SAE ARP1270A-2000
Aircraft Cabin Pressurization Control Criteria

Standard No.
SAE ARP1270A-2000
Release Date
2000
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE ARP1270A-2006
Latest
SAE ARP1270B-2015
Scope
These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: 1. To ensure aircraft safety 2. Physiology and limits which govern maximum permissible pressure time relations as related to aircraft passenger comfort. 3. General pressurization control system performance requirements design to satisfy (2). 4. Technical considerations relevant to satisfying (3). The purpose of the recommended practice is to provide the aerospace industry with guidelines as to the pertinent technology relating to the physiological consideration, the technical system requirements and design objectives for aircraft pressurization control systems. This recommended practice is applicable to pressurized aircraft regardless of the number of passengers or crew. The pressurization control system must provide maximum safety and passenger and crew comfort as a result of changes in cabin pressure altitude during the entire aircraft flight and during ground operation.

SAE ARP1270A-2000 history




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