Beech Aircraft Corp. v. Harris

631 F. Supp. 1449
CourtDistrict Court, W.D. Missouri
DecidedApril 8, 1986
Docket86-0349-CV-W-6
StatusPublished

This text of 631 F. Supp. 1449 (Beech Aircraft Corp. v. Harris) is published on Counsel Stack Legal Research, covering District Court, W.D. Missouri primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Beech Aircraft Corp. v. Harris, 631 F. Supp. 1449 (W.D. Mo. 1986).

Opinion

MEMORANDUM AND ORDER

SACHS, District Judge.

Plaintiff (“Beech”) seeks to restrain defendant federal officials from making public distribution of a printed document bearing a January 1986 date, which reproduces a report by a Department of Transportation research organization, Transportation Systems Center (“TSC”), to the Federal Aviation Administration (“FAA”). The report concerns several safety issues relating to a Beech aircraft, Model 35, known as a V-Tail Bonanza. Production of this model has been discontinued, but perhaps 10,000 *1451 planes remain in operation in the United States and overseas.

A preliminary draft of the report, which is itself a preliminary document awaiting further testing results, was “leaked” to a trade publication, The Aviation Consumer, and portions of the study were published under date of December 1, 1985. Beech contends there are serious unscientific and irresponsible errors in small but critical portions of the report, and that release of the report as a public document will create unwarranted alarm among pilots and users of the aircraft, particularly if certain phrases are quoted out of context. Beech is presently subject to about fourteen product liability lawsuits relating to the V-Tail Bonanza, and fears unwarranted refueling of litigation, misleading use of the document in evidence, economic harm, and serious difficulties in obtaining further product liability insurance.

Suit was filed in Kansas City because FAA has a regional office here, and the request for the report came from the FAA Small Aircraft Directorate, which has its headquarters here. Kansas City is the intended distribution point of the 300 copies of the report that have been printed. Beech and other small aircraft manufacturers are located in Wichita, Kansas. Plaintiff asserts federal question jurisdiction as well as jurisdiction under the Administrative Procedure Act. 28 U.S.C. § 1331, 5 U.S.C. §§ 701-6. While the federal defendants strongly resist judicial interference with their discretion to publish and distribute a report deemed to be in the public interest, jurisdiction has not been challenged.

A temporary restraining order was issued upon the filing of litigation last month, requiring defendants to withhold supplying materials in response to requests under the Freedom of Information Act, 5 U.S.C. § 552. At the end of the initial hearing on the motion for a preliminary injunction, the restraining order was continued and enlarged to forbid, temporarily, the public or private distribution of the report by defendants.

As of the recess of the hearing on March 21, 1986, plaintiff had demonstrated serious questions about the soundness of two portions of the report, one dealing with the aerodynamic lift characteristics of the wings of the aircraft and the other relating to the structural strength of the tail. The report was premised on only 2% of the lift being carried by the fuselage, whereas plaintiff initially calculated in the 1940s that the fuselage would bear 16% of the burden and current data shows that the fuselage does carry some 12-14.5%. Testimony offered by defendants’ expert witness, Terence Barnes, seemingly confirms this serious deficiency in the report, which may tend to create unwarranted doubts relating to the soundness of design of the wing structure of the V-Tail Bonanza and other aircraft.

A further critical issue concerns the tail “maneuvering limit envelope.” The report assumes there could be structural failures during anticipated flying conditions. Mr. Barnes agrees with plaintiff’s expert, William H. Schultz, that the report makes unwarranted assumptions, but Barnes does have some reservation, on present information, about possible failures during unanticipated but realistically conceivable flying conditions, not far removed from the anticipated flight “envelope.”

While the report lists significant numbers of in-flight structural failures of the V-Tail Bonanza, it confirms that the aircraft did meet all certification requirements when first manufactured, and there is no question raised concerning this aircraft’s compliance with current standards. The most troublesome issue presented is whether FAA’s current airworthiness standards for general aviation aircraft are adequate to the proper certification of “non-conventional tail aerodynamic configurations.” Recommendations of the report include (1) a further review of pertinent FAA standards, (2) a review of pilot certification requirements for “high performance, single-engine aircraft,” and (3) further limited testing to permit more definitive conclusions.

*1452 After Beech’s pre-litigation objections to the TSC report threatened a confrontation, FAA prepared an accompanying forward, dated March 7, 1986, referenced by rubber-stamp addition to the printed report. FAA states that the report identifies “no immediate safety concerns, provided the airplane is operated within the approved flight envelope. Therefore, no mandatory airworthiness or other immediate action is being considered at this time.” FAA criticizes the TSC report in several aspects, and asserts that “TSC used a simplified method (in calculating lift) that is inconsistent with the methodology generally accepted by the aviation community and FAA certification engineers.” FAA also notes that “TSC acknowledges in the report” that the assumed conditions that “would cause the tail to exceed limit loads” might not be “attainable in actual operation.” FAA states that the results of the TSC analyses are “retained, however, to maintain the independent nature of the report.”

Beech’s major concerns about the report deal with only a few pages in a document exceeding 100 pages in length. A much longer second document relating to accident reports is not challenged. It does appear, however, that the subject matter of the challenged portions is critical to opinions about the structural soundness of the V-Tail Bonanza. Beech has, moreover, supplemented the testimony at the hearing with a twelve-page critique, submitted as an in camera response to interrogatories.

Additional affidavits and exhibits were received in open court on March 29, 1986. Testimony was also heard from Barry D. Clements, FAA's Manager, Aircraft Certification Division, the author of the new forward to the report. He does not now appear to concede that portions of the report are as faulty as seems indicated in the forward that he signed. Although not an engineer, he did offer a plain-spoken testimonial endorsement of the general safety of the V-Tail Bonanza, observing simply that FAA does not consider it to be an unsafe aircraft.

Requests for copies of the report were admitted into evidence, as bearing on the public interest in a release of the report. Typical of the requests are the five that have been received in 1986.

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