Melgares v. Sikorsky Aircraft Corp.

613 F. Supp. 2d 231, 2009 U.S. Dist. LEXIS 21881, 2009 WL 723108
CourtDistrict Court, D. Connecticut
DecidedMarch 18, 2009
DocketCivil Action 08-cv-0995 (JCH), 08-cv-1002 (JCH), 08-cv-1014 (JCH)
StatusPublished
Cited by11 cases

This text of 613 F. Supp. 2d 231 (Melgares v. Sikorsky Aircraft Corp.) is published on Counsel Stack Legal Research, covering District Court, D. Connecticut primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Melgares v. Sikorsky Aircraft Corp., 613 F. Supp. 2d 231, 2009 U.S. Dist. LEXIS 21881, 2009 WL 723108 (D. Conn. 2009).

Opinion

RULING RE: DEFENDANTS’ MOTIONS TO DISMISS (DOC. NOS. 14, 21, & 43) 1

JANET C. HALL, District Judge.

I. INTRODUCTION

This is a consolidated product liability action arising out of a July 2006 helicopter crash near Tenerife, Spain that killed six persons. The plaintiffs are the survivors and estate representatives of two of the decedent aircrew members, the survivors and estate representatives of two of the decedent passengers, and the helicopter’s insurer (collectively, “the plaintiffs”). 2 The defendants are the helicopter’s manufacturer, the Sikorsky Aircraft Corporation (“Sikorsky”), and its parent, the United Technologies Corporation (“United Technologies”) (collectively, “the defendants”).

The plaintiffs allege the defendants violated the Connecticut Products Liability Act, Conn. Gen.Stat. § 52-572m, et seq., as amended, and the Connecticut Unfair Trade Practices Act, Conn. Gen.Stat. § 42-110b, et seq., (“CUTPA”). Specifically, the plaintiffs bring claims against the defendants under the theories of negligence, strict product liability, and breach of warranty for the defendants’ alleged breach of duties pertaining to the design, manufacture, assembly, inspection, testing, distribution, sale, servicing, maintenance, overhaul, and repair of the helicopter and its component parts, as well as the preparation, writing, approval and/or sale of warnings, instructions, and guidance for use of the helicopter and its component systems.

The defendants have moved to dismiss all three cases on the principle of forum non conveniens and, pursuant to Fed.R.Civ.P. 12(b)(7), for the failure to join an indispensable party under Fed.R.Civ.P. 19. For the reasons that follow, the defendants’ Motions to Dismiss (Doc. Nos. 14, 21, & 43) are granted on the forum non conveniens ground.

II. STANDARD OF REVIEW

In deciding a motion to dismiss, the court accepts the allegations of a complaint as true and construes them in a manner favorable to the pleader. Hoover v. Ron *236 win, 466 U.S. 558, 587, 104 S.Ct. 1989, 80 L.Ed.2d 590 (1984); Grandon v. Merrill Lynch & Co., 147 F.3d 184, 188 (2d Cir.1998). The court must draw all reasonable inferences in the plaintiffs favor. See, e.g., Yung v. Lee, 432 F.3d 142, 146 (2d Cir.2005) (discussing Rule 12(b)(6) motion to dismiss); Lunney v. United States, 319 F.3d 550, 554 (2d Cir.2003) (internal citations omitted) (discussing Rule 12(b)(1) motion to dismiss).

The instant Motions to Dismiss are based, inter alia, on the common law doctrine of forum non conveniens. “The principle of forum non conveniens is simply that a court may resist imposition upon its jurisdiction even when jurisdiction is authorized by the letter of a general venue statute.” Gulf Oil Corp. v. Gilbert, 330 U.S. 501, 507, 67 S.Ct. 839, 91 L.Ed. 1055 (1947). Thus, forum non conveniens is a discretionary device, which, in rare circumstances, permits a court “to dismiss a claim even if the court is a permissible venue with proper jurisdiction over the claim.” Wiwa v. Royal Dutch Petroleum Co., 226 F.3d 88, 100 (2d Cir.2000) (internal quotation omitted). As such, “[d]is-missal tor forum non conveniens reflects a court’s assessment of a range of considerations, most notably the convenience to the parties and the practical difficulties that can attend the adjudication of a dispute in a certain locality.” Sinochem Int’l Co. v. Malay. Int’l Shipping Corp., 549 U.S. 422, 127 S.Ct. 1184, 167 L.Ed.2d 15 (2007) (internal quotation omitted). “The forum non conveniens determination is committed to the sound discretion of the trial court.” Piper Aircraft Co. v. Reyno, 454 U.S. 235, 257, 102 S.Ct. 252, 70 L.Ed.2d 419 (1981).

III. BACKGROUND

A. Factual Overview

On the morning of July 8, 2006, a Sikorsky S-16N helicopter, registration EC-FJJ, crashed into the Atlantic Ocean off the island of Tenerife, Canary Islands, Spain. See National Transportation Safety Board (“NTSB”) Accredited Representative Field Notes, dated July 18, 2006 (“NTSB Field Notes”), Exh. 1 to Affidavit of Robert J. Spragg (“Spragg Affidavit”), at 1. The helicopter carried three crew (two pilots and a mechanic) and three passengers, all of whom were fatally injured in the crash. See id. The decedents included Tania Adia Martinez Zorilla, Alvaro Zapata Morales, Joaquin Ignacio Ortiz de Zarate Perez-Galdos, and Antonio Ruiz y Lacasa, whose survivors and estates are plaintiffs in the instant action.

At the time of the crash, the helicopter was owned and operated by Helicsa-Helicopteros, S.A., a Spanish corporation. See id. at 1-3. The helicopter was insured by plaintiff Banco Vitalicio de Espana Cia. Anonima de Seguros y Reaseguros, who eventually paid out insurance proceeds totaling 3,712,418.00 as a result of the accident. See Complaint, 08-cv-1002 (JCH), at ¶ 28.

At the time of the crash, the helicopter was under contract to the government of Spain and was being used for firefighting duties in the Canary Islands. When the accident occurred, the helicopter was on a positioning flight from the island of La Palma to the island of Gran Canaria, so that maintenance could be performed on one of the helicopter’s main rotor blades, which had started to lose nitrogen from its pressurized spar. See id. Accident investigators from Spain, the NTSB, and Sikorsky would eventually focus their inquiry on whether this main rotor blade failed in flight, causing the crash. See, e.g., e-mail from Wilfred A. Alfalla of Sikorsky to William English of the NTSB, dated September 20, 2006, Exh. 2 to Spragg Affidavit, at 1.

*237 The crash was investigated by the Spanish Civil Aviation Accident and Incident Investigation Commission, also known as the Comisión de Investigación de Accidentes e Incidentes de Aviación Civil (the “CIAIAC”). See Spanish Interim Accident Report, Exh. A to Mem. in Supp. of Motion to Dismiss, Doc. No. 15 (“Spanish Interim Accident Report”), at 8.

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613 F. Supp. 2d 231, 2009 U.S. Dist. LEXIS 21881, 2009 WL 723108, Counsel Stack Legal Research, https://law.counselstack.com/opinion/melgares-v-sikorsky-aircraft-corp-ctd-2009.