SAE AIR 5661A : 2017

Superseded

View Superseded by

COMPARTMENT DECOMPRESSION ANALYSIS

Available format(s)

Hardcopy , PDF

Superseded date

05-01-2022

Language(s)

English

Published date

05-01-2017

Publisher

SAE International

1. SCOPE
2. REFERENCES
3. REQUIREMENTS FOR COMPARTMENT
DECOMPRESSION ANALYSES
4. DESIGN MEASURES
5. ESSENTIAL EQUATIONS
6. TYPICAL ANALYSIS SCENARIOS
7. FLIGHT TESTING
8. GROUND TESTING
9. NOTES

This SAE Aerospace Information Report (AIR) provides data and general analysis methods for calculation of internal and external, pressurized and unpressurized airplane compartment pressures during rapid discharge of cabin pressure.

Committee	AC-9
DocumentType	Revision
Pages	60
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AIR5661A:2017(R2021)
Supersedes	SAE AIR 5661 : 2010

SAE AIR 1168/1 : 1990	THERMODYNAMICS OF INCOMPRESSIBLE AND COMPRESSIBLE FLUID FLOW
SAE AIR 825/1 : 2016	INTRODUCTION TO OXYGEN EQUIPMENT FOR AIRCRAFT
FAA AC 25-22 : 0	CERTIFICATION OF TRANSPORT AIRPLANE MECHANICAL SYSTEMS
SAE ARP 1270 : 2015	AIRCRAFT CABIN PRESSURIZATION CRITERIA
SAE AIR 1168/5 : 2011	Aerothermodynamic Test Instrumentation and Measurement
FAA AC 25-20 : 0	PRESSURIZATION, VENTILATION AND OXYGEN SYSTEMS ASSESSMENT FOR SUBSONIC FLIGHT INCLUDING HIGH ALTITUDE OPERATION
NASA STD 3000 VOL 3 : 1994	MAN-SYSTEM INTEGRATION STANDARDS - VOLUME 3
NASA STD 3000 VOL 2 : 1995	MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2
SAE AIR 1168/6 : 2011	Aircraft Fuel Weight Penalty Due to Air Conditioning(STABILIZED Jul 2011)
SAE AIR 1168/7 : 2011	AEROSPACE PRESSURIZATION SYSTEM DESIGN
NASA STD 3000 VOL 1 : 1995	MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 1
FAA AC 20-128 : 0	DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE