Edo Corp. v. Beech Aircraft Corp.

715 F. Supp. 990, 1988 U.S. Dist. LEXIS 12269, 1988 WL 159137
CourtDistrict Court, D. Kansas
DecidedOctober 21, 1988
DocketCiv. A. 85-2204-S
StatusPublished
Cited by7 cases

This text of 715 F. Supp. 990 (Edo Corp. v. Beech Aircraft Corp.) 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
Edo Corp. v. Beech Aircraft Corp., 715 F. Supp. 990, 1988 U.S. Dist. LEXIS 12269, 1988 WL 159137 (D. Kan. 1988).

Opinion

*991 MEMORANDUM AND ORDER

SAFFELS, District Judge.

A trial on this matter was held to the court on August 29, 1988, through September 9, 1988. After considering the evidence presented at that trial along with the written submissions of the parties, the court is prepared to rule.

FINDINGS OF FACT

1. Plaintiff EDO Corporation (“EDO”) is a New York corporation, having its principal place of business in the State of New York.

2. Fiber Science, Inc. was a California corporation and a wholly-owned subsidiary of EDO which merged with and into EDO in November 1983. As a result of the merger, EDO became the successor-in-interest to all contractual rights and obligations of Fiber Science, Inc. Fiber Science, Inc., and thereafter EDO’s Fiber Science Division (both referred to hereinafter as “FSD”) have maintained a principal place of business in Salt Lake City, Utah.

3. Defendant Beech Aircraft Corporation (“Beech”) is a Delaware corporation, having its principal place of business in the State of Kansas.

4. Beginning in September, 1982, Beech and EDO entered into a series of research and development contracts related to a new composite aircraft, the Starship. Beech chose EDO’s Fiber Science Division as a subcontractor on the Starship research and development program because of FSD’s experience with composite filament winding. Composite filament winding is a state of the art process for constructing non-metal aircraft. FSD was to design and construct the main wing for the Starship.

5. The first contract between FSD and Beech provided that FSD would conduct a design study for the wing structure and propose a design to Beech. The parties entered into this first contract in late 1982. The second, third and fourth contracts provided for further design, development and construction of the Starship wing.

6. The contracts incorporated by reference termination clauses identical to those contained in the Armed Services Procurement Regulations (ASPR). The clause at issue here provides as follows:

The performance of work under this contract may be terminated, in whole or from time to time in part, by the buyer in accordance with this clause. Termination of work hereunder shall be effected by delivery to the seller of a Notice of Termination specifying the extent to which performance or work under the contract is terminated and the date upon which such termination becomes effective.

7. This “termination for convenience” clause entitled the terminated party to receive all of its direct costs related to the contract as of the termination date, along with any other direct costs related to termination of the contract, plus a reasonable profit.

8. The first contract between EDO and Beech also provided that all patent and inventive rights arising from the contract would become the property of Beech, except that “procedures, designs, processes and concepts which [were] unique to [FSD] and which were developed prior to this subcontract that [FSD] has documentation for shall be exempt. [FSD] will so indicate in the final report to [Beech] the procedures, designs, processes and concepts that are exempt.”

9. The second, third, and fourth contracts contained similar language to that stated above, except that FSD was not required to set out the exempt procedures, designs, processes and concepts in writing.

10. The contracts in question also contained a non-competition clause. That clause provided:

For a period of six (6) years after the date of execution of this subcontract ... subcontractor shall not, except as authorized by contractor, provide to any third party, aircraft wing structure design consulting, manufacturing techniques, or manufacturing, tooling, or other technical information, or otherwise assist any such third party in the manufacturing of aircraft wing structures as the same re *992 late to fixed wing aircraft having gross weights less than 85,000 lbs. or with respect to inventions, trade secrets, technical information or data which was developed pursuant to contracts with subcontractor and/or title to the same belongs to contractor per this contract.

In negotiating the contracts, the parties had also considered an alternative clause, which was more inclusive and prohibited EDO from doing work on any aircraft structure, wing or otherwise, for another manufacturer. That option was rejected by the parties, and the less restrictive clause was agreed upon instead.

11. After the December 1982 contract, FSD developed its design concept for the Starship main wing and presented the design study to Beech in April 1983. That study included a proposal that an "H” section concept be employed to attach spars to the wing skins.

12. FSD did not indicate in the report that the “H” section concept was proprietary to FSD or that the concept was exempt from the contractual provision bestowing upon Beech patent and inventive rights to all concepts and designs developed pursuant to the contracts. Nor did FSD indicate at a later time that the concept was proprietary to FSD or exempt for the contractual inventive rights clause.

13. Work under the contracts proceeded, and in late 1983, FSD began to gear up to produce the Starship main wing.

14. In late 1983, FSD was presented an opportunity to bid on a research and development project for an Italian company, Ri-naldo Piaggio. Piaggio was developing an aircraft called the GP-180. Like the Star-ship, the GP-180 was a composite aircraft and was to employ a forward wing as a stabilizer, rather than the more conventional stabilizing back wing.

15. FSD was asked to bid on several components of the GP-180, including the forward wing and the wing tips and flaps on the main wing. FSD was not asked to bid on the main wing itself.

16. FSD officials were enthusiastic about the Piaggio opportunity, and began preparations to submit a bid. They also contacted Beech officials “out of courtesy” to advise them of the Piaggio opportunity.

17. Beech officials were strongly opposed to FSD pursuing the Piaggio opportunity. They cited the fact that Piaggio was a strong competitor of Beech, that the GP-180 would be a direct competitor of the Starship, and that it would be nearly impossible for FSD to keep work on the two projects separate. They also stated that they considered it a breach of the noncom-petition clause in the contracts between EDO and Beech.

18. Beech President and Chief Executive Officer, Linden Blue (“Blue”), told FSD officials that if they passed up the Piaggio opportunity and continued to work with Beech, FSD could be assured that it would continue in a productive relationship with Beech for some time into the indeterminate future. He pointed out that working with Piaggio would amount to “consorting with the enemy” and that such an arrangement might alter and compromise FSD’s good working relationship with Beech. However, when FSD President Robert Berrisford (“Berrisford”) asked Blue for a written commitment to a long term relationship with FSD, Blue refused.

19. FSD ultimately decided to forego the Piaggio opportunity, and instead to continue working with Beech.

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Cite This Page — Counsel Stack

Bluebook (online)
715 F. Supp. 990, 1988 U.S. Dist. LEXIS 12269, 1988 WL 159137, Counsel Stack Legal Research, https://law.counselstack.com/opinion/edo-corp-v-beech-aircraft-corp-ksd-1988.