`Declaration of John F. Grabowsky
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`Submitted on behalf of Seymour Levine
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`UNITED STATES PATENT AND TRADEMARK OFFICE
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`________________
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`BEFORE THE PATENT TRIAL AND APPEAL BOARD
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`________________
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`THE BOEING COMPANY
`Petitioner,
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`v.
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`SEYMOUR LEVINE
`Patent Owner
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`________________
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`Case IPR2015-01341
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`Patent RE039,618
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`_________________
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`DECLARATION OF JOHN F. GRABOWSKY IN SUPPORT OF PATENT
`OWNER’S RESPONSE PURSUANT TO 37 C.F.R. § 42.120
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`I, John F. Grabowsky, declare as follows:
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`Case IPR 2015-01341
`Declaration of John F. Grabowsky
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`1.
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`I have been retained by counsel for Patent Owner Seymour Levine as
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`an expert witness to provide testimony in the above-captioned Inter Partes Review
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`proceeding including on issues relating to the validity of U.S. Reissue Patent
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`RE39,618 (“the ’618 patent”) entitled Remote, Aircraft, Global, Paperless
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`Maintenance System. I make this Declaration based upon facts and matters within
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`my own knowledge.
`2.
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`In this IPR, I understand that the Patent Office has instituted a review
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`of claims 4, 5, 8, 9, 10, 14 and 16 of the ’618 patent based on various combinations
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`of references.
`3.
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`In preparation for this declaration, I have reviewed and am now
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`familiar with the following materials:
`a. The ‘618 patent including the specification and claims (Ex.
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`1001);
`b. Petition for Inter Partes Review of the ’618 patent dated June
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`4, 2015;
`c. Declaration of Dr. Albert Helfrick in Support of Petition for
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`Inter Partes Review of U.S. Patent No. RE 39,618 (Ex. 1002);
`d. Decision on Institution of Inter Partes Review of the ’618
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`patent dated December 21, 2015;
`e. Aeronautical Radio, Inc., Design Guidance for Onboard
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`Maintenance System: ARINC Characteristic 624-1 (1993)
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`(“ARINC 624-1”) (Ex. 1014);
`f. Ward, Power Plant Health Monitoring-The Human Factor,
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`Royal Aeronautical Society, Tenth Annual Symposium (1992)
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`(“Ward”) (Ex. 1015);
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`g. Aeronautical Radio, Inc., Flight Management Computer
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`System: ARINC Characteristic 702-6 (1994) (“ARINC 702-6”)
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`(Ex. 1016);
`h. Farmakis et al., U.S. Patent No. 5,714,948 (“Farmakis”) (Ex.
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`1021);
`i. Chetail, Le CFM 56-6 Sur A320 A Air France, NATO
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`Advisory Group for Aerospace Research and Development,
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`June 1988 (“Chetail”) (Ex. 1018);
`j. Dyson, Commercial Engine Monitoring Status At GE Aircraft
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`Engines, NATO Advisory Group for Aerospace Research and
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`Development, June 1988 (“Dyson”) (Ex. 1019).
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`4.
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`In making the statements, and reaching my opinions and conclusions
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`stated herein, I have considered the documents cited above in the context of my
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`own education, training, knowledge, and personal and professional experience,
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`including knowledge of the state of the art and the perspective of a person of
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`ordinary skill in the art at the time of the invention of the subject matter described
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`and claimed in the ’618 patent (i.e., 1995).
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`5.
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`I am being compensated for my time in connection with this IPR at a
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`rate of $500 per hour. My compensation is in no way dependent on, nor affects,
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`the substance of my statements in this Declaration. I have no direct financial
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`interest in the ’618 patent.
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`I.
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`BACKGROUND AND QUALIFICATIONS
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`6.
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`I have more than 45 years experience in the aerospace industry. I
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`earned a Bachelor’s Degree in Electrical Engineering from Lehigh University in
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`1969 and have worked in both the defense and commercial aerospace sectors
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`throughout my career. I was most recently the Chief Technology Office of
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`AeroVironment, Inc., where, among other responsibilities, I assisted
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`in
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`establishing technical direction for Unmanned Aircraft Systems.
