{"schema_version":1,"research_id":"eoa_inverse_innovation_exp06_external_evaluation_20260803","source_assessment_id":"catalytic_pathway_enablement__aviation_aeronautics:P1:v0","cell_id":"catalytic_pathway_enablement__aviation_aeronautics","search_queries":["site:faa.gov avionics software configuration management aircraft maintenance records part number software load","aircraft configuration management avionics replacement compatibility software part number maintenance records challenge","aviation MRO software automated configuration control component compatibility aircraft first party","FAA maintenance recordkeeping configuration conformity return to service avionics replacement","site:swiss-as.com AMOS aircraft configuration management component installation compatibility software load","site:docs.ifs.com aviation maintenance configuration rules incompatible part number aircraft","site:rusada.com ENVISION configuration management aircraft component compatibility automated compliance","site:icao.int aviation maintenance electronic records configuration management digital aircraft","site:ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43 section 43.7 43.9 return to service","site:faa.gov AC 120-78B electronic signatures records maintenance security integrity","site:easa.europa.eu electronic aircraft maintenance records AMC 20-25 records integrity security","aircraft maintenance digital records data quality fragmented systems report MRO 2024"],"sources":[{"source_id":"S1","title":"AC 43-216A — Software Management During Aircraft Maintenance","publisher":"Federal Aviation Administration","url":"https://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.information/documentID/1042076","source_class":"OFFICIAL_GUIDANCE","publication_date":"2023-08-25","accessed_at":"2026-08-03","claims_supported":["Aircraft software configuration during maintenance is a continuing-airworthiness concern.","FAA recognizes operator software-management programs as an acceptable compliance mechanism.","A bounded configuration-management workflow can be implemented without changing substantive regulatory requirements."]},{"source_id":"S2","title":"AC 120-78B — Electronic Signatures, Electronic Recordkeeping, and Electronic Manuals","publisher":"Federal Aviation Administration","url":"https://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.information/documentID/1043396","source_class":"OFFICIAL_GUIDANCE","publication_date":"2024-12-11","accessed_at":"2026-08-03","claims_supported":["Certificate holders may use compliant electronic recordkeeping systems for aircraft maintenance records, task cards, and airworthiness releases.","Electronic processing is legally feasible but must preserve applicable record and signature controls."]},{"source_id":"S3","title":"Easy Access Rules for Continuing Airworthiness — Regulation (EU) No 1321/2014, September 2025 revision","publisher":"European Union Aviation Safety Agency","url":"https://www.easa.europa.eu/en/document-library/easy-access-rules/online-publications/easy-access-rules-continuing-airworthiness?erules-id=ERULES-1963177438-1031","source_class":"GOVERNMENT_OR_REGULATOR","publication_date":"2025-09-10","accessed_at":"2026-08-03","claims_supported":["Continuing-airworthiness records must make aircraft and component status readily establishable.","Integrity, continuity, and traceability from operator or CAMO records to maintenance documentation, approved data, and release documents are inspection concerns.","Aircraft release-to-service records must be signed by authorized persons.","Physical and recorded part locations may need comparison to detect undocumented swaps."]},{"source_id":"S4","title":"Ensuring a Correct Aircraft Technical Configuration","publisher":"Airbus Safety First","url":"https://safetyfirst.airbus.com/ensuring-a-correct-aircraft-technical-configuration/?airbus-iframe=true&airbus-post=2089","source_class":"COMMERCIAL_FIRST_PARTY","publication_date":"2025-11","accessed_at":"2026-08-03","claims_supported":["Hardware part number alone may be insufficient because replacement LRUs can contain incompatible software loads.","Airbus reports incorrect technical configurations caused by failure to check installed software part numbers.","Operators should maintain dedicated software-configuration processes and roles.","Airbus Configuration Cockpit already compares as-maintained, as-flying, and as-reported configurations against allowed-parts data, identifies mismatches, and routes indeterminate cases to manual operator analysis.","Correct configuration management and consistent documentation are safety-relevant and operational pressure must not cause required checks to be skipped."]