Regulations 22

Division VI - Advanced Operation - Requirements for Manufacturers Manufacturer Deceleration - 901.76 For each model of remotely piloted aircraft system that is intended to conduct any of the operations referred to in subsection 901.69(1), the manufacturer shall provide the Minister with a declaration in accordance with subsection (2), except in the case of a model referred to in subsection 901.69(2) and that is intended to conduct any of the operations referred to in that subsection. The manufacturer's declaration shall: a) specify the manufacturer of the remotely piloted aircraft system, the model of the system, the maximum take-off weight of the aircraft, the operations referred to in subsection 901.69(1) that the aircraft is intended to undertake and the category of aircraft, such as a fixed-wing aircraft, rotary-wing aircraft, hybrid aircraft or lighter-than-air aircraft b) indicate that the manufacturer: declares that it meets the documentation requirements set out in section 901.78, and has verified that the system meets the technical requirements set out in Standard 922 - RPAS Assurance applicable to the operations referred to in subsection 901.69(1) for which the declaration was made. The manufacturer's declaration is invalid if: a) the Minister has determined that the model of remotely piloted aircraft system does not meet the technical requirements b) the manufacturer has notified the Minister of an issue related to the design of the model under section 901.77 Documentation - 901.78 A manufacturer that has made a declaration to the Minister in respect of a model of remotely piloted aircraft system under section 901.76 shall make available to each owner of that model of system a maintenance program that includes: instructions related to the servicing and maintenance of the system an inspection program to maintain system readiness any mandatory actions the manufacturer issues in respect of the system; and a RPAS operating manual that includes a description of the system the ranges of weights and centers of gravity within which the system may be safely operated under normal and emergency conditions the minimum and maximum altitudes and velocities within which the aircraft can be operated safely under normal and emergency conditions a description of the effects of foreseeable weather conditions or other environmental conditions on the performance of both the system and the pilot the characteristics of the system that could result in severe injury to crew members during normal operations the design features of the system, and their associated operations, that are intended to protect against injury to persons not involved in the operations the warning information provided to the pilot in the event of a degradation in system performance that results in an unsafe system operation condition procedures for operating the system in normal and emergency conditions assembly and adjustment instructions for the system