AIRCRAFT CABIN PRESSURIZATION CRITERIA

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-10-2015

Publisher

SAE International

1. SCOPE
2. REFERENCES
3. SYSTEM DESIGN PHILOSOPHY
4. SYSTEM DESIGN REQUIREMENTS
5. EQUIPMENT DESIGN REQUIREMENTS
6. SYSTEM DYNAMIC ANALYSIS AND TEST
7. PHYSIOLOGICAL EFFECTS OF CABIN PRESSURE
8. NOTES

Specifies the basic criteria for the design of cabin pressure control systems (CPCS) for general aviation, commercial and military pressurized aircraft.

Committee	AC-9
DevelopmentNote	Supersedes SAE AS 5379. (05/2011)
DocumentType	Standard
Pages	53
PublisherName	SAE International
Status	Current
Supersedes	SAE ARP 1270 : 2010 SAE AS 5379 : 1999

SAE ARP 217 D : 2016	TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
SAE AIR 4766 : 2012	AIR QUALITY FOR COMMERCIAL AIRCRAFT CABINS
SAE AIR 5661A : 2017	COMPARTMENT DECOMPRESSION ANALYSIS
SAE AIR 806 : 2015	AIR CONDITIONING OF AIRCRAFT CARGO
SAE ARP 85 : 2012	AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
SAE ARP 986 : 2015	GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
09/30203113 DC : 0	BS EN 4666 - AEROSPACE SERIES - AIRCRAFT INTEGRATED AIR QUALITY AND PRESSURE STANDARDS, CRITERIA AND DETERMINATION METHODS
13/30280751 DC : 0	BS EN 4666 - AEROSPACE SERIES - AIRCRAFT INTEGRATED AIR QUALITY AND PRESSURE STANDARDS, CRITERIA AND DETERMINATION METHODS
JSSG-2009 Revision A:2013	Air Vehicle Subsystems
SAE AIR 4766/1 : 2011	AIR QUALITY FOR COMMERCIAL AIRCRAFT CABIN - PARTICULATE CONTAMINANTS
TR 4666 : 2016	AEROSPACE SERIES - AIRCRAFT INTEGRATED AIR QUALITY AND PRESSURE STANDARDS, CRITERIA AND DETERMINATION METHODS

SAE ARP 488 : 2010	EXITS AND THEIR OPERATION - AIR TRANSPORT CABIN EMERGENCY
RTCA DO 178 : C2011	SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
MIL-STD-810 Revision G:2008	ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
SAE AIR 825/1 : 2016	INTRODUCTION TO OXYGEN EQUIPMENT FOR AIRCRAFT
FAA AC 25-22 : 0	CERTIFICATION OF TRANSPORT AIRPLANE MECHANICAL SYSTEMS
RTCA DO 254 : 2000	DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
SAE AIR 822 : 2014	OXYGEN SYSTEMS FOR GENERAL AVIATION
IEEE/ASTM SI_10-2010	American National Standard for Metric Practice
MIL-E-18927 Revision E:1983	ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
FAA AC 25-20 : 0	PRESSURIZATION, VENTILATION AND OXYGEN SYSTEMS ASSESSMENT FOR SUBSONIC FLIGHT INCLUDING HIGH ALTITUDE OPERATION
JSSG-2009 Revision A:2013	Air Vehicle Subsystems
FAA AC 61-107 : 2013	AIRCRAFT OPERATIONS AT ALTITUDES ABOVE 25,000 FEET MEAN SEA LEVEL OR MACH NUMBERS GREATER THAN .75
MIL-R-9345 Base Document:1954	REGULATOR AIR PRESSURE, AIRCRAFT CABIN,GENERAL SPECIFICATION FOR
SAE AIR 1168/7 : 2011	AEROSPACE PRESSURIZATION SYSTEM DESIGN
FAA AC 25-17 : 2009	TRANSPORT AIRPLANE CABIN INTERIORS CRASHWORTHINESS HANDBOOK
FAA AC 25.783-1 : 2005	FUSELAGE DOORS AND HATCHES

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SAE ARP 1270 : 2015

AIRCRAFT CABIN PRESSURIZATION CRITERIA

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