},{"source_id":"S5","title":"Electronic Aircraft Maintenance Records and Continuing Airworthiness Records","publisher":"International Civil Aviation Organization","url":"https://www.icao.int/operational-safety/normal-airworthiness","source_class":"OFFICIAL_GUIDANCE","publication_date":"2020","accessed_at":"2026-08-03","claims_supported":["Operators, manufacturers, and maintenance organizations are migrating toward electronic aircraft maintenance records.","Electronic-record implementation has recognized signature, security, integrity, and cross-system transferability challenges.","ICAO provisions and guidance accommodate electronic maintenance and continuing-airworthiness records."]},{"source_id":"S6","title":"Configuration Rules for Part Groups","publisher":"IFS","url":"https://docs.ifs.com/maintenix/24r1/Operator/enduser/Engineering_TechRecords/part_numbers_and_groups/c_configuration_rules_part_groups.html","source_class":"OFFICIAL_PRODUCT_DOCUMENTATION","publication_date":"2024-06-27","accessed_at":"2026-08-03","claims_supported":["Commercial aviation-maintenance software already models tail-specific part applicability, interchangeability, and incompatibility.","Existing rules can prohibit installation of an avionics unit when an incompatible sensor is installed.","Rules can condition part installation on whether specified tasks have been completed."]},{"source_id":"S7","title":"Add Part Requirement — IFS Cloud Aviation Maintenance 26R1","publisher":"IFS","url":"https://docs.ifs.com/ifsclouddocs/26r1/lang/en/ForwardOrLineMaintMobility/ActivityAddPartRequirement.htm","source_class":"OFFICIAL_PRODUCT_DOCUMENTATION","publication_date":"2026","accessed_at":"2026-08-03","claims_supported":["Current MRO workflows already capture aircraft, task, part number, part group, configuration-slot position, interchangeability, and installation/removal records.","Commercial systems can integrate configuration data with maintenance-task execution and preserve part-change records.","Operational integration requires online system access and authoritative workflow data."]},{"source_id":"S8","title":"Aircraft MRO 2.0: The Digital Revolution","publisher":"McKinsey & Company","url":"https://www.mckinsey.com/industries/travel/our-insights/aircraft-mro-2-point-0-the-digital-revolution","source_class":"AUTHORITATIVE_SECONDARY","publication_date":"2024-07-19","accessed_at":"2026-08-03","claims_supported":["Only 6 percent of surveyed MRO organizations reported digital and analytics integration at scale.","More than 80 percent of respondents identified data limitations as the most significant digital-adoption barrier.","Physical recordkeeping can produce fragmented collections that are difficult to digitize.","Successful implementation is associated with technician-centered design, leadership endorsement, and alignment with broader digital priorities."]}],"problem_evidence":{"support":"STRONG","rationale":"The exact safety problem is visible: Airbus documents replacement LRUs with correct hardware identifiers but incompatible software, required interchangeability checks, reported configuration errors, and cases requiring manual analysis. EASA requires traceable records capable of establishing configuration, while ICAO and MRO survey evidence identify fragmented records and transferability limitations. Public evidence establishes configuration-reconciliation burden and safety importance, although it does not quantify post-installation aircraft downtime for the proposed fleet and unit families.","source_ids":["S3","S4","S5","S8"]},"stakeholder_evidence":{"support":"STRONG","rationale":"Identifiable adopters are aircraft operators, certificate holders, CAMOs, and maintenance organizations; authorizers include their continuing-airworthiness, quality, and electronic-record program owners. Airbus explicitly calls for operator processes and dedicated roles and provides Configuration Cockpit to operators. FAA and EASA guidance establishes both the responsible organizations and the controlled electronic-record pathway. No named airline has publicly committed to this exact proposed lane.","source_ids":["S1","S2","S3","S4","S5"]},"prior_art":{"proximity":"ESTABLISHED_PRACTICE","closest_analogues":[{"name":"Airbus Configuration Cockpit","similarity":"Very close functional analogue: it ingests as-maintained and as-flying files, compares them with OEM as-reported configuration and allowed-parts data, identifies wrong part numbers, and sends non-automatable cases to manual operator analysis.","remaining_difference":"The proposal wraps this capability in a post-replacement