Jetcraft Corp. v. FlightSafety International, Inc.

781 F. Supp. 687, 1991 U.S. Dist. LEXIS 17646, 1991 WL 276098
CourtDistrict Court, D. Kansas
DecidedNovember 27, 1991
Docket89-1596-K
StatusPublished
Cited by5 cases

This text of 781 F. Supp. 687 (Jetcraft Corp. v. FlightSafety International, Inc.) is published on Counsel Stack Legal Research, covering District Court, D. Kansas primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Jetcraft Corp. v. FlightSafety International, Inc., 781 F. Supp. 687, 1991 U.S. Dist. LEXIS 17646, 1991 WL 276098 (D. Kan. 1991).

Opinion

MEMORANDUM AND ORDER

PATRICK F. KELLY, District Judge.

On December 10, 1988, a Cessna 650 owned by plaintiff Jetcraft made its final approach toward Runway 31 of the Hutchinson Municipal Airport. Johnny De Los Santos, a commercial pilot licensed by the FAA and employed by Transporte Aero, S.A., sat in the left-hand front seat of the aircraft and conducted the final approach. Beside him, in the right-hand front seat, sat Wesley D. Kimball, a flight instructor for defendant FlightSafety International, which had agreed to provide flight training for De Los Santos and the other passengers in the plane: Javier Vargas, Jose Gomez, and Jose Aruro Jiminez. At the time of the final approach, Vargas was also in the cockpit, sitting in the jump seat immediately behind Kimball and De Los Santos.

De Los Santos approached the field to conduct a “touch and go” landing under the supervision of Kimball. In a “touch and go” landing, the airplane is landed but not brought to a full stop. Instead, full power is applied to allow the aircraft to ■ take off again.

*690 As De Los Santos maneuvered the plane for its final approach, Kimball, as the pilot in the right-hand co-pilot seat, was the person responsible for the extension of the flaps and landing gear. De Los Santos called for Kimball to extend full flaps. Kimball complied, extending the flaps.

De Los Santos then called for Kimball to lower the landing gear. Kimball moved the landing gear handle to the down position. The red “gear unlocked” light on the instrument panel illuminated. A few seconds later, the landing gear extended and three green landing gear annunciator lights illuminated while the red “gear unlocked” light extinguished. The three green lights indicated to the pilots that the left, right, and nose landing gear were extended and locked in place. Kimball told De Los Santos, “Down and three green lights.” De Los Santos replied: “Check.”

De Los Santos noticed that his final approach, as indicated by the visual approach slope indicator, was a little high. He then descended to an appropriate position. Intending to reduce power on the airplane to idle when the plane descended to 50 feet, De Los Santos told Kimball to make an altitude call when the airplane reached that altitude. As the plane descended, Kimball confirmed on two separate occasions that the three landing gear lights continued to glow.

A slight crosswind of five to seven knots blew from the right side of the runway. De Los Santos gave the plane a slight amount of right rudder to correct for the wind. As the plane touched down, the left landing gear collapsed. Inside the cockpit, the landing gear unsafe horn sounded. The green landing light for the left landing gear no longer glowed green.

De Los Santos tried to advance the throttle to add power to the plane, which at this time was traveling at almost 90 knots. Vargas, seeing De Los Santos try to add power, warned, “We are crashing, pull the power back.” But, immediately after the landing gear safe horn sounded, the left wing touched the runway. The aircraft veered off the runway and came to a stop after hitting the frangible light stanchions lining the runway.

Jetcraft has now brought the present action, in which it seeks recovery for the damage to the Cessna 650. In the present motion, Jetcraft seeks a determination that defendant FlightSafety, and its agent, Kim-ball, owed it a duty of due care, that the defendants breached this duty, and that the breach was the proximate cause of the damages to the Jetcraft airplane. In support of its motion, Jetcraft argues that the doctrines of collateral estoppel, negligence per se, and res ipsa loquitur support each of the determinations of duty, breach, and proximate cause.

Summary judgment is proper where the pleadings, depositions, answers to interrogatories, and admissions on file, together with affidavits, if any, show there is no genuine issue as to any material fact, and that the moving party is entitled to judgment as a matter of law. Fed.R.Civ.P. 56(c). In considering a motion for summary judgment, the court must examine all evidence in a light most favorable to the opposing party, McKenzie v. Mercy Hospital, 854 F.2d 365, 367 (10th Cir.1988). The party moving for summary judgment must demonstrate its entitlement to summary judgment beyond a reasonable doubt. Ellis v. El Paso Natural Gas Co., 754 F.2d 884, 885 (10th Cir.1985). The moving party need not disprove plaintiffs claim; it need only establish that the factual allegations have no legal significance. Dayton Hudson Corp. v. Macerich Real Estate Co., 812 F.2d 1319, 1323 (10th Cir.1987).

In resisting a motion for summary judgment, the opposing party may not rely upon mere allegations or denials contained in its pleadings or briefs. Rather, the nonmoving party must come forward with specific facts showing the presence of a genuine issue of material fact for trial and significant probative evidence supporting the allegation. Anderson v. Liberty Lobby, Inc., 477 U.S. 242, 256, 106 S.Ct. 2505, 2514, 91 L.Ed.2d 202 (1986). Once the moving party has carried its burden under Rule 56(c), the party opposing summary judgment must do more than simply *691 show there is some metaphysical doubt as to the material facts. “In the language of the Rule, the nonmoving party must come forward with ‘specific facts showing that there is a genuine issue for trial.’ ” Matsushita Elec. Indus. Co., Ltd. v. Zenith Radio Corp., 475 U.S. 574, 587, 106 S.Ct. 1348, 1356, 89 L.Ed.2d 538 (1986) (quoting Fed.R.Civ.P. 56(e)) (emphasis in Matsushita ). One of the principal purposes of the summary judgment rule is to isolate and dispose of factually unsupported claims or defenses, and the rule should be interpreted in a way that allows it to accomplish this purpose. Celotex Corp. v. Catrett, 477 U.S. 317, 106 S.Ct. 2548, 91 L.Ed.2d 265 (1986).

The parties disagree as to the cause of the accident. Jetcraft suggests that it was the fault of Kimball, who somehow retracted the landing gear after initially placing the gear into the down and locked position. In support of this suggestion, Jetcraft points out that the landing gear extended and retracted a number of times before the accident without any abnormality. It further points to the results of a National Transportation Safety Board Factual Report of the accident, which stated:

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781 F. Supp. 687, 1991 U.S. Dist. LEXIS 17646, 1991 WL 276098, Counsel Stack Legal Research, https://law.counselstack.com/opinion/jetcraft-corp-v-flightsafety-international-inc-ksd-1991.