Raytheon Co. v. Helix Technology Corp.

10 Mass. L. Rptr. 510
CourtMassachusetts Superior Court
DecidedJuly 19, 1999
DocketNo. 984211D
StatusPublished
Cited by1 cases

This text of 10 Mass. L. Rptr. 510 (Raytheon Co. v. Helix Technology Corp.) is published on Counsel Stack Legal Research, covering Massachusetts Superior Court primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Raytheon Co. v. Helix Technology Corp., 10 Mass. L. Rptr. 510 (Mass. Ct. App. 1999).

Opinion

Fabricant, J.

INTRODUCTION

The plaintiff, Raytheon Company, brought this three-count action against the defendant, Helix Technology Corporation, seeking damages it claims were caused by defective components supplied by CTI-Cryogenics (“CTI”), a Division of Helix Technology Corporation. Count I of the complaint alleges breach of warranty. This matter is before the court on defendant Helix’s motion to dismiss count I as barred by the applicable statute of limitations. For the reasons set forth below, the defendant’s motion to dismiss, as to count I, is ALLOWED.

BACKGROUND

The complaint alleges the following facts. The plaintiff is the prime contractor for the Maverick missile program. Maverick missiles are the most widely used precision guided munition in the free world, designed [511]*511for close air support, interdiction and defense suppression missions by the Air Force, Navy and Marine Corps as well as by twenty-four United States allies. The defendant supplied cryoengines for installation in the missile’s imaging infrared guidance system. When the guidance system functions properly, the missiles give United States aircrews “launch and leave” capability at a wide range of distances and speeds, enhancing their safety by enabling them to perform evasive maneuvers after launching a missile.

In 1992, Helix and Raytheon entered into a contract pursuant to which Helix was to manufacture and deliver to Raytheon 5,370 cryoengines. These cryoengines were to be installed in the Fiscal Year 1991 guidance control system of the AGM-65 (“Maverick”) missiles produced by Raytheon for the United States Department of Defense. The contract consists of Purchase Order 77-8781-13-3029, Purchase Order Attachments and a document entitled Critical Item Product Fabrication Specification for Cryoengine for Common IR Guidance Subassembly.1 Pertinent provisions of these documents are the following:

Item 9: This Section shall be deleted and replaced in its entirety with the following:
WARRANTY: CTI-CRYOGENICS warrant that all goods manufactured by CTI-CRYOGENICS shall be free from defects in material, design, workmanship and title: provided, however, that this warranty shall be limited to goods found to be defective within a period of twelve (12) months from the date of delivery from CTI-CRYOGENICS. Warranty is void if the equipment is altered or modified by Ray-theon/User after delivery.
EXCEPT FOR THE EXPRESSED WARRANTY IN THE PREVIOUS PARAGRAPH, CTI-CRYOGENICS DISCLAIMS ALL WARRANTIES WITH RESPECT TO THE GOODS, INCLUDING ANY AND ALL IMPLIED WARRANTIES FOR MERCHANTABILITY, FITNESS FOR ANY PARTICULAR PURPOSE.

Purchase Order 77-8781-13-3029 Attachment 5 (capitalized as in original).

ANY VARIANCES FROM THE PART PRINT(S) AND/OR SPECIFICATIONS MUST BE AUTHORIZED BY AN APPROVED DEVIATION/WAIVER FROM RAYTHEON PRIOR TO SHIPMENT OF THE PART / MATERIAL TO RAYTHEON.
51. ORDER OF PRECEDENCE: THE REQUIREMENTS SPECIFIED HEREIN IN NO WAY RELIEVES (sic) THE SUPPLIER OF COMPLYING WITH THE DRAWING/SPECIFICATION REQUIREMENTS. IN THE EVENT OF A CONFLICT, THE PURCHASE ORDER REQUIREMENTS SHALL GOVERN.

Purchase Order 77-8781-13-3029 (capitalized as in original).

