DCT
2:20-cv-03471
CTAF Solutions LLC v. Rainbow Aircraft Inc
Key Events
Complaint
Table of Contents
complaint
I. Executive Summary and Procedural Information
- Parties & Counsel:
- Plaintiff: CTAF Solutions, LLC (Washington)
- Defendant: RAINBOW AIRCRAFT, INC. dba MGL AVIONICS (California)
- Plaintiff’s Counsel: SML Avvocati P.C.; Sand, Sebolt & Wernow Co., LPA
- Case Identification: 2:20-cv-03471, C.D. Cal., 04/14/2020
- Venue Allegations: Venue is alleged to be proper because Defendant is a California corporation with a regular and established place of business in the Central District of California.
- Core Dispute: Plaintiff alleges that Defendant’s line of iEFIS multi-function avionics displays infringes a patent related to systems and methods for displaying aircraft terrain awareness information.
- Technical Context: The technology concerns integrated avionics displays that provide pilots with situational awareness by graphically and textually presenting the aircraft's position relative to terrain, obstacles, and navigational waypoints.
- Key Procedural History: The complaint does not mention any prior litigation, Inter Partes Review (IPR) proceedings, or licensing history related to the patent-in-suit.
Case Timeline
| Date | Event |
|---|---|
| 2011-11-17 | U.S. Patent No. 10,389,396 Earliest Priority Date Claimed |
| 2019-08-20 | U.S. Patent No. 10,389,396 Issues |
| 2020-04-14 | Complaint Filed |
II. Technology and Patent(s)-in-Suit Analysis
U.S. Patent No. 10,389,396 - "TERRAIN AWARENESS AND WARNING AIRCRAFT INDICATOR EQUIPMENT"
- Patent Identification: U.S. Patent No. 10,389,396, issued August 20, 2019.
The Invention Explained
- Problem Addressed: The patent addresses the need for aircraft pilots, particularly when flying an instrument approach, to maintain situational awareness of their position relative to surrounding terrain, buildings, and other geographical features to ensure a safe distance is kept (’396 Patent, Abstract; col. 4:45-51). It also more broadly discusses challenges in managing radio communications and filtering relevant signals based on proximity and flight conditions, which requires precise locational data (’396 Patent, col. 5:1-col. 6:54).
- The Patented Solution: The invention provides a method and system for an avionics display that integrates multiple pieces of critical data. It uses a "terrain awareness and warning system" to identify a "location of interest" (e.g., an airport), calculates the aircraft's distance and bearing to that location, and then presents this information to the pilot in two distinct ways: first, as a graphical "aircraft situation display image" and second, as explicit textual or numerical values for the "calculated distance value and the calculated bearing value" (’396 Patent, col. 23:51-col. 24:62). This dual-mode presentation is a core feature of the asserted claims.
- Technical Importance: The technology aims to enhance flight safety by consolidating data from systems like GPS and geographical databases into a single, intuitive display, reducing pilot workload during critical flight phases (’396 Patent, col. 4:41-51).
Key Claims at a Glance
- The complaint asserts independent claims 1 (a method) and 13 (a system) (Compl. ¶¶14, 15).
- Independent Claim 1 (Method):
- determining a location of interest relative to an aircraft using a terrain awareness and warning system;
- calculating a distance value and a bearing value for the location of interest relative to the aircraft;
- providing first display data to an electronic display... to show an aircraft situation display image indicating the location of interest relative to the aircraft; and
- providing second display data to the electronic display... to show the calculated distance value and the calculated bearing value.
- Independent Claim 13 (System):
- an electronic display; and
- an electronic processor configured to perform steps nearly identical to those recited in Claim 1.
- The complaint does not explicitly reserve the right to assert dependent claims, but states it reserves the right to modify its infringement theories as discovery progresses (Compl. ¶33).
III. The Accused Instrumentality
Product Identification
- The "iEFIS Explorer," "iEFIS Discovery," and "iEFIS Challenger" multi-function displays (collectively, the "Accused Product") (Compl. ¶17 & fn. 1).
Functionality and Market Context
- The complaint describes the Accused Product as a "self-contained, fault-tolerant, multi-function display" for aircraft (Compl. ¶17). Its alleged functionality includes providing displays and processors to assist pilots in navigation by determining the aircraft's real-time situation using terrain maps, calculating the distance and bearing to a designated waypoint or destination, and showing this information on the display (Compl. ¶¶18-21).
IV. Analysis of Infringement Allegations
'396 Patent Infringement Allegations (Claim 1)
| Claim Element (from Independent Claim 1) | Alleged Infringing Functionality | Complaint Citation | Patent Citation |
|---|---|---|---|
| determining a location of interest relative to an aircraft using a terrain awareness and warning system; | The Accused Product "determines the real time situation of the aircraft using terrain maps" | ¶18 | col. 23:53-55 |
| calculating a distance value and a bearing value for the location of interest relative to the aircraft; | The Accused Product "calculates the distance and the bearing angle to a designated waypoint or destination" | ¶19 | col. 23:56-57 |
| providing first display data to an electronic display, the first display data configured to cause the electronic display to show an aircraft situation display image... | The Accused Product provides a "first display data that shows aircraft situation display image with respect to a waypoint" | ¶20 | col. 23:58-62 |
| providing second display data to the electronic display, the second display data configured to cause the electronic display to show the calculated distance value... | The Accused Product provides a "second display [that] shows the distance and bearing angle to the destination" | ¶21 | col. 24:1-4 |
'396 Patent Infringement Allegations (Claim 13)
The complaint alleges that the Accused Product enables a system that performs all the steps of Claim 13, incorporating by reference the functionalities alleged for Claim 1 (Compl. ¶¶22-23).
