Air Vehicle Systems (Mechanical)
Air vehicle subsystems (mechanical) include: landing, hydraulic power, fuel, aerial refuelling, mechanical, propeller and pneumatic systems, and so on. In Defence aircraft, these subsystems are usually designed to comply with an Authority recognised Airworthiness Code. However, with the increased prevalence of modifying civil-derivative aircraft for military use, there may be occasions where Defence's CRE is different to that which the aircraft was originally certified. Further, the design of some air vehicle subsystems (mechanical) may have an adverse impact on capability and interoperability if Defence's requirements are not considered during design development.
Defence's CRE remains a primary consideration when selecting aircraft for Defence use. Any limitations associated with air vehicle subsystems will be comprehensively disclosed in the aircraft's design data and will inform decisions on whether the aircraft can adequately meet Defence's CRE.
Hydro-mechanical Systems points of contact can be provided by DASA upon request by contacting DASA DTS Enquiries.