conformity-packet workflow with explicit queue metering, specialist rotation, regeneration thresholds, a retained signatory, and a prospective shadow assay. The source does not show that Airbus Configuration Cockpit itself produces the proposed return-to-service packet or uses those governance metrics.","source_ids":["S4"]},{"name":"IFS Maintenix/IFS Cloud configuration-management workflow","similarity":"Substantial overlap: commercial software represents tail applicability, part interchangeability and incompatibility, task prerequisites, configuration positions, and installation/removal records inside the maintenance workflow.","remaining_difference":"The opened documentation does not establish software-load compatibility coverage, post-install conformity-packet assembly, specialist exception rotation, or the proposed regeneration and selectivity assay as one packaged lane.","source_ids":["S6","S7"]},{"name":"FAA-compliant electronic maintenance-record program","similarity":"Provides the recognized electronic record, task-card, maintenance-record, and airworthiness-release infrastructure needed for the lane.","remaining_difference":"FAA guidance defines an acceptable controlled medium rather than the candidate's fleet-specific compatibility rules, packet transformation, exception triage, or performance claim.","source_ids":["S1","S2"]}],"distinctive_claim_remaining":"Only a site-specific incremental claim remains: for one operator, fleet type, and two predefined LRU families, the integrated packet-and-exception lane must reduce both median barrier-attributable packet cycle time and qualified-specialist minutes per accepted packet by at least 25% versus the current pathway and versus the simplest configured existing MIS/OEM compatibility function, while producing zero false-ready packets, missed conflicts, scope leaks, or increases in downstream signatory work. This is falsifiable but is not evidence of world novelty.","confidence":"HIGH"},"implementation_evidence":{"support":"STRONG","rationale":"The main technical elements already exist: electronic maintenance records, tail-specific applicability and incompatibility rules, maintenance-task integration, OEM configuration comparison, and manual handling of indeterminate cases. Workflow and authority feasibility are credible if the rules engine remains advisory and the authorized signatory retains release authority. Principal constraints are authoritative-data access, provenance, software-load identifiers, version control, electronic-record controls, cybersecurity, specialist capacity, and validation against known mismatches. These constraints are manageable in read-only shadow mode but require operator-specific approval and testing before operational use.","source_ids":["S1","S2","S3","S4","S5","S6","S7"]},"scores":{"meaningful_impact":{"score":4,"rationale":"Configuration errors are flight-safety relevant and compatible-spare determination can affect grounding. Reducing repeated review could improve availability and engineering productivity, but candidate-specific downtime prevalence is unmeasured.","source_ids":["S3","S4","S8"]},"stakeholder_pull":{"score":4,"rationale":"Regulators assign record and configuration responsibilities, Airbus urges dedicated operator processes and supplies a configuration checker, and MRO respondents report strong data limitations. No named operator has requested this exact packet lane.","source_ids":["S1","S3","S4","S8"]},"incremental_advantage":{"score":2,"rationale":"Airbus and IFS already implement most core functions. Possible advantage is the governed post-install packet, specialist-exception, and regeneration wrapper, which has no demonstrated advantage over configuring established tools.","source_ids":["S4","S6","S7"]},"distinctiveness_plausibility":{"score":1,"rationale":"The reusable compatibility dataset, automated rules, mismatch detection, manual exception handling, and configuration workflow are established practice. Remaining differentiation is implementation packaging and local performance.","source_ids":["S4","S6","S7"]},"technical_implementability":{"score":4,"rationale":"Required data models and workflow functions are commercially demonstrated. Integration and data-quality work may be substantial, especially for software loads and legacy records, but no fundamental technical barrier is visible.","source_ids":["S2","S4","S5","S6","S7","S8"]},"adoption_authority_feasibility":{"score":4,"rationale":"Operators, certificate holders, CAMOs, and quality owners are identifiable implementers. Shadow mode can preserve the existing authorized release decision, though operational