Tison v. Fidelity and Casualty Company of New York

181 So. 2d 835, 1965 La. App. LEXIS 3898
CourtLouisiana Court of Appeal
DecidedDecember 21, 1965
Docket10497
StatusPublished
Cited by11 cases

This text of 181 So. 2d 835 (Tison v. Fidelity and Casualty Company of New York) is published on Counsel Stack Legal Research, covering Louisiana Court of Appeal primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Tison v. Fidelity and Casualty Company of New York, 181 So. 2d 835, 1965 La. App. LEXIS 3898 (La. Ct. App. 1965).

Opinion

181 So.2d 835 (1965)

Doris Barton TISON et al., Plaintiffs-Appellees,
v.
The FIDELITY AND CASUALTY COMPANY OF NEW YORK et al., Defendants-Appellants.

No. 10497.

Court of Appeal of Louisiana, Second Circuit.

December 21, 1965.
Rehearing Denied January 26, 1966.

*837 Lunn, Irion, Switzer, Trichel & Johnson, Shreveport, for appellants.

Davenport, Farr & Kelly, Monroe, for intervenor Northern Ins. Co. of New York.

Martin S. Sanders, Jr., Winnfield, Thomas & Friedman, Natchitoches, for appellees.

Before HARDY, GLADNEY and AYRES, JJ.

GLADNEY, Judge.

This suit by the widow and minor daughter of S. P. Tison seeks recovery of damages from the Fidelity and Casualty Company of New York, the liability insurer of a single engine airplane owned and operated by C. C. Wallace. The plane crashed November 25, 1962 in Lincoln Parish killing Wallace and Tison, who was a guest passenger. The defendant insurer has appealed from an adverse judgment and appellees have answered the appeal asking for an increase in quantum.

Certain facts preceding the fatal flight are pertinent for proper understanding of the issues presented. Paw Paw Island, situated in the Mississippi River near Vicksburg, was the point of departure of the airplane with Shreveport as its destination. After participating in several days of deer hunting on the island Wallace and Tison were returning to their homes. Early that morning, the last day of the hunt, all of the hunters in the group had taken their stands but as the day wore along they returned to the camp at different times. Wallace came in about 8:30 A.M. but Tison did not return until about 1:30 P.M. and following his return to camp he packed up his equipment for his journey home. Prior to the departure of the plane at 3:35 P.M. Wallace consumed a number of drinks of whiskey which those present estimated contained about twelve ounces of alcohol. This evidence is not controverted by appellant. There is no evidence that Tison upon his return to camp actually saw or observed Wallace drinking and the testimony of witnesses clearly establishes that Wallace exhibited no visible signs of intoxication.

At takeoff time good flight weather prevailed at the island. The plane rose smoothly, circled the field and headed westward for Shreveport. It was apparently on its proper course when it reached a point near Monore from which Wallace communicated by radio with Harold V. Odom of the control tower at Selman Field, and reported he was flying at 8500 feet between layers of clouds, the base of the layer above being about 10,000 feet and the top of the lower layer at about 6000 feet altitude. Although the ground was not visible to Wallace then, the flying conditions placed him well within the limits of visual flight rules as prescribed by Federal Aviation Agency regulations.[1] There was no further radio *838 contact between Wallace and the ground after the airplane passed Monroe, and the record contains no evidence with respect to visibility near the 8500 foot level immediately preceding the crash of the plane which occurred at 4:10 P.M. Although the weather may have afforded clear visibility for Wallace at a high altitude just preceding the crash, flight conditions near the ground were unfavorable and rapidly changing for the worse. S. L. Stuckey, a flight instructor at Ruston, Louisiana, testified that throughout the afternoon at the Ruston airport the ceiling was between 200 and 500 feet and those conditions prevailed at the scene of the crash where he arrived shortly after it occurred. At approximately the same time Wallace was passing Monroe at least two other pilots were flying west but below the lower layer of clouds observed by Wallace and these pilots after proceeding a short distance west of Monroe found the ceiling so close to the ground they returned to Monroe where they landed to await a change in weather conditions.

On the following morning after the accident Peter Pompetti of Fort Worth, an air safety investigator for the Civil Aeronautics Board, made an investigation and report of his findings relating to the accident. Wreckage from the plane was found scattered over a wide area with the engine imbedded in the ground under circumstances which indicated that the plane had come apart in flight. In the Pompetti report statements by witnesses who observed the plane near the scene of the crash reported the aircraft was descending from the clouds at a high rate of speed in uncontrolled gyrating rolls to the left and disintegrating as it descended. The aircraft impacted with the ground while inverted and bounced twenty feet disintegrating further. The examination of the wreckage revealed the aircraft had sustained multiple in flight structure failures; that the propeller was rotating under power and the engine was capable of normal operation at the time of impact with the ground. There was no evidence of malfunction or failure of the engine or control system prior to the impact. Pompetti did not determine the cause of the loss of control by the pilot and reported he did not know what happened. Wallace possessed a private pilot's certificate for a single engine, land rating airplane and a current medical certificate. It is indicated that the pilot had flown a single engine airplane better than 400 hours. He was not qualified for instrument flight. The evidence as compiled in the Pompetti report establishes that the crash resulted from the stresses occasioned by in flight overloads, that is, the plane was flown at such speed or under such conditions of stress that the stresses exceeded the capacity or the ability of the plane to withstand the same and therefore the plane broke apart in the air. It appears, therefore, that some action on the part of the pilot while the airplane was in flight caused its coming apart and its destruction. The trial judge commented that there was no evidence from which it could be determined whether or not Wallace lost control of his airplane while flying in the fair weather between the layers of clouds at 8500 feet or whether he lost control after descending to the layer of clouds that lay below him.

Defenses urged by appellant are twofold: First, that no liability has been incurred because of the effect of policy exclusions relating (a) to violations of the instrument flight rule, and (b) violation of FAA rules prohibiting the operation of an aircraft while under the influence of intoxicating liquor; and, second, that recovery is barred by reasons of the legal doctrines of assumption of risk and contributory negligence.

The exclusionary clause provides that the policy does not apply when the insured operates the aircraft in violation of any regulations of the Federal Aviation Agency *839 applicable to instrument flying.[2] It is argued that Wallace attempted to operate under instrument flight conditions without being certified to do so, all in violation of Section 43.65(d) of the Civil Air Regulations which reads:

"§ 43.65 Instrument flight limitations. No person shall pilot an aircraft under instrument flight rules or in weather conditions less than the minimums prescribed for flight under Visual Flight Rules unless he holds a currently effective instrument rating issued by the Administrator."

The evidence clearly discloses that Wallace never held a currently effective instrument rating issued by the Administrator.

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181 So. 2d 835, 1965 La. App. LEXIS 3898, Counsel Stack Legal Research, https://law.counselstack.com/opinion/tison-v-fidelity-and-casualty-company-of-new-york-lactapp-1965.