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SAE ARP217 Rev D

Testing of Airplane Installed Environmental Control Systems (ECS)
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SAE ARP217 Rev D

Testing of Airplane Installed Environmental Control Systems (ECS)

PUBLISH DATE 1999
PAGES 30
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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.
SDO SAE: SAE International
Document Number ARP217
Publication Date March 1, 1999
Language en - English
Page Count 30
Revision Level D
Supercedes
Committee
Publish Date Document Id Type View
March 1, 1999 ARP217D Revision
Oct. 1, 1997 ARP217C Revision
Oct. 15, 1973 ARP217B Revision
March 1, 1960 ARP217A Revision
March 15, 1951 ARP217 Revision