Moyer v. Teledyne Continental Motors, Inc.
Opinions
OPINION BY
¶ 1 The instant matter is an action based on claims of negligence, breach of warranty and strict liability stemming from a single engine aircraft crash.1 Appellants, the adult children of decedents Ronald Moyer and Judy Moyer, appeal from the trial court’s Orders granting summary judgment in favor of Appellee Teledyne Continental Motors, Inc. (hereinafter “TCM”), and Appellee Piedmont Hawthorne Aviation, Inc., (hereinafter “Piedmont”) and from the Order sustaining the preliminary objections of Appellee DivCo, Inc. (hereinafter DivCo).2 Upon a review of the record, we affirm and find inapplicable the exceptions to the eighteen (18) year statute of repose established by the governing federal statute, the General Aviation Revitalization Act of 1994 (“GARA”), Pub.L. No. 103-298, 108 Stat. 1552 (codified as amended at 49 U.S.C.S. 40101, Note).3
¶ 2 In its Opinion filed pursuant to Pa. R.A.P. 1925(a), the trial court set forth the following factual background:
On January 26, 2003, Ronald and Judy Moyer were killed when their Beech V35B single engine aircraft crashed on a small island in the Delaware River. See [Appellants’] Response to TCM’s Motion for Summary Judgment. The Moyers departed from Wings Field in Philadelphia, Pennsylvania and were en route to Columbia, South Carolina. Id. Ronald Moyer, a licensed pilot, was flying the plane. While in flight, Moyer reported a partial loss of engine power. Id. Although air traffic control directed Moyer to a local airport, Moyer radioed back he did not have enough power to make it to the airport. Id. Moyer landed on a small island in the Delaware, but unfor[340] tunately impacted trees on the way down which resulted in an explosion and fire that killed Mr. and Mrs. Moyer. Id.
At the time of the accident, the Moyer’s [sic] aircraft contained an engine assembled by [Appellee] TCM (serial number 573483). TCM assembled and shipped the engine to Beech Aircraft in September, 1980. See Declaration of John S. Barton. Beech Aircraft then installed the engine on the aircraft and the aircraft was delivered to the original owner on April 8,1982. Id. At the time of the accident, the crankcase4 of the subject engine was a replacement, formerly in another TCM engine (serial number 519154). Id. TCM never inspected, repaired or modified either crankcase after the initial assembly. Id.
The crankcase in the aircraft at the time of the crash was repaired on previous occasions. On May 15, 1998, a crack was discovered in the original crankcase. See [Appellants’] response to TCM’s Motion for Summary Judgment. The engine was sent to [Appel-lee] (“Piedmont”) for repair. Id. Piedmont removed the crankcase and sent it to Appellee (“Div[C]o”), an FAA approved facility for repair. Id. Rather than repair the crankcase, Div[C]o replaced the crankcase and sent the replacement to Piedmont. Piedmont installed the Div[C]o crankcase in the subject aircraft. This replacement is the reason why the engine, at the time of the accident, contained a crankcase from an engine with a different serial number.
In November, 2002, the subject aircraft engine underwent additional repairs by a third party, Mr. Robert Ca-baniss, Jr. Cabaniss performed a “top overhaul” of the engine, replacing cylinder assemblies and connecting rod bearings designed and manufactured by Defendant Superior Air Parts “(Superior”). See Cabaniss Deposition, pg. 73, 74, and 82. During the November, 2002 repair, a silicon sealant was applied to the cylinders of the crankcase by Cabaniss, assisted by Moyer. Id. at 109-110. The sealant was not on TCM’s approved list of sealants for that engine.Footnotes
979 A.2d 336 (Moyer v. Teledyne Continental Motors, Inc.) — published by Counsel Stack Legal Research, free access to 12M+ legal documents.
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