Terry v. D3 Technologies CA4/1

CourtCalifornia Court of Appeal
DecidedMarch 27, 2014
DocketD063395
StatusUnpublished

This text of Terry v. D3 Technologies CA4/1 (Terry v. D3 Technologies CA4/1) 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
Terry v. D3 Technologies CA4/1, (Cal. Ct. App. 2014).

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Filed 3/27/14 Terry v. D3 Technologies CA4/1 NOT TO BE PUBLISHED IN OFFICIAL REPORTS California Rules of Court, rule 8.1115(a), prohibits courts and parties from citing or relying on opinions not certified for publication or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 This opinion has not been certified for publication or ordered published for purposes of rule 8.1115.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. 2 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

3 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

4 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

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