Terry v. D3 Technologies CA4/1

California Court of Appeal·Decided March 27, 2014·No. D063395·Unpublished

Opinion

Filed 3/27/14 Terry v. D3 Technologies CA4/1 NOT TO BE PUBLISHED IN OFFICIAL REPORTS California Rules of Court, rule 8.1115(a), prohibits courts and parties from citing or relying on opinions not certified for publication or ordered published, except as specified by rule 8.1115(b). This opinion has not been certified for publication or ordered published for purposes of rule 8.1115.

COURT OF APPEAL, FOURTH APPELLATE DISTRICT DIVISION ONE

STATE OF CALIFORNIA

BRIAN TERRY, D063395 Plaintiff and Appellant,

v. (Super. Ct. No. 37-2011-00092814-

CU-WT-CTL)

D3 TECHNOLOGIES, INC. et al.,

Defendants and Respondents.

APPEAL from a judgment of the Superior Court of San Diego County, Richard E.

L. Strauss, Judge. Affirmed.

Mitchell & Gilleon and James C. Mitchell for Plaintiff and Appellant.

Rukin Hyland Doria and Tindall and John Francis Hyland for Defendants and Respondents.

Brian Terry sued his former employer (D3 Technologies, Inc.) and its parent corporation (collectively, D3) for wrongful termination in violation of public policy and

preemptive retaliatory termination (Lab. Code, § 1102.51). The court granted D3's summary judgment motion and entered judgment in D3's favor. Terry appeals. We affirm.

FACTUAL AND PROCEDURAL SUMMARY Factual Summary

In summarizing the relevant facts, we assume the truth of the evidence submitted by Terry and disregard conflicting evidence presented by D3. (See Singleton v. United States Gypsum Co. (2006) 140 Cal.App.4th 1547, 1558.) Because we do not reach the causation issue, we omit a detailed description of the facts related solely to this issue.

D3 provides engineering and design services to the aerospace industry. In 2005, D3 hired Terry, an aerospace engineer who had substantial experience as a structural analysis engineer and stress analyst of aircraft component parts. During the next four years, Terry received raises and positive performance reviews.

In September 2009, D3 entered into a contract with Mitsubishi Aircraft Corporation (Mitsubishi) to design the tailcone of a commercial passenger jet (the MJET project). D3 was responsible for designing the tailcone and the systems to be installed within the tailcone, including struts and mounts for the auxiliary power unit (APU). The APU is used to restart the aircraft's engines if the main engines shut down, and is essential to the safe operation of the aircraft.

1 Labor Code section 1102.5 (§ 1102.5) was amended in 2013, and the amendments became effective on January 1, 2014. (Stats. 2013, ch. 781, § 4.1.) All further references to section 1102.5 are to the former version of the statute.

Terry was assigned to work on the MJET project as technical coordinator for the stress or vibration levels. One of Terry's main duties was to prepare, deliver, and "sign off on" a vibration report that outlines the possible stress or vibration levels on the parts and components of the tailcone assembly, including the APU mounting system. In this report Terry was required to certify that the stress or vibration levels within the tailcone assembly and its components were insignificant and/or covered by the specification levels for the tailcone assembly and aircraft. In other words, Terry was required to state and substantiate that the tailcone system is safe for the vibration and stress environment to which it will be exposed.

The Mitsubishi contract provided for two stages of design review: (1) a "Preliminary Design Review" (PDR); and (2) a "Critical Design Review" (CDR). As is typical in the industry, the contract incorporated an iterative process during which the entities work together to obtain a final design, and specified a multi-step review process requiring that D3 submit updated progress reports, including development, refinement and revision of the component designs. The contract provided deadlines for report submissions, and tied progress payments to timely completion of reports. The parties expected that throughout the design process there would be many changes to the reports, which contain express disclaimers that the information was preliminary and subject to modification.

During the PDR and CDR stages, if D3 could not include necessary data in a particular report, it could, as an alternative, submit a "Closure Plan" to note the missing

or incomplete data, outline the plan for obtaining that data, and state the expected date for doing so. The Closure Plan serves as a placeholder for missing or incomplete data.

After the PDR and CDR stages, the process moves into the production stage, during which the designs continue to evolve as blueprints are created and manufacturing commences. The manufacturer (or subcontractor) then conducts extensive testing of the entire aircraft to ensure the safety and integrity of the final aircraft design. The last stage is the "Certification Phase" during which the regulatory authorities approve the final aircraft design. This approval involves Federal Aviation Administration (FAA) review of all final engineering drawings, reports and data, and observations of all required testing. Upon successful completion of this rigorous review, the regulatory authorities issue a " 'Type Certification' " certifying that the aircraft meets the airworthiness requirements.

In February 2010, D3 submitted a vibration report, prepared by Terry, as part of its PDR submission to Mitsubishi. Shortly after, Mitsubishi rejected the report, concluding the report lacked necessary data regarding the stress and vibration levels for the tailcone assembly and its components within the actual " 'vibration environment' " (the environment to which the parts would be exposed during the aircraft's use). Under its contractual obligations, D3 was required to revise and resubmit all of the rejected reports by March 31, 2010.

D3 immediately directed Terry to prepare a revised vibration report substantiating that the tailcone assembly and its components are safe for the environment to which they would be exposed, i.e., the system components of the tailcone assembly were properly designed for the particular vibration environment. Based on his expertise, Terry

concluded that this certification required data regarding the particular vibration environment to which the tailcone would be exposed. Without the underlying data, Terry believed he "would be falsely stating" that this portion of the aircraft "met safety requirements."

During the next several weeks, Terry sought to obtain the necessary data from Mitsubishi and from a subcontractor, both of which had access to this information. However, neither the subcontractor nor Mitsubishi responded with the necessary information. In response, Terry repeatedly informed his supervisors that he could not prepare the requested report without the underlying data because of safety concerns. Terry made it "very clear to management in all levels of supervision" that he would not sign the report "without the vibration environment being defined to me."

After Terry made additional unsuccessful efforts to obtain the vibration environment data, D3 began to pressure him to prepare and sign a report certifying that "the system components had been properly assessed against the environment to which they would be exposed." Terry resisted, believing such statement would be false. Terry said: "Pressure was put on me to ignore aspects of the technical assessment, specifically, the need to compare the specification levels of equipment to the environment and conclude that they were safe for flight."

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