Grimm v. Gargis

303 S.W.2d 43, 74 A.L.R. 2d 599, 1957 Mo. LEXIS 728
CourtSupreme Court of Missouri
DecidedMay 13, 1957
Docket45399
StatusPublished
Cited by42 cases

This text of 303 S.W.2d 43 (Grimm v. Gargis) is published on Counsel Stack Legal Research, covering Supreme Court of Missouri primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Grimm v. Gargis, 303 S.W.2d 43, 74 A.L.R. 2d 599, 1957 Mo. LEXIS 728 (Mo. 1957).

Opinion

HOLMAN, Commissioner.

On Saturday afternoon, September 19, 1953, plaintiff, Gaylen E. Grimm, was injured in the crash of a “Cessna 170” airplane owned by Continental Exterminators, Inc., and being piloted by George Gargis. The pilot was killed in the crash. In this action plaintiff sought to recover damages for his personal injuries from the estate of said deceased and the corporate owner of the aircraft. The jury returned a verdict for $10,500 against both defendants. They have duly appealed from the ensuing judgment.

The evidence disclosed that it was customary for pilots and others interested in aviation to gather at Rosecrans Airport in St. Joseph, Missouri, on Saturday afternoons to fly planes and to discuss aviation while drinking coffee in the coffee shop. On this particular afternoon plaintiff, George Gargis, Pete Schuler, and another flew to Kansas City in Schuler’s plane. Upon their return, and after some discussion in the coffee shop, they, decided to make a flight over a wild fowl reserve north of St. Joseph, and Gargis said, “Let’s take my plane. I want to blow the dust off of it.” On this flight, plaintiff, Gargis, and Schuler were joined by Bob Madinger who had just arrived at the airport. The plane in question had been purchased by *46 the corporate defendant less than a month before and had been flown only a few hours. It was a dual control plane, but the undisputed evidence was that Gargis was the only pilot and was in control of the plane. Upon entering the plane Gargis sat in the left pilot seat, Schuler in the right front seat, Madinger in the left rear, and plaintiff in the right rear seat. After the plane was warmed up Gargis made some statement to the effect that he was going to make a short field take-off. A short field take-off is a maneuver used where there is limited space available. Its object is to get the plane off the ground quickly and climb enough to clear existing obstacles in a short running or flying distance. That manner of take-off is abnormal in the sense that, except for practice, it is used only where conditions make it necessary. The expert testimony was that a short field take-off is not dangerous if properly executed.

To a large extent an aircraft is caused to lift and stay in the air by the airflow over the wing area. A short field take-off is accomplished by the adjustment of flaps located in each wing. These are regulated by a lever which may be set in three different notches. The first notch will set the flaps at 20 degrees, the second at 40 degrees, and the third at 60 degrees. In a normal take-off the flaps are in neutral. In a short field take-off it is recommended that the flaps be set in the first notch, but it is optional with the pilot as to whether he uses the first or second notch. The normal speed at which a “Cessna 170” will leave the ground is 70 to 80 m.p.h. However, when the flaps are lowered it slows the speed of the plane but it will lift from the ground quicker and at a slower speed. The danger in this procedure is that if the rate of climb is too steep the plane will stall, and unless corrective measures are taken instantly the plane will fall. A stall occurs when the aircraft overclimbs to the point that it ceases to move forward, and, since there is no flow of air over the wings the lift is eliminated and the plane ceases to fly. The instant plane was equipped with a stall warning signal which would make a noise similar to a foghorn when the plane was approaching a stall.

In executing the take-off in question Gargis set the flaps in the second notch. The plane left the ground while going from 40 to 50 m.p.h. which is dangerously slow because at that speed it could stall at any time. Immediately after the craft “broke” ground the stall warning sounded and it continued to sound intermittently until the actual stall occurred. When the plane reached an altitude variously estimated at from 75 to 150 feet it came to a “standstill”; began to “wobble” and went “into a violent shudder.” At this point one wing dipped and the plane spiraled downward and crashed. Schuler and Madinger did not appear to have been injured, but, as stated, Gargis was killed and plaintiff injured.

There is no dispute in the evidence as to the cause of the crash and the action that the pilot should have taken in order to avoid it. The crash was caused by the abnormally sharp rate of climb (contributed to by the weight of four heavy men) which reduced the speed of the craft to the point where it was insufficient to complete the climb. As the plane approached a stall the proper procedure was to reduce the amount of flap used, thus lowering the nose of the plane and permitting it to gain speed before again continuing the climb. Instead of following that procedure Gargis, when the plane was dangerously near a., stall, put the “flaps” lever in the third (60 degree) notch, thus raising the nose of the plane even more instead of lowering it. The effect of that action was to further decrease the speed, thus maintaining the stall which caused the plane to crash. Additional facts will hereafter appear in the course of our discussion of the various points briefed.

We will first' consider the contention of defendants that the court erred in denying their separate motions for a *47 directed verdict for the reason that the facts ⅛ evidence were not sufficient to authorize a finding of negligence on the part of the deceased pilot, and for the further reason that plaintiff was guilty of contributory negligence as a matter of law. There is no merit in either contention. The petition was based on the res ipsa loquitur doctrine. However, recognizing that the proof disclosed specific acts of negligence on the part of the pilot, resulting in the crash, plaintiff properly submitted an instruction (given by the court) which required a finding of specific negligence as a predicate for his recovery. Jarboe v. Kansas City Public Service Co., 359 Mo. 8, 220 S.W.2d 27. Moreover, our foregoing statement discloses ample evidence from which the jury could reasonably find that the crash resulted from the pilot’s failure to use ordinary care in doing the acts which brought about the stall of the plane and his failure to take available remedial steps to regain a safe flying speed. Furthermore, even if we assume that plaintiff heard Gargis say that he was going to make a short field take-off (and made no protest) he would not be guilty of contributory negligence as a matter of law. Gar-gis was an experienced pilot with 1,200 hours flying time and there was evidence that a short field take-off is not hazardous when properly exfecuted. There was no evidence to indicate that plaintiff should have anticipated that he would perform that maneuver in a negligent and dangerous manner.

The corporate defendant next asserts that its motion for a directed verdict should have been sustained because there was no evidence that the deceased pilot was acting as the agent of said corporation. Plaintiff alleged that at the time and place in question the airplane was “owned and operated by defendant Continental Exterminators, Inc., by and through its agent, servant and employee George Gargis, deceased.” His theory of recovery against said defendant is more specifically disclosed in Instruction No. 3 wherein a verdict against that defendant was predicated upon a finding that “at all times mentioned in Instruction No.

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Bluebook (online)
303 S.W.2d 43, 74 A.L.R. 2d 599, 1957 Mo. LEXIS 728, Counsel Stack Legal Research, https://law.counselstack.com/opinion/grimm-v-gargis-mo-1957.