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  • MIL-E-18927 Revision E:1983

    Current The latest, up-to-date edition.

    ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR

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    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Outlines design and performance requirements for Environmental Control Systems required for occupied spaces and equipment on aircraft.

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

    Committee FSC 1660
    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    MIL-T-5842 Revision B:1985 TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION
    SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    SAE ARP 292 : 2014 ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS
    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
    DEFSTAN 00-970(PT1)SEC4/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    SAE ARP 987 : 2015 THE CONTROL OF EXCESS HUMIDITY IN AVIONICS COOLING
    MIL-D-23222 Revision A:1971 DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
    SAE AIR 1277 : 2005 COOLING OF MILITARY AVIONIC EQUIPMENT
    SAE ARP 217 D : 2016 TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
    MIL-W-81752 Revision A:1987 WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    SAE ARP 89 : 2012 AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM
    SAE ARP 1270 : 2015 AIRCRAFT CABIN PRESSURIZATION CRITERIA

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

    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL O 27210 : F OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL STD 800 : NOTICE 1 PROCEDURE FOR CARBON MONOXIDE DETECTION AND CONTROL IN AIRCRAFT
    MIL-B-81365 Base Document:1966 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
    AN929 Revision 14:2017 CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL-STD-2072 Base Document:1977 SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
    MS16051 Revision G:2014 COUPLING, GROUND COOLING, COMBAT TYPE AIRCRAFT
    MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-STD-882 Revision E:2012 System Safety
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS33740 Revision C:1999 NIPPLE, PNEUMATIC STARTING, 3 INCH ID
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL-B-81592 Revision A:1968 BLEED AIR SYSTEM, LOAD ANALYSIS OF, METHOD FOR
    MIL-D-8804 Revision B:1993 DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR
    MS33565 Revision C:1977 CONNECTION, GROUND LEAKAGE TEST, PRESSURIZED CABIN, AIRCRAFT (ASG)
    MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
    MIL-I-8673 Base Document:1955 INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
    MIL-T-18606 Base Document:1955 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
    MIL-R-9345 Base Document:1954 REGULATOR AIR PRESSURE, AIRCRAFT CABIN,GENERAL SPECIFICATION FOR
    MIL C 83488 : C COATING, ALUMINUM, ION VAPOR DEPOSITED
    MIL-I-8670 Revision B:1993 INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
    MIL-STD-1247 Revision D:2009 MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL-T-23103 Revision A:1971 THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR
    MIL-STD-785 Revision B:1980 RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
    MIL-HDBK-221 Base Document:1965 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
    MS16052 Revision B:1985 AIR INLET, COMBAT AIRCRAFT, GROUND COOLING
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