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`7.
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`I am the named inventor on a patent directed to an aircraft flight data
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`acquisition and transmission system for commercial aircraft. My Curriculum
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`Vitae detailing my experience and qualifications is attached as Exhibit 2012.
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`II. ONE OF ORDINARY SKILL IN THE ART
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`8.
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`Based on the technologies disclosed in the ’618 patent, one of
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`ordinary skill in the art would have at least a B.S. degree in electrical, systems, or
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`computer engineering, or an FAA Mechanic Certificate with an airframe rating in
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`accordance with 14 CFR part 65.71 and 65.85; as well as either an M.S. or
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`equivalent work experience, such as 3-5 years of experience in avionics.
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`9.
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`As a result of my more than 45-years’ experience in the aerospace
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`industry, I am very familiar with technology at issue. Accordingly, I am qualified
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`to provide expert opinions on the technology described in the ’618 patent as well
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`as the teachings of the cited references.
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`III. LEGAL STANDARDS
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`A. Claim Construction Standard
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`10.
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`I understand that in this Inter Partes Review, claims are to be given
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`their broadest reasonable construction in light of the specification as would be
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`read by a person of ordinary skill in the relevant art at the time of the invention.
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`B. Obviousness
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`11.
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`I have an understanding of the term “obviousness” based on my
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`experience with patents and based upon explanations provided to me by counsel in
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`this and other matters.
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`12.
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`I understand that to establish obviousness, one must construe the
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`scope of the prior art, identify the differences between the claims and the prior art,
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`and determine the level of skill in the pertinent art at the time of the invention.
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`There then must be an explicit, cogent reason based on the foregoing why it would
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`be obvious to modify the prior art to arrive at the claimed invention.
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`13.
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`It is my understanding that the analysis of the prior art with respect to
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`a determination of obvious/non-obviousness includes evidence relevant to the
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`finding of whether there is a teaching, motivation, or suggestion to select and
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`combine the references relied on as evidence of obviousness, though the analysis
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`is not limited to these issues. It is my further understanding that the motivation,
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`suggestion or teaching may come explicitly from statements in the prior art, the
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`nature of the problem to be solved or may be found explicitly or implicitly in
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`market forces, design incentives, the interrelated teachings of multiple patents,
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`known needs or problems in the art of the invention, and/or the background
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`knowledge, creativity, and common sense of a person of ordinary skill.
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`14.
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`It is my understanding that reconstructive hindsight based on the
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`invention to defeat the validity of the claimed invention is not permitted. Further,
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`whether a reference teaches away from the claimed invention must be considered
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`when determining a case of obviousness. The combination of references must
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`either expressly disclose the claimed invention as a whole, or suggest to one of
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`ordinary skill in the art modifications needed to meet all the claim limitations.
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`15.
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`It is also my understanding that certain secondary considerations
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`(including commercial success, long felt need in the industry, failure of others,
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`commercial acquiescence, copying, praise for the invention, professional approval
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`and recognition of the invention publications) are to be considered in determining
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`whether patent claims are non-obvious. In support of patent validity, there must be
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`a nexus between the claimed invention and the evidence of the secondary
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`consideration.
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`IV. PRIOR ART
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`A. Combination of Ward and ARINC 624-1 with ARINC 702-6
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`16. Ward is a paper discussing the history and progress of condition
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`monitoring systems for aircraft, including aircraft engines. It is expressly
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`concerned with gathering information to enable the timely and efficient
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`maintenance of the aircraft and/or systems on the aircraft. See, e.g., Ex. 1015 at 8.
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`Ward is not concerned with any other aspect of aircraft operation.
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`17. ARINC 624-1 is an ARINC report titled Design Guidance for
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`Onboard Maintenance System. It provides guidance on the design of an onboard
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`maintenance system (OMS), which includes as its central component a central
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`maintenance computer (CMC). See, Ex. 1014 at § 3.1. The sole focus of this
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`documents is aircraft maintenance.
