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SAE ARP 217 D : 2016

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
Available format(s)

Hardcopy , PDF

Superseded date

31-12-2022

Language(s)

English

Published date

26-10-2016

Publisher

SAE International

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Superseded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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Hardcopy - English
PDF - English
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