Honeywell Int'l, Inc. v. United States

756 F. Supp. 3d 1346, 2025 CIT 13
CourtUnited States Court of International Trade
DecidedJanuary 30, 2025
Docket17-00256
StatusPublished

This text of 756 F. Supp. 3d 1346 (Honeywell Int'l, Inc. v. United States) is published on Counsel Stack Legal Research, covering United States Court of International Trade primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

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Honeywell Int'l, Inc. v. United States, 756 F. Supp. 3d 1346, 2025 CIT 13 (cit 2025).

Opinion

Slip Op. 25-13

UNITED STATES COURT OF INTERNATIONAL TRADE

HONEYWELL INTERNATIONAL, INC.,

Plaintiff, Before: Mark A. Barnett, Chief Judge v. Court No. 17-00256 UNITED STATES,

Defendant.

OPINION

[Court grants Plaintiff’s motion for summary judgment and denies Defendant’s cross- motion for summary judgment because subject imports are correctly classified under subheading 8803.20.00 of the Harmonized Tariff Schedule of the United States.]

Dated: January 30, 2025

Wm. Randolph Rucker, Faegre Drinker Biddle & Reath, LLP, of Chicago, IL, argued for Plaintiff Honeywell International, Inc.

Edward F. Kenny, Senior Trial Counsel, Commercial Litigation Branch, Civil Division, U.S. Department of Justice, of New York, NY, argued for Defendant United States. On the brief were Brian M. Boynton, Principal Deputy Assistant Attorney General, Patricia M. McCarthy, Director, Justin R. Miller, Attorney in Charge, International Trade Field Office, and Aimee Lee, Assistant Director. Of counsel on the brief was Yelena Slapek, Office of the Assistant Chief Counsel, International Trade Litigation, U.S. Customs and Border Protection.

Barnett, Chief Judge: Plaintiff Honeywell International, Inc. (“Honeywell”)

commenced this case to contest the denial of three protests challenging U.S. Customs

and Border Protection’s (“Customs” or “CBP”) liquidation of Honeywell’s radial, web,

and chordal segments (the “imported segments” or “segments”) under subheading

6307.90.98 of the Harmonized Tariff Schedule of the United States (“HTSUS”), as

“[o]ther made up articles, including dress patterns,” dutiable at seven percent ad Court No. 17-00256 Page 2

valorem. Summons, ECF No. 1; Second Am. Compl., ECF No. 34. 1 Plaintiff alleges

that the segments are properly classified pursuant to HTSUS subheading 8803.20.00 as

“[p]arts of goods of heading 8801 or 8802: . . . [u]ndercarriages and parts thereof,” a

duty-free provision applicable to parts of aircraft. Second Am. Compl. ¶ 30. Honeywell

seeks summary judgment accordingly. Pl.’s Mot. for Summ. J., and accompanying

Mem. of Law in Supp. of Pl.’s Mot. for Summ. J. (“Pl.’s Mem.”), ECF No. 43. 2

Defendant United States (“the Government”) has cross-moved for summary judgment,

seeking classification of the segments pursuant to HTSUS subheading 6307.90.98. 3

Def.’s Cross-Mot. for Summ. J., and accompanying Mem. in Opp’n to Pl.’s Mot. for

Summ. J and in Supp. of Def.’s Cross-Mot. for Summ. J. (“Def.’s Cross-Mem.”), ECF

No. 54. For the reasons discussed herein, the court will enter judgment for Plaintiff.

1 All citations to the HTSUS are to the 2015 version, as determined by the date of

importation of the merchandise. See LeMans Corp. v. United States, 660 F.3d 1311, 1314 n.2 (Fed. Cir. 2011). 2 Plaintiff initially filed Exhibits A, B, and D appended to its motion for summary

judgment under seal. See ECF Nos. 42-1, 42-2, 42-4. Plaintiff later sought, and obtained, leave to unseal those exhibits. See Order (June 10, 2024), ECF No. 52; ECF Nos. 53, 53-1, 53-2 (Pl.’s Exhibits A, B, and D, respectively). In the filings accompanying Plaintiff’s motion to unseal, Plaintiff labeled Exhibits A, B, and D as Exhibits 1, 2, and 3. For consistency with the parties’ references to the exhibits in their briefs, the court refers to the exhibits as Exhibits A, B, and D. 3 Defendant is not seeking deference for Customs’ basis for rejecting heading 8803 as a

potential classification and advances different arguments in that regard. Oral Arg. at 1:23:05–1:23:20 (time stamp from the recording), https://www.cit.uscourts.gov/audio- recordings-select-public-court-proceedings; see also United States v. Mead Corp., 533 U.S. 218, 235 (2001) (the court affords deference to CBP’s classification rulings relative to their “power to persuade”) (quoting Skidmore v. Swift & Co., 323 U.S. 134, 140 (1944)). Court No. 17-00256 Page 3