adoption requires approved procedures, access controls, and record-system governance.","source_ids":["S1","S2","S3","S4"]},"evidence_readiness":{"score":3,"rationale":"Public sources establish the problem class, controls, and prior art, but not the operator-specific queue decomposition, error rate, specialist burden, benefit, or cost. Those require proprietary records and field testing.","source_ids":["S3","S4","S8"]},"safety_net_benefit":{"score":4,"rationale":"A read-only second check with fail-closed routing can detect hardware/software configuration mismatch without authorizing flight. Benefit depends on independent data and must not create automation complacency or replace prescribed identification steps.","source_ids":["S2","S3","S4","S5"]},"scalability":{"score":3,"rationale":"Rules and templates are reusable, but each fleet, modification state, OEM data interface, and operator approval environment needs validation. Legacy-data limitations and manual exception load can constrain scale.","source_ids":["S4","S5","S6","S8"]}},"score_confidence":"MODERATE","costs":{"first_evidence":{"band_2026_usd":"50K_TO_250K","scope":"Design and execute a read-only, 20-case, three-comparator shadow study; freeze rules and data; obtain independent qualified review; analyze case-level time, labor, discrepancies, and downstream work.","confidence":"LOW","assumptions":["One fleet type and two LRU families","Existing records are exportable without new production interfaces","Approximately 8–16 weeks of part-time avionics, records, quality, data-engineering, security, and evaluation effort","No certification credit or operational release is sought"],"source_ids":[]},"initial_deployment_startup":{"band_2026_usd":"250K_TO_1M","scope":"Configure or prototype the intake contract, compatibility dataset, rules, packet template, audit logging, dashboards, access controls, and one-fleet integrations after a successful shadow result.","confidence":"LOW","assumptions":["Existing MRO/MIS and identity infrastructure can be extended","No aircraft-side hardware change","Commercial configuration functions are licensed or already available","Includes validation and operator procedure updates but not fleet-wide rollout"],"source_ids":["S2","S4","S6","S7"]},"operational_launch":{"band_2026_usd":"1M_TO_5M","scope":"Production-grade deployment for one operator and fleet type, including authoritative integrations, cybersecurity review, data reconciliation, validation corpus, training, controlled procedures, monitoring, redundancy, and launch support.","confidence":"LOW","assumptions":["Multiple legacy interfaces require production integration","Operator governance and quality approval are required","Qualified specialist coverage and independent audit are funded","Does not include replacing the operator's core MRO platform"],"source_ids":["S2","S5","S8"]},"annual_recurring":{"band_2026_usd":"250K_TO_1M","scope":"Dataset and rule maintenance, source reconciliation, specialist exception coverage, audits, cybersecurity and platform operations, training, incident response, and periodic revalidation for the bounded fleet.","confidence":"LOW","assumptions":["Two to four partial or full-time resource equivalents plus platform costs","Exception volume remains bounded","Major fleet or avionics-family expansion is excluded","Existing MRO licenses remain separately funded"],"source_ids":["S4","S6","S7"]}},"verified_pipeline_gates":{"externally_supported_problem":{"status":"YES","reason":"OEM, regulator, standards-body, and industry evidence independently establish configuration mismatch risk, traceability requirements, fragmented records, and manual-analysis cases.","source_ids":["S3","S4","S5","S8"]},"externally_credible_adopter_or_authorizer":{"status":"YES","reason":"Aircraft operators, certificate holders, CAMOs, maintenance organizations, quality owners, and authorized release personnel are explicit responsible parties; Airbus already offers a related operator tool.","source_ids":["S1","S2","S3","S4"]},"distinct_testable_incremental_claim":{"status":"YES","reason":"A paired field test can compare cycle time, specialist minutes, downstream work, and the full error distribution against both the current path and configured established tools. The claim is locally incremental, not novel.","source_ids":["S4","S6","S7"]},"bounded_next_evidence_step":{"status":"YES","reason":"A capped 20-case, read-only shadow study with frozen scope, paired comparators, independent review, and immediate stop conditions is bounded and reversible.","source_ids":["S2","S3","S4"]},"no_unresolved_safety_or_authority_stop":{"status":"YES","reason":"Shadow