Bocker v. Hartzell Engine Technologies LLC

CourtDistrict Court, D. Delaware
DecidedJanuary 26, 2023
Docket1:21-cv-01174
StatusUnknown

This text of Bocker v. Hartzell Engine Technologies LLC (Bocker v. Hartzell Engine Technologies LLC) is published on Counsel Stack Legal Research, covering District Court, D. Delaware primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Bocker v. Hartzell Engine Technologies LLC, (D. Del. 2023).

Opinion

IN THE UNITED STATES DISTRICT COURT FOR THE DISTRICT OF DELAWARE

HANNA BOCKER, SARAH BOCKER ) and BARBARA BOCKER as ) Administrator of the Estate of GERARD ) BOCKER and BARBARA BOCKER, ) Individually, ) ) Plaintiffs, ) ) v. ) Civil Action No. 21-1174-MN-CJB ) HARTZELL ENGINE TECHNOLOGIES, ) LLC and CONTINENTAL AEROSPACE ) TECHNOLOGIES, INC. f/k/a ) CONTINENTAL MOTORS, INC., ) ) Defendants. )

REPORT AND RECOMMENDATION In this action filed by Plaintiffs Hannah Bocker, Sarah Bocker and Barbara Bocker Individually and as Administrator of the Estate of Gerard Bocker (“Plaintiffs”), presently before the Court is Defendant Continental Aerospace Technologies, Inc. f/k/a Continental Motors, Inc.’s (“Continental”) motion to dismiss Plaintiffs’ Second Amended Complaint (“SAC”) against it, or to strike portions of the SAC, pursuant to Federal Rules of Civil Procedure 12(b)(6) and 12(f) (the “Motion”). (D.I. 50) For the reasons that follow, the Court recommends that the Motion be GRANTED and that the SAC’s claims against Continental be dismissed. I. BACKGROUND A. Factual Background This matter arises from the August 17, 2019 crash of a Cessna T303 aircraft (the “aircraft”) in Lagrangeville, New York. (D.I. 48 at ¶ 17) The aircraft was piloted by Francisco Knipping-Diaz and it held two passengers, Teofilo Antonio Diaz and Eduardo Tio. (Id. at ¶¶ 20- 21) Shortly after takeoff from an airport in Lagrangeville, the aircraft lost engine power at a low altitude and was unable to climb. (Id. at ¶¶ 22, 25, 62) As a result of this failure to climb, the pilot lost directional control and the aircraft began to drift left; thereafter, it rolled left and ultimately crashed and hit the Bocker family’s residence. (Id. at ¶¶ 26-27, 62, 64-65) Both the aircraft and the Bocker residence burst into flames. (Id. at ¶¶ 29, 65)

Inside the Bocker residence at the time were Gerard Bocker and his daughters, Plaintiffs Hannah Bocker and Sarah Bocker. (Id. at ¶¶ 5, 28) Mr. Bocker died due to the crash. (Id. at ¶ 31) Hannah Bocker lived but was severely burned. (Id. at ¶ 32) Sarah Bocker also lived; she was able to jump out of a window of the house and suffered some resulting injuries. (Id. at ¶ 33) Plaintiff Barbara Bocker, Mr. Bocker’s wife and the mother of Hananh and Sarah Bocker, was not on site; she was later named as the Administrator of Mr. Bocker’s estate. (Id. at ¶¶ 3, 5; D.I. 51 at 2) The pilot, Mr. Knipping-Diaz, died in the crash, while the two passengers survived. (D.I. 48 at ¶¶ 20-21) The aircraft was equipped with two (L)TSIO-520-AE3B piston engines (“the engines”); these engines were designed and manufactured by Continental. (Id. at ¶¶ 36-37) The SAC

alleges that the reason the aircraft crashed was that its engines were not capable of making sufficient power to remain airborne and suffered a “powerplant failure[,]” leaving them “unable to perform as a result.” (Id. at ¶¶ 67, 73) The SAC also makes clear, in turn, that: (1) the engines were “equipped with turbo components[,]” referred to in the SAC as “turbochargers[,]” which had been “incorporat[ed]” into the engines at some point after the engines were manufactured; (2) the purpose of turbocharging an engine is to increase its performance at higher altitudes, as the air thins and becomes less dense, so that the fuel/air mixture can remain at or close to sea level; and (3) it was these turbochargers that “malfunction[ed]” and that “cause[d]

