ACMS Report Filtering for Spurious Aircraft Maintenance Alerts

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Solution Overview

Problem

Existing aircraft maintenance and inspection scheduling is inefficient and costly due to the generation of unnecessary reports from aircraft condition monitoring systems, leading to unwarranted maintenance actions.

Innovation Solution

Implementing a flight data collection system with an aircraft condition monitoring system that includes a report filter device to identify and filter spurious data, ensuring only valid reports are transmitted for maintenance decisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the ACMS generates and transmits all flight data reports for maintenance monitoring, then the reliability of maintenance scheduling is improved, but the quantity of unnecessary maintenance actions increases due to spurious data

Engineering Contradiction:
Improvemaintenance scheduling reliabilityVSAvoidunnecessary maintenance actions
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent applies preliminary action by implementing a filter device that preprocesses flight data reports before they reach the maintenance scheduling system. The filter device identifies and removes spurious data patterns (such as impossible sensor readings, duplicate reports, and erroneous trouble codes) in advance, ensuring that only valid data triggers maintenance actions. This preliminary filtering prevents the generation of unnecessary maintenance schedules while maintaining reliable monitoring of actual aircraft conditions.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If maintenance inspections are scheduled based on all ACMS reports, then the completeness of monitoring is improved, but the loss of time and resources increases due to unwarranted maintenance operations

Engineering Contradiction:
Improvemonitoring completenessVSAvoidmaintenance time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent applies the extraction principle by separating valid flight data from spurious data through a dedicated filter device. The filter extracts only meaningful maintenance-relevant information from the total ACMS report stream by identifying and excluding erroneous patterns such as impossible parameter values, duplicate fault reports, and sensor malfunctions. This extraction ensures complete monitoring of actual aircraft issues while eliminating time-wasting false alarms that would otherwise require unnecessary maintenance interventions.

Inventive Principle:
Principle #2Taking out (Extraction)

3Productivity

If the ACMS processes all flight data items in real-time, then the productivity of data collection is improved, but the device complexity increases due to the need for sophisticated filtering mechanisms

Engineering Contradiction:
Improvedata collection efficiencyVSAvoidfiltering system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent applies segmentation by dividing the filtering function into distinct modular components within the filter device. Each module handles specific types of spurious data identification (sensor validation, duplicate detection, error pattern recognition, etc.). This segmented approach maintains high data collection productivity by processing all flight data items in real-time while managing system complexity through organized, specialized filtering modules rather than a single complex filtering system.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP4653323A1Flight data collection system and method for filtering aircraft condition monitoring system reports
Publication Date: 2025.11.26 AIRBUS OPERATIONS GMBH
  • EP4653323A1 patent drawingFigure 1~2
  • EP4653323A1 patent drawingFigure 3~4
  • EP4653323A1 patent drawing

AI summary

A flight data collection system, FDCS, (10) for an aircraft (A) includes a flight data acquisition unit, FDAU, (12) configured to collect flight data (FD) from aircraft and avionics components (11) on-board of the aircraft (A) and to tabulate the collected flight data (FD) as real-time flight reports (FR), and an aircraft communication and reporting system, ACARS, management system (15) coupled to the FDAU (12) and configured to transmit the real-time flight reports (FR) generated by the FDAU (12) as either air-to-ground or ground-to-ground communication (GR) to ground-based systems (20). The FDAU (12) comprises an aircraft condition monitoring system, ACMS, (13) configured to monitor and process flight data (FD) from the aircraft and avionics components (11). The ACMS (13) comprises a report filter device (14) configured to identify spurious data in the recorded flight data of the ACMS (13) and to filter the real-time flight reports (FR) output to the ACARS management system (15) based on the identified spurious data.