SAE ARP 1270 : 2015
Current
The latest, up-to-date edition.
AIRCRAFT CABIN PRESSURIZATION CRITERIA
Hardcopy , PDF
English
01-10-2015
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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 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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