| Claim Element (from Independent Claim 13) | Alleged Infringing Functionality | Complaint Citation | Patent Citation |
|---|---|---|---|
| an electronic display; and an electronic processor configured to: determine a location of interest relative to an aircraft using a terrain awareness and warning system; | The Accused Product includes displays/processors that "determine... the real time situation of the aircraft using terrain maps" | ¶¶18, 22 | col. 24:49-54 |
| calculate a distance value and a bearing value for the location of interest relative to the aircraft; | The processor "calculates the distance and the bearing angle to a designated waypoint or destination" | ¶¶19, 22 | col. 24:55-56 |
| provide first display data to an electronic display... to show an aircraft situation display image... | The processor provides "first display data that shows aircraft situation display image with respect to a waypoint" | ¶¶20, 22 | col. 24:57-60 |
| and provide second display data to the electronic display... to show the calculated distance value and the calculated bearing value. | The processor provides a "second display [that] shows the distance and bearing angle to the destination" | ¶¶21, 22 | col. 24:60-62 |
Identified Points of Contention
- Scope Questions: A central question may be whether the term "terrain awareness and warning system," as used in the patent, reads on the Accused Product's alleged use of "terrain maps" (Compl. ¶18). The defense could argue that "terrain awareness and warning system" implies a specific type of certified equipment (like a formal TAWS), whereas the complaint appears to allege a more general-purpose navigation mapping function.
- Technical Questions: The claims require both "first display data" for a graphical image and "second display data" for the calculated values. A question for the court will be whether the Accused Product provides these as distinct data sets as claimed, or if the textual information is merely an integrated/overlaid part of a single graphical display data stream. The separation of these elements in the claims suggests a potential distinction that may be a focus of litigation.
No probative visual evidence provided in complaint.
V. Key Claim Terms for Construction
The Term: "terrain awareness and warning system"
- Context and Importance: This term appears in both independent claims and is foundational to the invention. Its construction will determine whether the Accused Product's general-purpose mapping and navigation features fall within the scope of the claims. Practitioners may focus on this term because its definition could either broadly cover many modern avionics systems or be limited to a narrow, specific class of FAA-certified safety equipment.
- Intrinsic Evidence for Interpretation:
- Evidence for a Broader Interpretation: Dependent claim 6 defines the system as "capable of determining one or more locations of interest... via retrieval of terrain information from the geographical database," suggesting any system using a GPS and a terrain database could qualify (’396 Patent, col. 24:14-19).
- Evidence for a Narrower Interpretation: The patent title, "TERRAIN AWARENESS AND WARNING AIRCRAFT INDICATOR EQUIPMENT," and the abstract's focus on maintaining a "safe distance" from mountains and buildings could be argued to limit the term to systems with specific, active warning capabilities, not just passive display functions (’396 Patent, Title; Abstract).
The Term: "aircraft situation display image"
- Context and Importance: This term defines the graphical output required by the claims. The dispute may turn on whether the Accused Product's map display constitutes the specific "image" contemplated by the patent.
- Intrinsic Evidence for Interpretation:
- Evidence for a Broader Interpretation: The patent does not provide a specific definition, which may support giving the term its plain and ordinary meaning, potentially covering any graphical map showing an aircraft's position relative to a point of interest.
- Evidence for a Narrower Interpretation: The patent repeatedly contextualizes the invention in the setting of an "instrument approach" (e.g., Claim 7) (’396 Patent, col. 24:20-21). A defendant might argue this implies the "image" must conform to specific standards or formats used for certified instrument flight, rather than being a generic moving map.
VI. Other Allegations
Indirect Infringement
- The complaint makes a conclusory allegation of induced infringement, stating Defendant encouraged infringement that resulted in direct infringement, but it does not plead specific underlying facts, such as references to user manuals or marketing materials that instruct users to perform the infringing acts (Compl. ¶28).
Willful Infringement
- The complaint alleges Defendant had knowledge of its infringement "at least as of the service of the present Complaint" (Compl. ¶26). This allegation supports a claim for post-filing willfulness but does not assert pre-suit knowledge of the patent or infringement.
VII. Analyst’s Conclusion: Key Questions for the Case
The resolution of this dispute will likely depend on the court's determination of two key issues:
- A core issue will be one of definitional scope: can the claim term "terrain awareness and warning system," which has a specific meaning in aviation regulation, be construed broadly enough to read on the general-purpose "terrain maps" and navigation functions allegedly present in the accused iEFIS products?
- A key evidentiary question will be one of claim element separation: does the Accused Product’s display function generate distinct "first display data" for a graphical image and "second display data" for numerical values, as separately required by the claim language, or does it generate a single, integrated data stream for one composite display?
Analysis metadata