2 and contribute[d] to the power loss experienced on board the aircraft[,]” resulting in the crash. (Id. at ¶¶ 36, 45, 79, 89; see also D.I. 51 at 10; D.I. 55 at 4) The SAC appears to allege two possible theories as to why or how the aircraft crashed, both of which appear to be related to the engine’s turbochargers.1 First, it notes that if the

fuel/air mixture provided to the engine is not appropriate, or if the aircraft does not provide sufficient fuel or fuel free of contaminants, then the engine will not be able to make “rated power[.]” (D.I. 48 at ¶¶ 68, 71) The SAC also explains that if a “turbocharger malfunctions or seizes” then this can cause the engine to “not receive an appropriate fuel/air mixture and [that will, in turn] cause a loss of power.” (Id. at ¶ 46) And it asserts that just before the crash, “the signatures in the propellers and control levers confirm that the aircraft was not making rated power on takeoff.” (Id. at ¶ 72) Second, the SAC notes that “investigation reveal[ed] that the aircraft’s turbocharger wastegates were in vastly different positions, with the left wastegate nearly closed, confirming that the engine was demanding additional boost in reaction to a malfunction of the engine” and that post-accident, there was evidence of a “turbocharger seizure

or induction blockage” that had caused the left “wastegate on [the] engine [to] attempt to raise the manifold pressure[.]” (Id. at ¶¶ 69-70) In the factual background sections of the SAC,2 Plaintiffs repeatedly plead that Defendant Hartzell Engine Technologies, LLC (“Hartzell”) “made” and “manufactured” the

1 It could be that these allegations (which are mixed together largely in paragraphs 68 to 72 of the SAC) are not meant to reference to two separate theories, but instead one combined theory. It is difficult to say since the SAC, as will be further discussed below, is difficult to construe. 2 The SAC is structured as follows. First, there is a section titled “The Parties” (which provides some basic factual allegations about the parties to the suit) and one titled “Jurisdiction and Venue” (which includes Plaintiffs’ allegations about those subjects). (D.I. 48 at ¶¶ 1-16) Next, there are three sections in which Plaintiffs appear to be laying out the facts 3 turbochargers and their associated components (including wastegates and controllers) that were a part of the engines in the accident aircraft; the SAC also states that these turbochargers were “the responsibility of the defendant Hartzell.” (Id. at ¶¶ 47, 49, 79, 89) Although Hartzell manufactured the turbochargers and was responsible for them, in these factual background

sections, the SAC also avers that Continental “specified and procured” the turbochargers or was responsible for their “design and procurement.” (Id. at ¶¶ 49, 85; see also id. at ¶¶ 87, 89) Moreover, at various places in the SAC, it is alleged that Continental was the “type certificate holder” and the “production [certificate] holder” for the aircraft’s engines, and that this meant that Continental: (1) “had a duty to ensure that the engines were airworthy and safe, and would not suffer a sudden and unforeseen loss of power”; (2) “was responsible to ensure that the engines, including their turbocharging systems, functioned”; (3) “holds responsibility for airworthiness and functionality of the engine assembly, to specifically include its turbocharging system”; and (4) bears “ultimate responsibility for the defects in the turbocharging systems of the accident engines[.]” (Id. at ¶¶ 19, 81-82, 86, 88)

Further relevant allegations in the SAC will be discussed in Section II below. B. Procedural Background Plaintiffs filed their original Complaint initiating this case on August 12, 2021. (D.I. 1) Shortly thereafter, Plaintiffs filed a First Amended Complaint (“FAC”). (D.I. 9) United States

relevant to the accident and, relatedly, to the allegations of liability later found in the Counts of the SAC: “Factual Background[,]” “Background of the Accident Aircraft and its Engines” and “Accident Investigation[.]” (Id. at ¶¶ 17-89) For ease of reference, the Court has and will refer to these three sections herein as the “factual background” sections of the SAC. Next there is a section titled “Damages” that includes the allegations related to that topic. (Id.

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

Related

Ashcroft v. Iqbal
556 U.S. 662 (Supreme Court, 2009)
Mora v. University of Texas Southwestern Medical Center
469 F. App'x 295 (Fifth Circuit, 2012)
Fowler v. UPMC SHADYSIDE
578 F.3d 203 (Third Circuit, 2009)
Delaware Health Care, Inc. v. MCD Holding Co.
893 F. Supp. 1279 (D. Delaware, 1995)
Sliger v. Prospect Mortgage, LLC
789 F. Supp. 2d 1212 (E.D. California, 2011)
Smith v. Liberty Mutual Insruance Company
201 A.3d 555 (Superior Court of Delaware, 2019)
Jaroslawicz v. M&T Bank Corp
962 F.3d 701 (Third Circuit, 2020)
Schultes v. Kane
50 A.D.3d 1277 (Appellate Division of the Supreme Court of New York, 2008)
Fitzpatrick v. Currie
52 A.D.3d 1089 (Appellate Division of the Supreme Court of New York, 2008)
Earsing v. Nelson
212 A.D.2d 66 (Appellate Division of the Supreme Court of New York, 1995)
Barclay v. Techno-Design, Inc.
129 A.D.3d 1177 (Appellate Division of the Supreme Court of New York, 2015)
Carson Optical Inc. v. eBay Inc.
202 F. Supp. 3d 247 (E.D. New York, 2016)
Jaroslawicz v. M&T Bank Corp.
296 F. Supp. 3d 670 (D. Delaware, 2017)
Sincavage v. Barnhart
171 F. App'x 924 (Third Circuit, 2006)
Henderson v. Carlson
812 F.2d 874 (Third Circuit, 1987)

Cite This Page — Counsel Stack

Bluebook (online)
Bocker v. Hartzell Engine Technologies LLC, Counsel Stack Legal Research, https://law.counselstack.com/opinion/bocker-v-hartzell-engine-technologies-llc-ded-2023.