Certification Standards
Certification standards applicable to the airworthiness of an aircraft contain many requirements. Some of these requirements can only be met by specifying a maximum weight for the aircraft, and demonstrating that the aircraft can meet the requirement at all weights up to, and including, the specified maximum. These requirements include:
- structural requirements – to ensure the aircraft structure is capable of withstanding all the loads likely to be imposed on it during maneuvering by the pilot, and gusts experienced in turbulent atmospheric conditions.
- performance requirements – to ensure the aircraft is capable of climbing at an adequate gradient with all its engines operating; and also with one engine inoperative.
At the MTOW, all aircraft of a type and model must be capable of complying with all these certification requirements.
Read more about this topic: Maximum Takeoff Weight
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