ct. 2897, 101 L.Ed.2d 930-31, reh’g denied, — U.S. -, 109 S.Ct. 11, 101 L.Ed.2d 962 (1988), and Boyle v. United Technologies Corp., 792 F.2d 413 (4th Cir.1986),

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874 F.2d 946, 1989 U.S. App. LEXIS 14536, 1989 WL 47044, Counsel Stack Legal Research, https://law.counselstack.com/opinion/ramey-v-martin-baker-aircraft-co-ca4-1989.