Service Content
Comprehensive airworthiness certification consulting services;
DO-160G full-set verification testing services and technical capabilities;
Software and hardware testing and verification services based on ARP4754 and ARP4761, compliant with DO-178 and DO-254 relevant standards;
Technical services including strength, fluid dynamics, fluid-structure interaction, process engineering, thermodynamics, and reliability simulation;
Reliability improvement and reliability qualification services (including reliability simulation, reliability enhancement, reliability prediction, reliability growth, reliability qualification, etc.);
Six performance characteristics technical services for airborne equipment;
Simulation, testing, and remediation services related to vibration and noise.
Scope of Services: Research, development, evaluation, and certification services for civil aviation, low-altitude aircraft, and other aircraft and airborne equipment that meet the requirements of (CCAR-21, CCAR-23, CCAR-25, CCCAR-27, CCAR-29, CCAR-92).
Testing Standards: SAE ARP4754, ARP4761, DO-160, DO-178, DO-254, DO-311, GJB899A, MIL STD 2165, GJB 2072-1994, GJB 368B-2022, GB42590, GB/T38058, etc.
Testing Items: Software and hardware testing of airborne equipment according to DO160, DO311, DO178, DO254, etc.; Reliability-related testing of airborne equipment according to GJB899A, including enhanced testing; Software and hardware testing of airborne equipment is conducted according to standards such as SAE ARP4754, ARP4761, DO-178, DO-254, DO-311, GJB899A, MIL STD 2165, GJB 2072-1994, GJB 368B-2022, etc. Full-process certification consulting services;
Relevant Qualifications: CNAS and CMA accreditations for standards such as DO-160, DO-178, DO-254, DO-311, GJB899A, GJB 2072-1994, GJB 368B-2022, GB42590, and GB/T38058.
Testing Cycle: Non-standard testing on demand.
Service Background
Civil aircraft with a maximum takeoff weight greater than 25KG must obtain an airworthiness certificate issued by the Civil Aviation Administration of China (CAAC) for commercial operation. During the certification process, various methods such as analysis, simulation, and testing must be used to demonstrate that the aircraft or onboard equipment complies with the relevant airworthiness regulations.
Similarly, civil aircraft with a maximum takeoff weight less than 25KG must meet the mandatory national standard GB42590 for commercial operation.
Our Advantages
The third-party testing organization with the most comprehensive technical capabilities in the civil aviation field and the most participated in civil aircraft models, possessing rich experience in technical and testing services.
Having participated in the drafting of relevant testing standards in the civil aviation field, their interpretation of these standards possesses a certain degree of authority.
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