In Re Aviation Products Liability Litigation

347 F. Supp. 1401, 1972 U.S. Dist. LEXIS 11868
CourtUnited States Judicial Panel on Multidistrict Litigation
DecidedSeptember 25, 1972
DocketDocket 104
StatusPublished
Cited by3 cases

This text of 347 F. Supp. 1401 (In Re Aviation Products Liability Litigation) is published on Counsel Stack Legal Research, covering United States Judicial Panel on Multidistrict Litigation primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
In Re Aviation Products Liability Litigation, 347 F. Supp. 1401, 1972 U.S. Dist. LEXIS 11868 (jpml 1972).

Opinion

OPINION AND ORDER

PER CURIAM.

The cases comprising this products liability litigation can be segregated into two broad categories. One category consists of actions by corporate plaintiffs asserting claims for damages allegedly caused by defects in the design, manufacture and installation of a gas turbine helicopter engine produced by the Allison Division of General Motors Corporation. The other category consists of actions asserting claims for personal injuries sustained when a helicopter powered by the same type engine crashed 'because of an alleged in-flight engine failure.

Plaintiffs in twelve actions pending in seven different districts moved the Panel to transfer these cases (hereinafter referred to as the Schedule A cases) to a single district for coordinated or consolidated pretrial proceedings. The Panel issued an order to show cause why eight apparently related eases (hereinafter referred to as the Schedule B cases) should not also be considered for transfer pursuant to 28 U.S.C. § 1407. On the basis of the papers filed and the hearing held, we find that all of the Schedule A cases and some of the Schedule B cases will clearly benefit from transfer to a single district for coordinated or consolidated pretrial proceedings.

I. Schedule A Cases

A. Background

Plaintiffs in the Schedule A cases are represented by the same lead counsel. Each plaintiff is a corporate owner or operator of a commercial helicopter powered by a gas turbine engine designed and manufactured by the Detroit Diesel Allison Division of General Motors Corporation (hereinafter Allison). Each action concerns the design, manufacture and installation of the helicopter engine, known as the Allison 250-C18. Allegations concerning the design and manufacture of the helicopter frame are common to some of the cases, as are charges of improper performance of overhaul, modification and repair service. 1

The claims for damages in each of the cases are similar: (1) damages to helicopters and to plaintiff’s business as a result of crashes or emergency landings caused by premature failures and malfunctions of the helicopter’s engine during flight; (2) damages to plaintiff’s business as a result of down time required to make engine modifications and repairs specified by the Federal Aviation Agency and Allison.

B. Arguments of the Parties

Movants urge that the existence of common questions of fact makes transfer to a single district for coordinated or consolidated pretrial proceedings necessary in order to promote the just and efficient conduct of the litigation and to avoid duplicitous discovery and unnecessary inconvenience to the parties and witnesses. Movants contend that the issue of fact central to each lawsuit is the airworthiness of the Allison 250-C18 engine, including its design, development, manufacture and installation. It is asserted that although the specific defects alleged in each separate ease may not be identical they are all interwoven so as to cover the engine’s general condition and airworthiness. It is also asserted that discovery common to all cases will con *1403 cern the extent to which Allison controlled and directed the installation of the engine by the helicopter manufacturers and each incident of engine overhaul modification and repair performed by its authorized distributors.

Allison agrees that consolidation of the Schedule A cases for coordinated pretrial proceedings is necessary, but urges that transfer of the Lametti action 2 be denied because discovery is near completion. Allison also points out that transfer of the Freeman action 3 is unnecessary because that case settled shortly after trial began.

All other defendants 4 oppose transfer of any of the cases in which they are named. Although these defendants generally admit that certain common issues of fact are alleged, they argue that these issues are outnumbered by separate and distinct factual issues peculiar to each case. They assert that since the helicopters were operated in different environments under varying atmospheric conditions, both of which affect the performance of the aircraft and the engine, a substantial amount of local discovery concerning each mishap is necessary and will not be common.

These defendants contend that transfer will restrict their efforts to complete local discovery and will require them to participate in discovery not useful to them. They also contend that an important factor weighing against the desirability of transfer under Section 1407 is the lack of a single district with jurisdiction over all defendants, which precludes any real possibility of a common trial on liability.

C. The Question of Transfer

It is clear from the legislative history of Section 1407 that multidistrict products liability litigation was envisioned as susceptible to effective treatment under Section 1407. 5 There is no dispute that two of the three statutory requirements to transfer exist in this litigation: these are civil actions involving one or more common questions of fact which are pending in more than one district. The opposition to transfer, however, strongly urges that the issues of fact are not so common that the convenience of the parties and witnesses and the just and efficient conduct of the litigation will be promoted by transfer under Section 1407. We do not agree.

Each action against Allison will require discovery concerning the design, manufacture and installation of the Allison 250-C18 engine. Even though different component parts are involved in different cases, discovery common to all cases will concern engineers responsible for the overall design and development of the engine. And plaintiffs may also be interested in deposing the company officials who relied on those engineers. Furthermore, if it is true, as plaintiffs assert, that Allison controlled the installation of the engines by the airframe manufacturers and dictated the specifications regarding overhaul, modification and repair to the authorized distributors, discovery on these issues will likely be common.

We are convinced that transfer of the Schedule A cases to a single district for coordinated or consolidated pretrial proceedings is necessary. For the convenience of the parties and witnesses it is highly desirable that witnesses relevant to the common issues be deposed but once. And only through a coordinated pretrial discovery program, tailored to fit the discovery needs of each party and supervised by a single judge, can overlapping and duplicitous discovery be avoided *1404 and the just and efficient conduct of the litigation assured. 6

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Cite This Page — Counsel Stack

Bluebook (online)
347 F. Supp. 1401, 1972 U.S. Dist. LEXIS 11868, Counsel Stack Legal Research, https://law.counselstack.com/opinion/in-re-aviation-products-liability-litigation-jpml-1972.