SAE ARP 217 D : 2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
Hardcopy , PDF
31-12-2022
English
26-10-2016
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1. SCOPE
2. REFERENCES
3. ENVIRONMENTAL CONTROL SYSTEMS
4. TESTS ON INSTALLED SYSTEMS
5. TEST REPORTS
Covers ground and flight test of airplane installed Environmental Control Systems (ECS). Supplies an environment controlled within specific operational limits of comfort and safety, for humans, animals and equipment. Includes pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration and environment composition (ozone, contaminants, etc.)
| Committee |
AC-9
|
| DocumentType |
Standard
|
| Pages |
30
|
| ProductNote |
THIS STANDARD IS NOW STABILIZED
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AIR 1957 : 2015 | HEAT SINKS FOR AIRBORNE VEHICLES |
| SAE AIR 1277 : 2005 | COOLING OF MILITARY AVIONIC EQUIPMENT |
| ASHRAE HDBK REFRIGERATION : 2014 | ASHRAE HANDBOOK - REFRIGERATION |
| SAE ARP 699 : 2015 | HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT |
| SAE AIR 1826 : 2016 | ACOUSTICAL CONSIDERATIONS FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM DESIGN |
| SAE ARP 85 : 2012 | AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES |
| SAE AIR 806 : 2015 | AIR CONDITIONING OF AIRCRAFT CARGO |
| SAE ARP 1270 : 2015 | AIRCRAFT CABIN PRESSURIZATION CRITERIA |
| SAE ARP 1323 : 2012 | TYPE MEASUREMENTS OF AIRCRAFT INTERIOR SOUND PRESSURE LEVELS DURING CRUISE |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| SAE AIR 1706 : 1997 | THE ADVANCED ENVIRONMENTAL CONTROL SYSTEM (AECS) COMPUTER PROGRAM FOR STEADY STATE ANALYSIS AND PRELIMINARY SYSTEM SIZING |
| SAE ARP 292 : 2014 | ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS |
| SAE AIR 1823 : 1996 | ENGINEERING ANALYSIS SYSTEM (EASY) COMPUTER PROGRAM FOR DYNAMIC ANALYSIS OF AIRCRAFT ECS |
| SAE ARP 731 : 2015 | GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT |
| STANAG 2895 : 1990 | EXTREME CLIMATIC CONDITIONS AND DERIVED CONDITIONS FOR USE IN DEFINING DESIGN/TEST CRITERIA FOR NATO FORCES MATERIAL |
| SAE ARP 1796 : 2015 | ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-T-18606 Base Document:1955 | TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
| SAE ARP 89 : 2012 | AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM |
| SAE ARP 1307 : 2013 | MEASUREMENT OF EXTERIOR NOISE PRODUCED BY AIRCRAFT AUXILIARY POWER UNITS (APUS) AND ASSOCIATED EQUIPMENT DURING GROUND OPERATION |
| SAE AIR 1266 : 1993 | FAULT ISOLATION IN ENVIRONMENTAL CONTROL SYSTEMS OF COMMERCIAL TRANSPORTS |
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