Bracisco v. Beech Aircraft Corp.

159 Cal. App. 3d 1101, 206 Cal. Rptr. 431, 1984 Cal. App. LEXIS 2497
CourtCalifornia Court of Appeal
DecidedSeptember 11, 1984
DocketA012110
StatusPublished
Cited by4 cases

This text of 159 Cal. App. 3d 1101 (Bracisco v. Beech Aircraft Corp.) is published on Counsel Stack Legal Research, covering California Court of Appeal primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Bracisco v. Beech Aircraft Corp., 159 Cal. App. 3d 1101, 206 Cal. Rptr. 431, 1984 Cal. App. LEXIS 2497 (Cal. Ct. App. 1984).

Opinion

Opinion

PANELLI, J.

Plaintiffs, surviving wife and children of decedent Eugene Bracisco, appeal from a judgment entered on a jury verdict in favor of defendant Beech Aircraft Corporation in a wrongful death action.

Facts

This action arose from the death of Eugene Bracisco while piloting a Beechcraft C-35 Model Bonanza airplane. The accident occurred when Bracisco’s plane crashed into a tree near his home on a flight from Hayward to Middletown on December 23, 1972. Bracisco’s widow and children (plain *1104 tiffs) brought the instant wrongful death action alleging negligence and strict liability in tort against the plane’s manufacturer, Beech Aircraft Corporation (Beech), its subsidiary Beechcraft West, Richard H. Dederian, owner of “Flight Care” airplane maintenance facility, and Shell Oil Company, supplier of the plane’s gasoline.

The case proceeded to trial by jury. At the close of plaintiffs’ case the trial court granted Shell Oil Company’s motion for nonsuit. At the completion of the trial, the jury returned a verdict in favor of each of the remaining defendants, specifically finding Beech was not negligent or strictly liable for Bracisco’s death. Plaintiffs appeal solely from the judgment entered in favor of Beech on the strict liability claim which was premised on the charge the plane was defectively designed.

Evidence introduced at trial can be summarized as follows: Bracisco worked in San Francisco and would fly home to Middletown on the weekends. It was his custom, upon arriving in Middletown, to circle the valley where his house was located before landing at the local airport. On the day of the accident several witnesses saw and heard Bracisco’s plane before it crashed. Bracisco’s plane approached the valley in a descending left turn. There was conflicting testimony regarding whether or not the plane’s engine was fully audible during Bracisco’s descent. Some witnesses testified they could hear the engine, but it was running slow, decelerating. One of these witnesses testified there was a sudden surge of engine power split seconds before the crash. At least one eyewitness testified the plane’s engine was clearly audible at full power during its descent.

Expert testimony regarding the cause of the crash was also in conflict. Plaintiffs’ expert testified the accident occurred as a result of “unporting” of the left fuel tank during the plane’s descending left turn, resulting in a loss of engine power. “Unporting” occurs when the plane’s nose is allowed to drop below the horizon and the fuel sloshes forward in the tank and away from the fuel line port or pickup outlet leading to the engine. The resulting diminishing fuel supply causes the engine to slow down, idle and eventually stop. Under this theory, Bracisco struggled during his descent to get fuel back to the" engine but succeeded in doing so only moments before impact. Plaintiffs claimed “unporting” occurred due to defective design of the plane’s fuel tanks. They also claimed Beech was aware the unporting problem rendered the plane unsafe, but failed to give adequate instructions, directions or warnings in this regard.

Beech’s experts opined the cause of the crash was an “accelerated stall” from which Bracisco was unable to recover. A “stall” in aeronautical terms refers to a situation where a plane moves too slowly to maintain adequate *1105 lift on the wings so that the plane begins to fall rather than fly or glide. An “accelerated stall” occurs when as the result of a sharp turn, centrifugal force makes the plane “heavier” and the minimum speed needed to keep the wings lifted is increased. Failing to maintain the needed speed under the circumstances resulted in the crash. Beech’s position was that the crash was not caused by defective design but by Bracisco’s error in piloting the plane.

In instructing the jury, the trial court gave a modified version of BAJI No. 2.60 2 regarding plaintiffs’ and defendants’ burden of proof for each of the alleged strict liability and negligence claims. This instruction was followed by a modified version of BAJI No. 9.00.5 defining design defect, 3 and by plaintiffs’ special instruction No. 22 4 providing a product is defective if warnings are required in order to make it safe and these are not given.

Plaintiffs’ principal contention on appeal is that the version of BAJI No. 2.60 which the court gave the jury erroneously stated plaintiffs’ burden of *1106 proof regarding defective design under Barker v. Lull Engineering Co. (1978) 20 Cal.3d 413, 432 [143 Cal.Rptr. 225, 573 P.2d 443, 96 A.L.R.3d 1]. They claim this error was prejudicial and requires reversal in light of the instruction’s misleading effect, Beech’s counsel’s reliance upon it in his closing argument, and the fact there was a great degree of conflict in the evidence regarding defective design. We find this contention meritorious.

Discussion

I. Waiver of error. *

II. BAJI No. 2.60, as given, was prejudicial.

Our Supreme Court in Barker v. Lull Engineering Co., supra, 20 Cal.3d 413, held a product may be found defective in design under either of two alternative tests: “First, ... if the plaintiff establishes that the product failed to perform as safely as an ordinary consumer would expect when used in an intended or reasonably foreseeable manner. Second, ... if the plaintiff demonstrates that the product’s design proximately caused his injury and the defendant fails to establish, in light of the relevant factors, that, on balance, the benefits of the challenged design outweigh the risk of danger inherent in such design.” (Id., at p. 432.)

In the present case, the version of BAJI No. 2.60 given to the jury listed seven issues which plaintiffs had the burden of establishing by a preponderance of the evidence. It also stated defendant Beech had the burden to show the benefits of the challenged design outweighed its concomitant risks. More importantly, it did not, however, specify that not all of the seven listed elements need be proven by the plaintiffs in order to establish a prima facie case of defective design. 6 It also failed to specify under what circumstances the burden shifts to defendant to show the benefits inherent in the defective design outweigh its risks. Although BAJI No. 2.60 abstractly listed each party’s burden of proof, it failed to put the listed issues into perspective under Barker’s alternative defective design tests. This failure to *1107 correctly allocate the prescribed burdens rendered the given instructions erroneous and misleading.

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Bluebook (online)
159 Cal. App. 3d 1101, 206 Cal. Rptr. 431, 1984 Cal. App. LEXIS 2497, Counsel Stack Legal Research, https://law.counselstack.com/opinion/bracisco-v-beech-aircraft-corp-calctapp-1984.