Learjet Corp. v. Spenlinhauer

707 F. Supp. 44, 1989 U.S. Dist. LEXIS 1931, 1989 WL 17249
CourtDistrict Court, D. Maine
DecidedFebruary 14, 1989
DocketCiv. No. 88-0125-P
StatusPublished
Cited by2 cases

This text of 707 F. Supp. 44 (Learjet Corp. v. Spenlinhauer) is published on Counsel Stack Legal Research, covering District Court, D. Maine primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Learjet Corp. v. Spenlinhauer, 707 F. Supp. 44, 1989 U.S. Dist. LEXIS 1931, 1989 WL 17249 (D. Me. 1989).

Opinion

GENE CARTER, District Judge.

MEMORANDUM OF DECISION AND ORDER GRANTING PLAINTIFF’S MOTION FOR SUMMARY JUDGMENT ON ITS CLAIM AND GRANTING PLAINTIFF’S MOTION FOR SUMMARY JUDGMENT ON THE COUNTERCLAIMS

In this matter Plaintiff seeks payment for maintenance and modification work it performed on a Learjet aircraft owned by Defendant. Defendant has counterclaimed in counts alleging negligence, fraud, breach of warranty, and violation of Federal Air Regulations. Before the Court now is Plaintiffs motion to dismiss or for summary judgment on the counterclaims and its motion for summary judgment of its claim on account. Under Maine choice-of-law rules, see Day & Zimmerman, Inc. v. Challoner, 423 U.S. 3, 4, 96 S.Ct. 167, 168, 46 L.Ed.2d 3 (1975), the state with the most significant relationship to the events surrounding the issues raised in the counterclaim is Kansas. See Beaulieu v. Beaulieu, 265 A.2d 610 (Me.1970); Adams v. Buffalo Forge Co., 443 A.2d 932, 934 (Me.1982). Therefore, with the agreement of both parties, Defendant-Counter-claimant’s Memorandum in Opposition to Plaintiffs Motion for Summary Judgment and to Dismiss at 1 and Memorandum of Points and Authorities in Support of Learjet’s Motions to Dismiss and for Summary Judgment at 5-9, this Court will apply Kansas law. See Adams v. Gates Learjet Corp., Civ. No. 4-86-782-E (N.D.Tex. Aug. 9, 1988) (finding Kansas law applicable in a multiple plaintiff action against Learjet raising the same issues raised by Defendant’s counterclaim here).

The undisputed1 facts show that Defendant purchased a Model 24F Learjet from Plaintiff in 1977. In response to Plaintiffs application, the Federal Aviation [46]*46Administration (FAA) issued a type certificate for the Model 24 in 1966 and for the Model 24F in 1976. In 1981, the FAA issued Airworthiness Directive (AD) 81-16-08 restricting Defendant’s aircraft from a 51,000 foot service ceiling to 45,000 feet. Revision 3 of Optional AD 81-16-08, issued in 1983, permitted operation of the aircraft at 51,000 feet if service kits AMK 81-12, 82-4, and 82-5 were installed. AD 84-17-02, issued in 1984, required installation of service kits AMK-13B, 82-4, and 82-5 on Defendant’s aircraft if AD 81-16-08, revision 3, had not been complied with.

In July 1986. Defendant’s undamaged plane was delivered to a Learjet service center for installation of these kits. The AD work on Defendant’s plane is shown on work order 3-3241-6354-04 dated July 25, 1986. Doug McCullom authorized the work on Defendant’s behalf. Defendant received an invoice for $39,253.27 for the modifications. Although he has acknowledged the invoice, he has not paid it.

Negligence

Count I of the counterclaim alleges that Plaintiff negligently designed both the horizontal stabilizer trim actuator system and the flight control systems’ stall warning systems on the Learjet Model 24. Defendant claims compensatory and consequential damages for the repairs to these systems on his plane made in accordance with AD 84-17-02. Plaintiff has moved for summary judgment on the grounds that Kansas law does not permit recovery in tort for purely economic losses. The Court agrees.

In 1965 the California Supreme Court articulated the seminal majority rule for determining the border line between tort and contract recovery. In Seely v. White Motor Co., 63 Cal.2d 9, 45 Cal.Rptr. 17, 403 P.2d 145 (1965), the court held that economic loss caused by qualitative defects cannot be recovered in tort. In Daitom, Inc. v. Pennwalt Corp., 741 F.2d 1569, 1581 (10th Cir.1984), the Court of Appeals for the Tenth Circuit declared that Kansas had adopted the Seely rule. The court, however, modified the rule somewhat, stating that

it is only when the nature of the defect, the type of the risk, and the manner of injury derive from the unreasonable dangerousness of the product that tort recovery can be pursued. This is consistent with the relative policies underlying the law of warranties and the law of torts.

Id. at 1582 (applying the rule of Pennsylvania Glass Sand Corp. v. Caterpillar Tractor Co., 652 F.2d 1165 (3d Cir.1981)). Other decisions by the federal courts construing Kansas law reflected this approach by holding that when the damage for which relief is sought results not from a sudden, calamitous occurrence but from the product’s failure to live up to expectations, recovery in tort is not permitted. Agristor Leasing v. Meuli, 634 F.Supp. 1208, 1217 (D.Kan.1986); Owens-Corning Fiberglas v. Sonic Development Corp., 546 F.Supp. 533, 542 (D.Kan.1982) (claim for damages for removing defective compressors and having them rebuilt does not properly sound in tort).

In this case the manner of injury did not derive from the unreasonable dangerousness of the product, and there is no allegation of a sudden, calamitous occurrence causing damage. Rather, Defen[47]*47dant/Counterclaimant alleges that Plaintiff failed to design the aircraft properly and that it therefore had to he repaired in compliance with the PAA’s AD 84-17^02; the damages Defendant seeks are the repair costs and revenues lost during repairs. Such damages, if proven, represent a loss of the benefit of the bargain and not an unexpected loss to person or property. Agristor Leasing, 634 F.Supp. at 1217. Therefore, under Kansas law no tort recovery is available,2 and summary judgment is appropriate on Count I.

Count IV also sets forth a negligence theory of recovery; i.e., that violation of the Federal Air Regulations constitutes negligence per se. Defendant argues that this claim merely adds another ground of negligence for recovery. Since the type of damage alleged by Defendant is not cognizable in negligence, he may not recover on this claim and summary judgment is appropriate.3

Count III

In his Memorandum in Opposition to Plaintiffs Motion for Summary Judgment and to Dismiss, Defendant “agrees that his Warranty Claim (Count III) is time barred.” The Court therefore will treat Count III as voluntarily withdrawn by Defendant.

Count II

Count II of the Counterclaim sets forth a claim for fraud or misrepresentation alleging that Plaintiff made material representations to the FAA and others that the horizontal stabilizer trim system and related flight control systems and autopilot complied with 14 C.F.R. Part 25 and were adequately and safely designed. Defendant alleges that the representations were false and that Plaintiff knew that they were false or, in any event, made them recklessly. Defendant further alleges that Plaintiff knew that the FAA represented the flying public and intended that the FAA should rely on the representations and certify the aircraft as airworthy. Finally, Defendant alleges that the FAA

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