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SAE ARP1270B

Current

Current

The latest, up-to-date edition.

Aircraft Cabin Pressurization Criteria

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

10-01-2015

US$175.82
Excluding Tax where applicable

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.

DevelopmentNote
Supersedes SAE AS 5379. (05/2011)
DocumentType
Standard
Pages
53
PublisherName
SAE International
Status
Current
Supersedes

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

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 ARP85F 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 ARP85F:2019 Air Conditioning Systems for Subsonic Airplanes<br>

SAE ARP488E 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 AIR822C 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 AIR1168/7A 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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