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SAE ARP 292 : 2014

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS
Available format(s)

Hardcopy , PDF

Superseded date

08-07-2020

Language(s)

English

Published date

01-01-2014

1. SCOPE
2. REFERENCES
3. DESIGN PHILOSOPHY
4. SYSTEM APPROACHES
5. SYSTEM DESIGN REQUIREMENTS
6. EQUIPMENT DESIGN REQUIREMENTS
7. ENVIRONMENT

This ARP discusses design philosophy, system and equipment requirements, environmental conditions, and design considerations for helicopter environmental control systems (ECS).

Committee
AC-9
DocumentType
Standard
Pages
54
PublisherName
SAE International
Status
Superseded
SupersededBy

SAE ARP 731 : 2015 GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT
SAE ARP 217 D : 2016 TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
SAE ARP 89 : 2012 AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM

FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
SAE ARP 699 : 2015 HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT
SAE AIR 1826 : 2016 ACOUSTICAL CONSIDERATIONS FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM DESIGN
AFGS 87145 : A NOTICE 1 ENVIRONMENTAL CONTROL, AIRBORNE
CFR 29(PTS1900-1910) : 0 LABOR - OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR
SAE ARP 4418 : 2008 PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES
ISO 2026:1974 Aircraft Connections for starting engines by air
STANAG 3315 : 1998 AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
STANAG 3372 : 2014 LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING
SAE ARP 85 : 2012 AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
MIL-B-81365 Base Document:1966 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
SAE AIR 4362 : 2014 NBC PROTECTION CONSIDERATIONS FOR ECS DESIGN
SAE AIR 1812 : 2017 ENVIRONMENTAL CONTROL SYSTEMS LIFE CYCLE COST
STANAG 3610 : 2015 CHARACTERISTICS OF CONDITIONED BREATHABLE AIR SUPPLIED TO AIRCRAFT ON THE GROUND
MIL-E-18927 Revision E:1983 ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
SAE AS 8040B : 2013 HEATER, AIRCRAFT INTERNAL COMBUSTION HEAT EXCHANGER TYPE
SAE ARP 86 : 2011 HEATER, AIRPLANE, ENGINE EXHAUST GAS TO AIR HEAT EXCHANGER TYPE
SAE AIR 860 : 2011 AIRCRAFT ELECTRICAL HEATING SYSTEMS
STANAG 3208 : 2009 AIR CONDITIONING CONNECTIONS
SAE AIR 1539 : 2007 ENVIRONMENTAL CONTROL SYSTEM CONTAMINATION
FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
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
MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
SAE ARP 1796 : 2015 ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
SAE ARP 986 : 2015 GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
SAE ARP 89 : 2012 AIRCRAFT COMPARTMENT AUTOMATIC TEMPERATURE CONTROL SYSTEM
FAA AC 20-135 : 0 POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA
SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES

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