This AIR does not provide detailed background or rationale for the technical contents of AS36100A, which are separately provided in AIR36108, AS36100A background and development record.
AS36100A exclusively defines the general geometric parameters (insofar as they affect restraint on board aircraft), minimum performance requirements and testing parameters of unit load devices. Additional areas as per AS36100A paragraph 1.1, such as continued airworthiness and maintenance requirements, design and testing methods, unit load devices design specifications and accessories, and rules for proper operation/utilization and operating staff training also need to be considered for designing unit load devices, and are covered by other documents, listed in AIR36105A.






