Testing of Airplane Installed Environmental Control Systems (ECS)

Standard:
Reaffirmed:
  • 2016-10-26
 
  • CURRENT
Publisher:
  • SAE International
Pages:
77
Scope:

This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment.

Rationale:

ARP217D has been reaffirmed to comply with the SAE five-year review policy.

History:
Standard Published Revision Status
ARP217D 2016-10-26 Latest Reaffirmed
1997-10-01 Historical Revised
1973-10-15 Historical Revised
1960-03-01 Historical Revised
1951-03-15 Historical Issued
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