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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

    Available format(s):  Hardcopy, PDF

    Superseded date:  12-31-2022

    Language(s):  English

    Published date:  10-26-2016

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. ENVIRONMENTAL CONTROL SYSTEMS
    4. TESTS ON INSTALLED SYSTEMS
    5. TEST REPORTS

    Abstract - (Show below) - (Hide below)

    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.)

    General Product Information - (Show below) - (Hide below)

    Committee AC-9
    Document Type Standard
    Product Note THIS STANDARD IS NOW STABILIZED
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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 : E 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 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL T 18606 : 0 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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