Patricia LaCourse v. Defense Support Services LLC

980 F.3d 1350
CourtCourt of Appeals for the Eleventh Circuit
DecidedNovember 17, 2020
Docket19-13883
StatusPublished
Cited by15 cases

This text of 980 F.3d 1350 (Patricia LaCourse v. Defense Support Services LLC) is published on Counsel Stack Legal Research, covering Court of Appeals for the Eleventh Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Patricia LaCourse v. Defense Support Services LLC, 980 F.3d 1350 (11th Cir. 2020).

Opinion

USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 1 of 28

[PUBLISH]

IN THE UNITED STATES COURT OF APPEALS

FOR THE ELEVENTH CIRCUIT ________________________

No. 19-13883 ________________________

D.C. Docket No. 3:16-cv-00170-RV-HTC

PATRICIA LACOURSE, Individually and as personal representative of the Estate of Lt. Colonel Matthew LaCourse,

Plaintiff - Appellant,

versus

PAE WORLDWIDE INCORPORATED, et al.,

Defendants,

DEFENSE SUPPORT SERVICES LLC, Witness 7, Witness 8, Witness 9, JOHN DOES, 1 through 10 inclusive, Defendants - Appellees. ________________________

Appeal from the United States District Court for the Northern District of Florida ________________________

(November 17, 2020) USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 2 of 28

Before WILSON, NEWSOM, and ANDERSON, Circuit Judges.

NEWSOM, Circuit Judge:

This appeal requires us to decide whether and to what extent the Death on

the High Seas Act, 46 U.S.C. §§ 30301–08, applies to Patricia LaCourse’s

wrongful-death action, in which she alleges that PAE Worldwide Incorporated

failed to properly service and maintain the F-16 that her husband was flying when

it crashed into the Gulf of Mexico. We must also determine whether PAE, which

was operating under a services contract with the United States Air Force, is

shielded from liability by the so-called “government contractor” defense.

For the reasons that follow, we hold that DOHSA governs LaCourse’s

action, that it provides LaCourse’s exclusive remedy and preempts her other

claims, and that PAE is entitled to the protection of the government-contractor

defense.

I

A

The tragic story underlying this appeal began when an Air Force F-16

fighter jet departed Tyndall Air Force Base, east of Panama City, Florida, for a

continuation-training sortie. The only person on board was the pilot, Matthew

LaCourse, a retired Air Force Lieutenant Colonel employed as a civilian by the

Department of Defense. The plan was for Lt. Col. LaCourse to take the jet out

2 USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 3 of 28

over the Gulf of Mexico, perform a series of training maneuvers, and then return to

Tyndall. Unfortunately, he never came back. During the flight—for reasons the

parties dispute—the F-16 crashed into the Gulf more than twelve nautical miles

offshore. Sadly, Lt. Col. LaCourse was killed.

Five years prior to the accident, PAE’s predecessor—Defense Support

Services—had been awarded a contract with the Air Force to provide aircraft

service and maintenance at Tyndall, including, as it turns out, on the F-16 that Lt.

Col. LaCourse was flying when he crashed. In performing under the contract, PAE

was required to follow detailed guidelines and adhere to specific standards,

including Air Force Instructions (AFIs), Technical Orders (TOs), and Job Guides

(JGs), all of which were prepared by or on behalf of the Air Force.

F-16s are equipped with two hydraulic systems: A and B. The systems

operate independently of one another and are designed to allow the plane to

continue to fly in the event that one of them fails. Beginning two months before

the crash, the jet at issue here experienced a succession of problems that implicated

one or both of its hydraulic systems. In particular, on separate occasions: (1)

hydraulic fluid was discovered in the outboard flight-control accumulator gauge;

(2) System B’s hydraulically actuated landing gear twice failed to retract during

flight; (3) a hydraulic system pressure-line clamp on System A broke; (4) System

B’s reservoir accumulator was found to be depleted; (5) a pre-flight control check

3 USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 4 of 28

revealed a hydraulic leak; (6) System A’s cockpit indicator showed no pressure

and System B’s flight-control accumulator pre-charge was low; and (7) both

systems failed a “confidence run.”1 The F-16 was serviced and parts were repaired

or replaced as these problems were identified.

On the day of the crash, the F-16 experienced two issues shortly before

takeoff. First, the emergency-power unit took longer than expected to activate

during the pre-flight check. Second, and more importantly for our purposes, the jet

initially failed the “pitch-override check”—in which the pilot applies full pressure

to the stick and presses a switch to make the stabilizers at the tail move a few

inches or degrees in a nose-down direction. Despite these two “hiccups,” as one

witness called them, the jet ultimately passed all of its pre-flight checks, which

indicated no problem with the hydraulic systems. The PAE mechanics who

conducted the pre-flight checks were satisfied that the plane was safe to operate,

and they released it for flight.

During the sortie, the F-16 performed a number of aerial maneuvers leading

up to a “pitch-back”—an over-the-shoulder tactical maneuver in which the pilot

uses the pitch axis to rejoin another aircraft. By all accounts, everything leading

up to the pitch-back appeared normal—i.e., no gauge, light, warning, or caution

1 The district court assumed that each of these problems was related to the hydraulic systems for purposes of deciding LaCourse’s claims on summary judgment but noted that this was “far from certain.” 4 USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 5 of 28

indicated any problem, and there were no reports of any vibrations, shakes, etc.

The issue that led to the crash occurred at the end of the pitch-back maneuver—Lt.

Col. LaCourse appeared to level off and there followed, as one witness described

it, “a period of no data, no inputs, no control or . . . no maneuvers,” at which point

the jet entered a “pitch-down” from about 12,000 feet. There is no evidence that

Lt. Col. LaCourse made any effort to eject or radio for help during his final

descent.2

B

Lt. Col. LaCourse’s widow and personal representative, Patricia LaCourse,

filed this wrongful-death action and jury demand in Florida state court alleging

state-law claims for negligence, breach of warranty, and breach of contract. PAE

removed the case to federal court based on federal-officer jurisdiction, diversity

jurisdiction, and jurisdiction under DOHSA—which, in relevant part, confers

admiralty jurisdiction “[w]hen the death of an individual is caused by wrongful act,

neglect, or default occurring on the high seas.” 46 U.S.C. § 30302. Resisting

PAE’s removal, LaCourse disputed that federal jurisdiction existed on any basis.

2 Although it has no real bearing on the issues before us, it’s worth noting—by way of background—that the parties vigorously dispute the crash’s cause. LaCourse and her experts blame the F-16’s dual-hydraulic system, as well as PAE’s failure to discover, diagnose, and address the problems. PAE and its experts, by contrast, posit that Lt. Col. LaCourse suffered a G-induced loss of consciousness following the pitch-back. 5 USCA11 Case: 19-13883 Date Filed: 11/17/2020 Page: 6 of 28

Once in federal court, PAE moved for partial summary judgment, arguing

that DOHSA governed LaCourse’s suit and, accordingly, that any potential

recovery should (per the statute) be limited to pecuniary damages. The district

Free access — add to your briefcase to read the full text and ask questions with AI

Related

Cite This Page — Counsel Stack

Bluebook (online)
980 F.3d 1350, Counsel Stack Legal Research, https://law.counselstack.com/opinion/patricia-lacourse-v-defense-support-services-llc-ca11-2020.