Associated Aviation Underwriters v. George Koch Sons, Inc.

712 N.E.2d 1071, 1999 Ind. App. LEXIS 957, 1999 WL 410374
CourtIndiana Court of Appeals
DecidedJune 22, 1999
Docket82A01-9901-CV-1
StatusPublished
Cited by12 cases

This text of 712 N.E.2d 1071 (Associated Aviation Underwriters v. George Koch Sons, Inc.) is published on Counsel Stack Legal Research, covering Indiana Court of Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Associated Aviation Underwriters v. George Koch Sons, Inc., 712 N.E.2d 1071, 1999 Ind. App. LEXIS 957, 1999 WL 410374 (Ind. Ct. App. 1999).

Opinion

OPINION

DARDEN, Judge

STATEMENT OF THE CASE

Associated Aviation Underwriters (AAU) appeals from a declaratory judgment determining that AAU’s “all-risks” insurance policy issued to George Koch Sons, Inc. (Koch) provided coverage for engine damage to Koch’s aircraft.

We affirm.

ISSUE

Whether the trial court’s judgment determining that an “all-risk” policy issued by AAU provided coverage for Koch’s property loss is clearly erroneous.

FACTS

In 1993, Koch purchased a 1986 Cessna Citation S/II aircraft. Over a two-year period, the aircraft’s instruments never indicated that either of the aircraft’s two engines exceeded the maximum allowable temperature. However, in June of 1995, the pilot for Koch *1073 began to notice that the right engine was running approximately five degrees hotter than the left. By September or October of 1995, the right engine was operating at 85 degrees hotter than the left engine.

In November of 1995, Koch was notified that the aircraft engine had “a badly cracked stator,” that an “HT turbine wheel [] was damaged beyond use,” and that there was “heavy rubbing on all of the blades.” (R. 444, 448). It was reported to Koch that the engine damage resulted from an improperly installed high turbine seal ring that allowed excessive heat to escape.

At all relevant times, Koch had insurance on the aircraft under an “all-risk” policy issued by AAU. Koch submitted a claim under the policy, seeking compensation for the money it had spent to repair the engine damage. In a letter to Koch, the senior claims adjuster for AAU acknowledged that the damage sustained by the engine “resulted from the misinstalled high turbine seal ring,” and that “[bjecause the high turbine seal ring was misinstalled, it failed to perform its intended function.” (R. 588). Nevertheless, the adjuster stated that AAU was denying the claim based on an exclusionary provision which precluded coverage for physical damage caused by (a) wear and tear, (b) deterioration, or (c) mechanical breakdown of equipment, components or accessories installed in the aircraft.

Thereafter, Koch filed a complaint for declaratory judgment seeking a determination that the policy issued by the defendant provided coverage for the damage to its aircraft engine. Following a bench trial, the trial court entered judgment in favor of Koch. The trial court determined that the damage to the engine was caused by the negligent installation of a seal ring in the engine during maintenance work on the aircraft and concluded that this peril was not excluded from coverage under AAU’s “all-risk” policy.

DECISION

Standard of Review

At Koch’s request, the trial court entered findings of fact and conclusions of law pursuant to Ind. Trial Rule 52(A). When the trial court makes requested findings of fact and conclusions of law under T.R. 52(A), reversal is appropriate only where the judgment is clearly erroneous. Mutchman v. Consolidation Coal Co., 666 N.E.2d 461, 465 (Ind.Ct.App.1996), trans. denied. A judgment is clearly erroneous when it is unsupported by the findings of fact and conclusions of law entered on those findings. Id. Findings of fact are clearly erroneous when the record lacks any evidence or reasonable inferences to support them. Bell v. Clark, 670 N.E.2d 1290 (Ind.1996). In determining whether the findings are clearly erroneous, we neither judge the credibility of the witnesses nor reweigh the evidence, but consider only evidence and reasonable inferences that support the judgment. Lawson v. Lawson, 695 N.E.2d 154, 155-56 (Ind.Ct.App.1998).

We initially note that we agree with the trial court’s characterization of the policy at issue as an “all-risks” policy for physical damage subject to certain exclusions. Under “Coverage F” of the policy entitled “All Risk Basis,” AAU was obligated “[t]o pay for any physical damage loss to the aircraft.” (R. 18). An “all-risk” insurance policy extends coverage to risks not generally covered under other insurance policies. Cavalier Group v. Strescon Industries, Inc., 782 F.Supp. 946, 954 (D.Del.1992). Such policies generally permit recovery for all fortuitous losses in the absence of fraud or misconduct of the insured, unless the policy contains a specific provision expressly excluding the loss from coverage. Id.; Bd. of Educ. v. International Ins. Co., 292 Ill.App.3d 14, 225 Ill.Dec. 987, 684 N.E.2d 978, 981 (1997), appeal denied, 175 Ill.2d 523, 228 Ill.Dec. 716, 689 N.E.2d 1137; 13A George J. Couch, Couch on Insurance § 48:141 at 139 (M.S. Rhodes ed.1982); 43 Am.Jur.2d, Insurance § 505; Annotation, Coverage Under All-Risk Insurance, 30 A.L.R.5th 170 (1995). Therefore, we must determine whether the insurance policy at issue expressly excludes from coverage Koch’s engine loss.

In the present case, the trial court found that the engine damage at issue was caused by the negligence of a third party, Cessna. Specifically, the trial court determined that Cessna improperly installed a seal ring in the engine during maintenance *1074 work and that this ultimately resulted in engine damage over a two-year period. Notwithstanding AAU’s assertion to the contrary, this finding is supported by the evidence. James Clifford, the aircraft mechanic in charge of the repairs made to the aircraft, testified that the mis-installation of the H.T. seal ring prevented the engine from operate ing as designed. Clifford indicated that the misplaced seal ring did not allow the components in the enginé to expand and contract in the normal dimensional planes in which the manufacturer designed them to move. This caused the stator to warp and crack and caused damage to other engine components. The foregoing evidence reveals that Cessna was negligent in installing the H.T. seal ring, and that this negligent act set into motion the chain of events which caused the engine damage sustained by Koch. Therefore, the trial court’s determination that the engine damage was the result of the negligence of a third party is not clearly erroneous.

Nevertheless, AAU claims that its policy contains a provision excluding coverage for the engine damage by pointing to the following exclusion:

This policy does not apply: ... to physical damage ... caused by and confined to (a) wear and tear, (b) deterioration or (c) mechanical or electrical breakdown or failure of equipment, components or accessories installed in the aircraft unless such physical damage be coincident with and from the same cause as other loss covered by this policy.

(R. 19) (emphasis added).

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712 N.E.2d 1071, 1999 Ind. App. LEXIS 957, 1999 WL 410374, Counsel Stack Legal Research, https://law.counselstack.com/opinion/associated-aviation-underwriters-v-george-koch-sons-inc-indctapp-1999.