Sievers v. Beechcraft Manufacturing Co.

497 F. Supp. 197, 1980 U.S. Dist. LEXIS 15528
CourtDistrict Court, E.D. Louisiana
DecidedJuly 18, 1980
DocketCiv. A. 78-1167
StatusPublished
Cited by4 cases

This text of 497 F. Supp. 197 (Sievers v. Beechcraft Manufacturing Co.) is published on Counsel Stack Legal Research, covering District Court, E.D. Louisiana primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Sievers v. Beechcraft Manufacturing Co., 497 F. Supp. 197, 1980 U.S. Dist. LEXIS 15528 (E.D. La. 1980).

Opinion

OPINION

ROBERT F. COLLINS, District Judge.

This matter came on for hearing on June 9, 1980, at the pretrial conference, on the renewed motion of defendant, Beech Aircraft Corporation, for summary judgment. After considering the arguments of counsel, the submitted memoranda, the evidence in the record, and the applicable law, the Court hereby GRANTS the motion of Beech Aircraft Corporation for summary judgment.

The suit arises out of the crash into Lake Pontchartrain of a Beech Air King aircraft, Model 200, on April 18, 1977. The owner of the aircraft was Tidewater Marine Service, Inc. (Tidewater). Five persons were killed in the crash, including Gerald Sievers, who was employed by Tidewater as one of the two pilots for the aircraft. Plaintiff, Marilyn P. Sievers, on her own behalf and as natural tutrix of her minor children, filed this action against Beech Aircraft Corporation, the manufacturer of the aircraft, for the wrongful death of her husband, Gerald Sievers. Plaintiff also filed suit against United Beechcraft, Inc., Hangar One, Inc., Pratt-Whitney Aircraft of Canada, Ltd., Bendix Corporation, Hartzell Propellers, Inc., and Borg-Warner Corporation. Through a combination of court ordered and voluntary dismissals, the only remaining defendant is Beech Aircraft Corporation (Beech).

The aircraft was sold to Tidewater by Hangar One, Inc. on April 25, 1975. Beech completed the manufacturing of the aircraft on October 25, 1975, and Tidewater took delivery of the aircraft at the factory four days later. For the year and a half prior to the accident, the aircraft was owned, operated, and controlled by Tidewater and its employees assigned to pilot and maintain the aircraft. Hangar One, Inc. performed the majority of the maintenance work on the aircraft under a Federal Aviation Administration approved progressive maintenance report. As evidenced by the dismissal of Hangar One, Inc., the maintenance of the aircraft is not at issue in this suit.

On the day of the accident, the aircraft was prepared for a routine flight for the following morning. Gerald Sievers informed Coy Neal, the chief pilot, that the aircraft was ready for flight. According to the National Transportation Safety Board Investigative Report (NTSB Report), on the afternoon of the accident Gerald Sievers met with several of his friends at a nearby auto garage. After a couple of beers, the conversation turned to flying and it was decided that the group would join Gerald Sievers in a flight in the aircraft. The group left for the airport at about 9:15 p. m.

The aircraft departed New Orleans International Airport at about 9:35 p. m. The pilot, Gerald Sievers, had informed the local controller that the aircraft would proceed *199 eastbound on a test flight for about 10 to 15 minutes. The flight progressed normally until the time it was positioned by radar for its landing approach. Following the radio acknowledgment from the aircraft of routine traffic advisories, the radar controller noted that the aircraft began to lose altitude and to deviate from its assigned course. The controller attempted to warn the aircraft of its loss of altitude several times, however, the controller received no response from the aircraft. Shortly thereafter, the aircraft disappeared from the controller’s radar scope, and the Coast Guard and Parish Sheriff’s Office were notified that the aircraft had probably crashed in the western area of Lake Pontehartrain.

Following the accident, the National Transportation Safety Board (NTSB) began an exhaustive investigation in order to determine the cause of the crash. Unfortunately, due to the force of the aircraft’s impact, most of the major components were totally destroyed. However, a large part of the horizontal stabilizer of the aircraft was recovered. The NTSB examination “showed the component to be twisted/distorted/separated from the vertical fin assembly due to severe impact/overload force. The examination of the separated surfaces showed evidence of overload. No evidence of pre-impact failure was noted.” NTSB Report, page 9a. The NTSB concluded that the probable cause of the accident was “undetermined” and listed the “stolen or unauthorized use of [the] aircraft” as a contributing factor. Beech’s Exhibit C (The NTSB Probable Cause Sheet).

Beech moves for summary judgment pursuant to Fed.R.Civ.P. 56, on the grounds that there are no genuine issues as to any material facts and that Beech is entitled to judgment as a matter of law. In its Statement of Uncontested Material Facts, filed June 3, 1980, Beech contends that there is no genuine issue to be tried as to the following material facts:

Extensive discovery has developed no information which indicates that any alleged act of negligence by Beech or any alleged manufacturing defect in the accident aircraft, Beech King Air Model 200, N. 256 TM, Serial No. BB-96, caused or contributed to causing the crash of the aircraft on April 18, 1977.

This is the second time Beech has brought a motion for summary judgment based on the fact that plaintiff has failed to develop any evidence to show that any act of negligence of Beech or any alleged manufacturing defect caused or contributed to the crash of the aircraft. On September 26, 1979, the Court denied Beech’s motion in order that the facts concerning the accident could be more fully developed. Plaintiff has engaged in extensive discovery. However, she has not been able to develop any evidence establishing a causal nexus between any alleged deficiency in the aircraft and the crash.

At the outset, it is noted that trial courts are hesitant to render summary judgment in negligence actions; nevertheless, this Court is also aware that summary judgment is proper in those cases in which there is no genuine issue as to any fact that is crucial to plaintiff’s cause of action so that as a matter of law he cannot recover. See, Wright and Miller Federal Practice and Procedure: Civil § 2729, and cases cited therein. In such cases, summary judgment ought to be used to avoid useless trials. 6 Moore’s Federal Practice ¶ 56.02[10]. Where it is clear from the evidence presented at the hearing on a motion for summary judgment that the movant would be entitled to a directed verdict were the case to proceed to trial, summary judgment ordinarily should be granted. Ruffin v. County of Los Angeles, 607 F.2d 1276, 1280 (9th Cir. 1976). “Summary judgment has been granted in numerous cases where the plaintiff has failed to show evidence of negligence on the part of the defendant.” Cousins v. Yaeger, 394 F.Supp. 595, 599 (S.D.Fla.1975). See also, Wilkinson v. Powell, 149 F.2d 335 (5th Cir. 1945); McBride v. Proctor & Gamble Mfg. Co., 300 F.Supp. 1150 (E.D.Tenn.1969); Amick v. Gooding Amusement Co., 248 F.Supp. 782 (D.S.C.1966). Pursuant to the standards of Fed.R.Civ.P. 56, this Court has considered the *200

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497 F. Supp. 197, 1980 U.S. Dist. LEXIS 15528, Counsel Stack Legal Research, https://law.counselstack.com/opinion/sievers-v-beechcraft-manufacturing-co-laed-1980.