MIL-E-18927 Revision E:1983
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The latest, up-to-date edition.
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
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Important note : All end users must be registered with an Account prior to user licenses being assigned.Outlines design and performance requirements for Environmental Control Systems required for occupied spaces and equipment on aircraft.
| Committee |
FSC 1660
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| DocumentType |
Standard
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| Pages |
48
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| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| 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 |
| 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 | Connections, Ground Leakage Test, Pressurized Cabin, Aircraft |
| 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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