| Cell chemistry and configuration | Compatibility with the selected cell chemistry, series count, pack voltage, and intended operating profile. | BMS specification, supported cell configuration, and documented operating limits. | Compare the limits with the cell datasheet and the aircraft’s electrical requirements. |
| Size, mass, and integration | Board dimensions, mass, connector layout, mounting, enclosure needs, and thermal conditions. | Dimensioned drawing, mass specification, connector details, and integration guidance. | Check the drawing against available aircraft space and review the design in a representative installation. |
| Protection functions | Documented responses to overvoltage, undervoltage, overcurrent, short circuit, and temperature conditions, as applicable to the design. | Protection thresholds, timing details, recovery behavior, and test records. | Review fault behavior and confirm that protection settings suit the cells and aircraft loads. |
| Cell monitoring and balancing | Cell-voltage monitoring capability, balancing method, balancing conditions, and specified measurement performance. | Monitoring accuracy specification, balancing-current data, and validation procedure. | Check that the stated performance is suitable for the chosen pack and intended maintenance strategy. |
| Current sensing and load capability | Continuous and transient current limits, sensing method, thermal derating, and behavior under representative load changes. | Current ratings, thermal test conditions, derating information, and overload test results. | Compare ratings with measured aircraft load profiles; do not rely on peak-current figures alone. |
| Telemetry and interfaces | Supported communication interfaces, message definitions, update behavior, fault reporting, and compatibility with the flight-control system. | Interface control document, protocol details, sample data, and integration support plan. | Run an integration test using the intended flight controller and software configuration. |
| Environmental and vibration validation | Stated operating and storage conditions, vibration robustness, connector retention, and environmental test coverage. | Test reports identifying the test method, sample configuration, conditions, and results. | Confirm test conditions reflect the aircraft’s actual environment and installation. |
| Safety and transport documentation | Applicability of battery and product safety requirements, plus transport documentation for the complete battery configuration. | Relevant test reports and declarations. For lithium batteries offered for transport, request applicable UN 38.3 test documentation and the test summary. | Verify the documents apply to the supplied cell or battery type; confirm shipping rules with the carrier and destination authority. |
| Quality and traceability | Production controls, revision management, component traceability, inspection, and handling of nonconforming units. | Quality-system certificate if held, sample inspection records, revision-control process, and corrective-action procedure. | Check certificate scope and validity where applicable; review lot-level records and change-notification practices. |
| Customization and engineering support | Ability to support required form factor, firmware settings, interface changes, sample builds, and design verification. | Written development scope, sample schedule, revision plan, and engineering support terms. | Clarify ownership of design files, firmware changes, and validation responsibilities before placing an order. |
| Supply continuity and service | Quoted lead time, production capacity, lifecycle notification, warranty terms, and post-delivery technical support. | Written commercial terms, support process, warranty conditions, and end-of-life notification policy. | Confirm terms for the target market, expected order volumes, and the project’s service-life requirements. |