Ramey v. Martin-Baker Aircraft Co.

656 F. Supp. 984, 1987 U.S. Dist. LEXIS 2632
CourtDistrict Court, D. Maryland
DecidedMarch 19, 1987
DocketCiv. A. N-85-3143
StatusPublished
Cited by3 cases

This text of 656 F. Supp. 984 (Ramey v. Martin-Baker Aircraft Co.) is published on Counsel Stack Legal Research, covering District Court, D. Maryland 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., 656 F. Supp. 984, 1987 U.S. Dist. LEXIS 2632 (D. Md. 1987).

Opinion

MEMORANDUM

NORTHROP, Senior District Judge.

This lawsuit arises out of an accident at the Naval Test Center at Patuxent River, Maryland. Plaintiff Gary Ramey, an aircraft mechanic, suffered a serious injury while attempting to remove an ejection seat from a Navy F-18 aircraft. Following the accident, Gary and Amanda Ramey 1 initiated suit against McDonnell Douglas Corporation (“McDonnell”), Martin-Baker Aircraft Company Ltd. (“Martin-Baker”), Quinton Rix (“Rix”) and Thomas Waller (“Waller”) in the Circuit Court for St. Mary’s County, Maryland. Following the Circuit Court’s grant of summary judgment in favor of McDonnell, 2 the defendants removed the case to this Court on the basis of diversity jurisdiction. 28 U.S.C. § 1332. In a Memorandum and Order dated May 20, 1986, this Court granted defendant Rix’s motion for summary judgment. 3 Presently before this Court is Martin-Baker’s motion for summary judgment based on the government contract defense. After a careful review of the pleadings and supplemental documentation submitted by the parties, the Court finds that no hearing is necessary. Local Rule 6.

I.

On October 27, 1981, Rix, a McDonnell assistant foreman, assigned Ramey and Waller, another mechanic, the task of removing a Martin-Baker SJU-5 ejection seat from Full Scale Development (“FSD”) 4 F-18 Aircraft No. 3 for the purpose of performing maintenance. The ejection seat is intended to provide pilots with an automatic emergency escape route. It operates by way of a catapult behind the ejection seat which is powered by the firing of *986 three ballistic charges. A rocket motor under the seat provides additional propulsion to propel the seat from the aircraft. An F-18 air crewman need only pull an ejection handle located between the crewman’s legs to initiate the ejection process. Upon ejection, trip rods fixed to the aircraft structure pull sears from the drogue gun and the time release mechanism (“TRM”). 5 Thus activated, the drogue gun fires and deploys two small drogue parachutes, which immediately act as a stabilizing brake for the seat and its occupant. The TRM, or the “brains” of the seat, delays the release of the drogue parachute and the separation of the crewman from the seat until the seat reaches a safe speed, position and altitude. The SJU-5 ejection seat is designed to permit a safe ejection from both a stationary F-18 aircraft on the flight deck of an aircraft carrier and from an F-18 moving at speeds of 600 knots at any altitude.

There is no genuine dispute that the assignment of removing the SJU-5 ejection seat from FSD Aircraft No. 3 is potentially dangerous due to the very nature of the components making up the ejection system. 6 On the day of the accident, this danger was compounded by three unfortunate circumstances. First, neither Ramey nor Waller was qualified to remove the ejection seat from the aircraft. Second, the portable cranes customarily used to lift ejection seats out of cockpits were not available. This meant that the ejection seat had to be removed by manually disassembling its various pieces. Lastly, Ramey and Waller followed McDonnell’s admittedly ambiguous instructions, 7 known as Quality Planning Instruction Sheets (“QPIS”), for removal of the ejection seat bucket and ejection seat. {See Defendant’s Exh. 5, QPIS 74-82-06; Defendant’s Exh. 6, QPIS 74-82-02).

Following a logical interpretation of McDonnell QPIS 74-82-06 for seat bucket removal, Ramey and Waller removed the seat bucket and the entire safety pin set, which, when installed, prevent the ballistic rocket and catapult components from firing. 8 It appears from the record that, while it may have been wrong to remove all of the safety pins, it was impossible to remove less than all of the pins because they were centrally connected. 9 Once all of the pins were removed, the ejection seat was like a “gun with its safety off.” (Charleville Dep. at 147).

Ramey and Waller next turned to QPIS 74-82-02 for guidance on how to remove the remainder of the seat. There is some dispute as to whether this QPIS was the correct instruction to follow for manually *987 removing the seat. 10 In any event, following this QPIS, Ramey and Waller disconnected the trip rods from the aircraft structure and left them dangling from the firing sears on the ballistic TRM and the ballistic drogue parachute gun, despite instructions 9 and 12 of QPIS 74-82-02 which require the trip rods to be secured to the ejection seat. (Defendant’s Exh. 6 at ¶¶ 9, 12). Ordinarily, this would not have created a dangerous situation, but as the safety pins for these ballistic components had been removed, the trip rods on the FSD aircraft would fire the ballistic charges in the components if either rod was pushed downward or upward. (Burrell Affidavit at ¶¶ 10, 15; Charleville Dep. at 140-42, 146).

Ramey then stood above the aircraft cockpit, straddling the ejection seat, and attempted to lift the seat out of the cockpit. Realizing that the seat was too heavy, Ramey dropped it back into the cockpit. According to the Navy and McDonnell investigators, the lowering of the ejection seat caused the unsecured TRM trip rod to contact the hull of the aircraft. This caused sear removal which, in turn, fired the drogue gun ballistic charge. (Defendant’s Exh. 1 at 9). Ramey fell from the aircraft when the ballistic charge detonated and injured himself.

In the complaint, plaintiffs assert product liability claims against Martin-Baker based on theories of negligence, breach of warranty and strict liability. They elaborate on these theories in their opposition to the summary judgment motion by stating that the design of the trip rod, firing lever and sears components of the ejection seat was defective in that these components could be activated by either a downward force or an upward force, notwithstanding the fact that only a downward force was contemplated for emergency ejection purposes. Thus, plaintiffs conclude that, if the components had been designed as a single-action device, the inadvertent detonation would not have been possible and the accident involving Ramey would not have occurred. Further, plaintiffs assert that Martin-Baker should have placed a warning on the ejection seat cautioning that the ballistic cartridges be removed prior to seat removal. Lastly, plaintiffs claim that Martin-Baker should have provided instructions such that maintenance on the ejection seat could be performed safely.

Martin-Baker has moved for summary judgment asserting that the government contract defense bars plaintiffs’ claims. 11 Both parties have blurred the issues and Martin-Baker has not fully addressed all of plaintiffs’ claims.

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Bluebook (online)
656 F. Supp. 984, 1987 U.S. Dist. LEXIS 2632, Counsel Stack Legal Research, https://law.counselstack.com/opinion/ramey-v-martin-baker-aircraft-co-mdd-1987.