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SAE ARP 217D:2016-10-26
Testing of Airplane Installed Environmental Control Systems (ECS)More info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2016-10-26 |
| ICS | 49.090 : On-board equipment and instruments |
| Number of pages | 30 |
| Replace | SAE ARP 217C:1997-10-01 |
| Set | AEROPAKS10U-10 |
| Year | 2016 |
| Document history | SAE ARP 217C:1997-10-01 |
| Country | USA |
| Keyword | SAE 217;SAE ARP217D;SAE ARP217D;SAE ARP 217 |