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`18. ARINC 702-6 is an ARINC characteristic titled Flight Management
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`Computer System. Its purpose is to set forth “the characteristics of a Flight
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`Management Computer System [(FMS)],” which is “designed to provide
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`performance data and fuel management display and control functions, and
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`navigation and guidance to a desired flight plan based on energy efficient
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`profiles.” Ex. 1016 at §§ 1.1-1.2. The FMS includes two major components, the
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`flight management computer (FMC) and the Control/Display Unit (CDU).” Id. at
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`§ 1.4. I am familiar with FMCs and the role they play on an aircraft. The FMC is
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`designed to provide its information to the pilot so that the pilot can manage the
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`flight plan and track the progress of the flight. None of the functions of the FMC
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`relates to aircraft maintenance and, to the extent information is sent to the ground,
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`none of that information is intended to facilitate maintenance. See, for example,
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`the list of downlink message in Attachment 8B, Section 4. None of these
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`messages relates to maintenance. Ex. 1016 at p. 81.
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`19.
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`In my opinion, one of ordinary skill in the art looking to solve
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`problems with existing aircraft maintenance systems and develop an aircraft
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`maintenance systems, such as the one claimed in the ’618 patent, would not have
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`looked to ARINC 702-6 for solutions. A person of ordinary skill in the art would
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`not, therefore, have been motivated to combine this document with Ward and
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`ARINC 624-1, which are maintenance-focused documents. There are many
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`systems onboard a commercial airplane with many that are generally unrelated.
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`See, the list of “Related Documents” in ARINC 624-1, which lists fifteen related
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`ARINC and other documents, but does not list ARINC 702-6. Ex. 1014 at §1.4.
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`In my opinion, therefore, it is incorrect to say, as Dr. Helfrick does, that just
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`because a commercial aircraft might have both the CMC described in ARINC
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`624-1 and the FMC described in ARINC 702-6, one of ordinary skill in the art
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`would have been motivated to combine these references in solving the problems
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`addressed by the claimed invention. See, Helfrick Decl. at ¶ 103.
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`B. Combination of Ward and ARINC 624-1 with Farmakis
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`20. Farmakis is a U.S. patent titled Satellite Based Aircraft Traffic
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`Control System. It is directed exclusively at “tracking and control of aircraft and
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`other vehicles” and it discloses downloading GPS and other position data solely
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`for the purpose of allowing the air traffic control facility to “continuously
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`monitor[] and track[] [the] aircraft.” Ex. 1021 at 1:13-15; 4:32-36. Farmakis is
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`unrelated to aircraft maintenance and does not disclose or even refer to aircraft
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`maintenance or an aircraft maintenance system.
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`21.
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`In my opinion, one of ordinary skill in the art looking to solve
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`problems with existing aircraft maintenance systems and develop an aircraft
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`maintenance systems, such as the one claimed in the ’618 patent, would not have
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`looked to Farmakis for solutions. A person of ordinary skill in the art would not,
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`therefore, have been motivated to combine this document with Ward and ARINC
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`624-1, which are maintenance-focused documents. In my opinion, therefore, it is
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`incorrect to say, as Dr. Helfrick does, that just because all of these references
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`disclose transmitting data from an aircraft to the ground during flight, one of
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`ordinary skill in the art would have been motivated to combine these references in
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`solving the problems addressed by the claimed invention. See, Helfrick Decl. at ¶
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`106. Moreover, communication of data from the aircraft to the ground is, at best,
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`incidental to Ward and ARINC 624-1, which, as discussed above, are directed
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`more broadly to aircraft maintenance systems.
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`C. Combination of Dyson and Chetail
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`1.
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`Claim Construction
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`22.
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`I understand that Petitioner has proposed a construction for the term
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`“maintenance advice” to mean “problem-specific maintenance information, such
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`as trends, alerts, or isolation of faults.” I disagree with this construction because it
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`does not adequately reflect how one of ordinary skill in the art would understand
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`this term in light of the specification of the ’618 patent.
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`23. The specification describes maintenance advisories, which
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`I
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`understand to refer to the messages containing the claimed “maintenance advice.”