BACKGROUND I. Material Facts Not In Dispute

A party moving for summary judgment must show “there is no genuine dispute as

to any material fact and the movant is entitled to judgment as a matter of law.” U.S.

Court of International Trade (“USCIT”) Rule 56(a). Parties submitted separate

statements of undisputed material facts with their respective motions and responses to

the opposing party’s statements. Confid. Pl.’s Statement of Material Facts Not In

Dispute (“Pl.’s SOF”), ECF No. 42; Def.’s Resp. to Pl.’s Statement of Material Facts Not

In Issue (“Def.’s Resp. Pl.’s SOF”), ECF No. 54; Def.’s Statement of Undisputed

Material Facts (“Def.’s SOF”), ECF No. 54; Pl.’s Resp. to Def.’s Statement of

Undisputed Material Facts (“Pl.’s Resp. Def.’s SOF”), ECF No. 60. Upon review of the

Parties’ facts (and supporting exhibits), 4 the court finds the following undisputed and

material facts.

Honeywell is the importer of record for the segments and made the subject

entries through the ports of Minneapolis, Charlotte, and Atlanta in 2015 and 2016. Pl.’s

4 The Government submitted physical samples of the segments, a needled preform, and

aircraft brake discs for the court’s review. See Def.’s Form 23, ECF No. 56. The physical samples are designated as Defendant’s Physical Exhibits 2 (chordal segment), 3 (radial segment), 4 (web segment), 18 (needled preform), 19 (densified carbon-carbon aircraft brake disc (stator)), and 20 (densified carbon-carbon aircraft brake disc (rotor)). “A rotor is a rotating disc used in an aircraft brake assembly that is keyed to the wheel assembly and provides friction and heat absorption during braking.” Pl.’s SOF ¶ 30; see also Def.’s Resp. Pl.’s SOF ¶ 30 (admitting without waiving objection as to cited authority). A stator, including auxiliary stators referred to as the pressure plate and the backing plate, “is a stationary disc used in an aircraft brake assembly that is keyed to the torque tube and provides friction and heat absorption during braking.” Pl.’s SOF ¶ 31; Def.’s Resp. Pl.’s SOF ¶ 31. Court No. 17-00256 Page 4

SOF ¶¶ 1–3; Def.’s Resp. Pl.’s SOF ¶¶ 1–3. At the time of entry, Honeywell classified

the segments under either subheading 6307.90.98 or 8803.20.00. Def.’s Resp. Pl.’s

SOF ¶ 4 (citing Customs documentation filed pursuant to USCIT Rule 73.1); see also

Pl.’s SOF ¶ 4 (averring entry classification under subheading 6307.90.98). Customs

liquidated the segments under subheading 6307.90.98. Pl.’s SOF ¶ 5; Def.’s Resp.

Pl.’s SOF ¶ 5.

The segments are made from nonwoven polyacrylonitrile (“PAN”) fiber fabric

material that is cut to a specific shape and size as described in one of three Engineering

Material Specifications: EMS-182, EMS-183, or EMS-270. Pl.’s SOF ¶¶ 11–12; Def.’s

Resp. Pl.’s SOF ¶¶ 11–12; see also Pl.’s SOF ¶ 21; Def.’s Resp. Pl.’s SOF ¶ 21

(admitting that “the segments are cut to a specific inner radius and outer radius”).

The below diagram, taken from patents for the segments, depicts the shape of

the segments in relation to the PAN fiber fabric material from which the segments are

cut:

Pl.’s Ex. D at 4, ECF No. 53-2. Court No. 17-00256 Page 5

As shown above, the segments are arc shaped. Id.; Pl.’s SOF ¶¶ 15, 18; Def.’s

Resp. Pl.’s SOF ¶¶ 15, 18. The court’s inspection of the segments indicates that each

segment is approximately ten and a half inches across at its widest portion,

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