Taylor v. Mooney Aircraft Corp.

464 F. Supp. 2d 439, 2006 U.S. Dist. LEXIS 84476, 2006 WL 3386642
District Court, E.D. Pennsylvania·Decided November 21, 2006·No. Civ.A. 03-221·Published·Cited by 2 cases

Opinion

MEMORANDUM

ROBERT F. KELLY, District Judge.

Before this Court are the Motions for Summary Judgment filed by Defendants Mooney Aircraft Company (“Mooney”) and Honeywell International Inc. (“Honeywell”). For the reasons set forth below, Defendants’ motions are granted in full.

I. BACKGROUND

This action arises out of an airplane crash that resulted in the deaths of pilot Peter Sandek (“Peter”), his wife Jo Ellen, and their son Kyle (collectively the “San-deks”). Geoffrey Gish, a Georgia resident appointed as representative for the estates of the decedents, filed these wrongful death and survival actions against Honeywell, Mooney, and other defendants in the Philadelphia Court of Common Pleas on November 25, 2002. His claims are based on theories sounding in strict products liability, negligence, misrepresentation, breach of warranty, and outrageous and willful conduct. Removal to this Court occurred on January 1, 2003. Ralph L. Taylor III (“Taylor”), a Georgia resident duly appointed by the Georgia Probate Court, replaced Mr. Gish as representative of the estates on November 1, 2004. Taylor voluntarily dismissed Defendant Parker Hannifin Corporation on June 30, 2006. Honeywell and Mooney moved for summary judgment as to all claims raised on behalf of the decedent’s estates on September 12, 2006.

The airplane crash that killed the San-deks occurred on November 26, 2000. After taking off from Bradford Regional Airport at 10:53 a.m., Peter radioed to the air traffic controllers that he had an emergency and needed to return. He said he had engine trouble, but did not describe his situation with any detail. Peter requested vectors back to the runway. He never put his airplane on the proper course back to the airport. Witnesses stated that they saw the aircraft fly over the airport twice, once heading north and then heading south. Air traffic controllers lost radar contact with the Sandeks aircraft at approximately 11:17 a.m. The wreckage of the airplane was later found in a wooded area 10 miles northeast of the airport.

Bradford Regional Airport is a small airport located in northwestern Pennsylvania, about 20 miles south of the New York border. The Sandeks had left their Georgia home on November 22, 2006, with the intention of flying to Olean, New York to spend the Thanksgiving holiday with family. Peter intended to land in Olean, but was required to land at Bradford due to bad weather. Snowy conditions prevented Peter from landing in Olean. He was directed to an alternate airport in Bradford. Upon landing, the Sandeks continued their journey to New York by automobile. The family remained in New York until November 26, 2000, when they drove to Pennsylvania in preparation for their return flight home to Georgia.

Peter was a licensed pilot and was certified to fly his aircraft in visual as well as instrument conditions. On November 26, 2006, weather conditions at Bradford were poor. There was very limited visibility. Pilots were required to fly under instrument flight conditions because visual flight was impossible. In instrument flight con *444 ditions, the pilot relies exclusively on his instruments while flying the plane. Peter, recently licensed to fly in instrument conditions, filed an instrument flight plan with air traffic control, and the family commenced their flight back home to Georgia.

Peter was piloting a Mooney M20K, registration number M252MW, which he owned and operated. The Mooney M20K is a small propeller driven airplane, capable of carrying four people. This airplane and its component parts were manufactured and assembled in 1987. Mooney originally sold this aircraft to the G.B. Dupont Co. on January 30, 1987. The airplane was equipped with a Honeywell flight control system, which included a Honeywell KI-256 Flight Command Indicator. Known as an attitude indicator, the KI-256 displays the orientation of the plane relative to the actual horizon. Pilots rely on the attitude indicator when flying under instrument flight condition. Honeywell’s KI-256 was powered by vacuum pressure. Mooney, the airplane manufacturer, had installed a dry engine driven vacuum pump in this aircraft to generate the vacuum pressure needed to power the attitude indicator. Parker Hannifin, who was dismissed from this action, manufactured the vacuum pump used on this airplane. An investigation of the airplane after the crash showed that the vacuum pump on this airplane was badly worn and failed during the flight.

The Federal Aviation Administration (“FAA”) has promulgated a rule on the use of powered instruments in aircraft. In 14 C.F.R. § 23.1331, the FAA has mandated that every instrument using a power source must have a warning light to indicate when power is not adequate to sustain proper instrument performance. That rule allows for the use of integrated or separate warning lights. An integrated warning light is one that is built right into the face of the attitude indicator, visible on the instrument itself. A separate warning light is one that is located somewhere other than on the instrument, in this case on the airplane’s instrument panel. The Mooney’s instrument panel was similar to that of an automobile’s dashboard.

Honeywell did not include an integrated warning light in its KI-256. Mooney installed a separate warning light in compliance with the FAA regulations. The warning light for the attitude indicator was placed in the center of the aircraft’s instrument panel. The light illuminated anytime that the airplane’s vacuum pressure was below the level required to power the KI-256. In its Pilot’s Operating Handbook, Mooney explained the importance of an illuminated warning light. The handbook explained that an illuminated light meant that vacuum pressure in the aircraft was at an unsafe level, and the information obtained from the attitude indicator was unreliable and pilots should disregard it. The handbook was included with the airplane. The FAA approved the handbook and overall design of the Mooney M20K, and certified this aircraft as airworthy.

An electric auxiliary vacuum pump was included on the aircraft in the event that the primary dry engine driven vacuum pump failed to produce the required vacuum pressure. Once the pilot was alerted by the low vacuum pressure warning light, he could engage the auxiliary pump by turning a switch mounted on the instrument panel. When using the auxiliary pump, the pilot was instructed to monitor the mechanical vacuum gauge installed in his instrument console to determine whether acceptable vacuum pressure was present in the system. This gauge showed the level of vacuum pressure in the airplane’s system at all times, regardless of which pump was utilized. After the accident, the auxiliary electric pump was tested and functioned properly.

*445 The Sandeks were domiciliaries of the State of Georgia. Ralph Taylor, the representative of the estates, is a Georgia resident. The estates of the decedents are being probated in Georgia. Peter purchased this airplane in Georgia from a Georgia corporation, GLM. That corporation has maintained and serviced the aircraft in Georgia since 1998. WHP Aviation, Inc., a Georgia company, was employed to service this aircraft. Peter also used the Epps Air Service, Inc., incorporated in Georgia, for additional maintenance after he purchased the airplane.

Free access — add to your briefcase to read the full text and ask questions with AI

Taylor v. Mooney Aircraft Corp., 464 F. Supp. 2d 439, 2006 U.S. Dist. LEXIS 84476, 2006 WL 3386642 (E.D. Pa. 2006).

464 F. Supp. 2d 439 (Taylor v. Mooney Aircraft Corp.) — published by Counsel Stack Legal Research, free access to 12M+ legal documents.

Related

Henning v. Suarez Corp. Industries, Inc.
713 F. Supp. 2d 459 (E.D. Pennsylvania, 2010)
In Re September 11th Litigation
494 F. Supp. 2d 232 (S.D. New York, 2007)