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`According to the specification of the ’618 patent, maintenance advisories do more
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`than just relay alerts and other fault information received from the aircraft. It
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`describes them as “represent[ing] the latest diagnostic procedures and problem
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`specific maintenance information” ’618 patent at 7:1-2. The maintenance
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`advisories are “based on an expert system for fault isolation that will save both
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`time and money in getting a safe to fly aircraft back in service.” Id. at 3:35-39.
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`See also, id. at 7:61-65 (“The manufacturer’s facility 108 transmits expert system
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`repair advisories to the aircraft’s 10 maintenance personnel. These include the
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`latest approved, problem specific, service manual data to efficiently and safely
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`correct the aircraft’s problem.”)
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`24.
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`In my opinion, one of ordinary skill in the art would understand this to
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`mean that the expert system takes the data from the aircraft and, in addition to
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`calculating trends, issuing alerts and isolating any indicated faults, the system also
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`makes some recommendation for an appropriate maintenance action.
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`25. This is consistent with the plain and ordinary meaning of the word
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`“advice.” I have reviewed the dictionary definition cited by the Board in its
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`Institution Decision and believe that definition number 3: “recommendation
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`regarding a decision or course of conduct” is more consistent with how one of
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`ordinary skill in the art would understand this term in light of the specification
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`than definition number 4, relied on by the Board, “information or notice given.”
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`See Ex. 3001 at 3.
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`26.
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`In my opinion, the proper construction of the term “maintenance
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`advice” is “problem-specific maintenance information, including recommended
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`maintenance actions.”
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`2.
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`“Maintenance Advice” in the Combination of Dyson and
`Chetail
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`27. Dyson describes a commercial engine monitoring system from GE
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`Aircraft Engines. As described by Dr. Helfrick, Dyson discloses that software,
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`called “GEM” for “Ground-based Engine Monitoring” can generate alert
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`messages and trends and plots based on aircraft data sent to the ground. See,
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`Helfrick Decl. ¶ 83. I disagree with Dr. Helfrick’s conclusion that such data
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`represents “maintenance advice” as claimed in the ’618 patent.
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`28. The disclosed “alert messages and trend plots” tell a user what is
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`happening, but do not provide any information about what to do in response to the
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`alert or what maintenance might be suggested by the plotted trends. These “alert
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`messages and trend plots” do not recommend any specific action. In my opinion,
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`they do not provide any “advice” as that term would be properly understood by
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`one of ordinary skill in the art and do not, therefore, satisfy the claimed
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`“maintenance advice.”
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`29. Similarly with Chetail, which describes Air France’s operational
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`experience with “ground-based monitoring of jet-engine cruising data,” Ex. 1018
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`at 15-1, there is no disclosure of “maintenance advice.” Chetail describes a
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`system where engine data collected onboard an aircraft is transmitted to the
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`ground using the ACARS system. The data is received by “the closest SITA
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`ground-station” and then resent to the central computer at Air France. Id. at 15-2.
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`Once in the Air France system, the data is processed by the GEM system, the
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`same system used in Dyson, which “seeks to recognize commonplace errors as
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`soon as they appear.” Id. at 15-3. Chetail describes the algorithm used to detect
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`when a given parameter “is greater than or equal to a predetermined threshold.”
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`Id. When this occurs, “a message is automatically sent by the central calculator”
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`and “appears on screens in the Control Department” at the main maintenance
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`base. Id. This appears to be the same “alert” referred to in Dyson.
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`30. The message generated and sent by the Air France system described
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`in Chetail and relied on by Dr. Helfrick as the claimed “maintenance advice,”
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`simply alerts the maintenance personnel that some engine parameter has reached
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`or exceeded some threshold. It does not, however, provide any information about
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`what caused that parameter to exceed the threshold nor does it provide any advice
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`as to what the maintenance personnel should do to correct it. In my opinion, this
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`simple threshold exceedance alert does not provide any “advice” as that term
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`would be properly understood by one of ordinary skill in the art and does not,
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`therefore, satisfy the claimed “maintenance advice.”
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`I declare under penalty of perjury under the laws of the United States that
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`the foregoing is true and correct.
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`Executed March 28, 2016, at Maui, Hawaii.
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`John F. Grabowsky
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