ARP217A Testing of Airplane Installed Environmental Control Systems (Ecs)
03/01/1960
- Issuing Committee
- Content
- 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.
- Pages
- 11
- Citation
- SAE International Recommended Practice, Testing of Airplane Installed Environmental Control Systems (Ecs), SAE Standard ARP217A, Revised March 1960, Issued March 1951, https://doi.org/10.4271/ARP217A.