3.2.1.8 Operating Life. The unit shall be capable of meeting the performance requirements specified herein for a minimum of 200 hours of accumulated operation over the operating temperature range of 3.2.2. Continuous periods of running shall not exceed 1.0 hour with at least one-half hour off-time between consecutive one-hour operating periods.

Specification document CI32175-107.

The cryoengines are intended to cool the detector portion of Maverick’s guidance system. If the cryoengines fail to function properly, the guidance system is rendered ineffective. Over time it became apparent to Raytheon that the guidance systems of the Fiscal Year 1991 Mavericks did not perform as well as those deployed earlier. Prior to 1997, defective cryoengines caused three percent of guidance unit failures. In 1997, testing of Maverick missiles revealed a cryoengine failure rate of forty-four percent. The plaintiff informed the defendant and thereafter undertook its own investigation to determine the cause of these cryoengine failures. The plaintiffs failure analysis revealed that helium leaked from two seals in the cryoengines and that these seal failures resulted from impurities, particularly cotton fibers and metal slivers that were introduced into the cryoengines during the manufacturing process. The defects in the cryoengines were inherently unknowable to the plaintiff until the units failed and plaintiffs investigation was completed. The plaintiff has incurred considerable expense investigating and remedying these failures.

Raytheon brought this action against Helix on August 14, 1998. The complaint does not provide a date of delivery of the cryoengines. It does, however, acknowledge, at paragraph 15, that the contract warranty “was generally limited” to defects found within twelve months from the date of delivery. Paragraph 15 goes on to assert that the specification document “explicitly extended CTI’s warranty to the future performance of the cryoengines.” Paragraph 15 thus implicitly acknowledges that delivery occurred more than twelve months prior to discovery of the alleged defect, and more than four years prior to suit. The defendant’s affidavit supplies March 11, 1994, as the last delivery date, and the plaintiff does not contradict this assertion. In light of the allegations of paragraph 15 of the complaint, the Court treats this fact as undisputed for purposes of this motion.

DISCUSSION

For purposes of a motion to dismiss pursuant to Mass.R.Civ.P. 12(b)(6), the allegations of fact in the complaint must be treated as true and the plaintiff is entitled to all favorable inferences. General Motors Acceptance Corp. v. Abington Casualty Ins. Co., 413 Mass. 583, 584 (1992). A motion to dismiss should be granted only if “it appears beyond doubt that the plaintiff can prove no set of facts in support of his claim which would entitle him to relief.” General Motors Acceptance Corp. v. Abington Casualty Ins. Co., 413 Mass. at 584, quoting Nader v. Citron, 372 Mass. 96, 98 (1977), quoting Conley v. Gibson, 355 U.S. 41, 45-46 (1957).

[512]*512While the Court must assume the truth of all well-pleaded factual allegations, characterizations and conclusions of law warrant no such consideration. See e.g. Boston & M.R.R. v. County Com'rs of Middlesex County, 239 Mass. 127, 131 (1921). “The interpretation of a contract presents a question of law for the court, except to the extent disputed facts bear upon such interpretation.” USM Corp. v. Arthur D. Little Systems, Inc., 28 Mass.App.Ct. 108, 116 (1989). The determination of whether a contract contains ambiguity is also a question of law for the court. Fashion House, Inc. v. K-Mart Corp., 892 F.2d 1076, 1083 (1st Cir. 1989). Thus, those portions of the complaint that assert interpretations of the contract provisions are legal, rather factual, and do not bind the Court in considering the motion to dismiss.

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Related

Raytheon Co. v. Helix Technology Corp.
13 Mass. L. Rptr. 334 (Massachusetts Superior Court, 2001)

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Bluebook (online)
10 Mass. L. Rptr. 510, Counsel Stack Legal Research, https://law.counselstack.com/opinion/raytheon-co-v-helix-technology-corp-masssuperct-1999.