processing can be read-only and non-authoritative; the existing pathway and authorized signatory remain controlling. Any mismatch, unauthorized access, or scope leakage stops the study. Operational authority remains unverified and is outside the first step.","source_ids":["S1","S2","S3","S4","S5"]},"credible_cost_scope_and_range":{"status":"UNCERTAIN","reason":"Scopes and resource-equivalent bands are bounded, but no direct pricing, operator architecture, licensing, interface count, labor rate, or exception-volume evidence was publicly available among the eight sources.","source_ids":["S4","S6","S7","S8"]}},"next_evidence_step":"With an operator's continuing-airworthiness, quality, cybersecurity, and records approvals, prospectively process no more than 20 already scheduled replacements from one fleet type and two LRU families in read-only shadow mode. Before access, freeze eligibility, source snapshot, rule version, the 25% time-and-specialist-effort thresholds, and zero-tolerance safety falsifiers. For the same cases compare: (A) the authoritative current workflow; (B) the simplest available configured MIS/OEM compatibility-check function without the proposed specialist-and-packet wrapper; and (C) the proposed lane. An independent qualified reviewer must adjudicate every packet and all reroutes. Falsify the intervention if it misses the 25% thresholds, shifts work to signatories or engineering, fails repeated ready-state restoration, or produces any false-ready packet, missed conflict, untraceable evidence, unauthorized access, scope expansion, or weakened required check.","blocking_evidence":["No public case-level estimate of post-install packet delay, repeat handoffs, specialist minutes, rework, or aircraft downtime for the proposed fleet and LRU families.","No named operator commitment, data-access authorization, or approved shadow-study sponsor.","No head-to-head evidence against Airbus Configuration Cockpit or configured IFS/MRO functionality.","No validated compatibility dataset, software-load identifier mapping, known-mismatch test corpus, or measured source-record error rate.","No operator-specific legal, cybersecurity, labor, procedure-change, and electronic-record approval assessment.","No direct vendor pricing, integration estimate, exception volume, or recurring-maintenance estimate.","No live evidence that the facilitator restores to a verified ready state across repeated cases without downstream workload transfer."],"research_disposition":"KNOWN_PRACTICE_DIFFUSION","world_novelty_boundary":"The search establishes only that closely matching configuration comparison, incompatibility rules, maintenance-workflow integration, and manual exception analysis are established practices. It does not measure world novelty, patentability, freedom to operate, market size, or realized impact. The only unevaluated boundary is whether the proposed post-install packet, governance, and regeneration bundle yields superior local operational performance over properly configured existing products.","arm":"COMPLETE_PROPOSAL_PORTFOLIO","candidate_version":0,"controller_recommendation":{"action":"STOP_EMPIRICAL_RESEARCH_NEEDED","repairable":false,"material_progress_observed":true,"progress_targets":["Secure a named operator/CAMO or quality sponsor and written authority for read-only use of the required maintenance and configuration records.","Complete a documented fit-gap comparison against Airbus Configuration Cockpit and the operator's existing IFS/MRO/MIS capabilities before building new software.","Pre-register the 20-case protocol, paired comparators, 25% performance thresholds, zero-tolerance safety falsifiers, and downstream-work measures.","Validate provenance, software-load mappings, rule versions, access controls, and a known-mismatch test corpus before processing real cases.","Obtain operator-specific resource estimates or vendor quotes for prototype integration, production launch, and annual rule/data stewardship.","Execute the independent shadow study and report every case, reroute, discrepancy, false-ready outcome, specialist minute, and regeneration action without extrapolation."],"reason":"Bounded web research resolves the problem class, adopter, authority pathway, implementation feasibility, and closest prior art. It also shows substantial collision with established Airbus and IFS practices. Whether the proposed wrapper provides any incremental operator benefit now depends on proprietary case records, a live configured comparator, and prospective shadow testing; those questions cannot be repaired by further public web search."},"proposal_index":1}