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TESTING OF PROTOTYPE AIRPLANE AIR CONDITIONING SYSTEMS
- Aerospace Standard
- ARP217A
- Revised
Sector:
Issuing Committee:
Language:
English
Scope
These recommendations are written to cover the testing of air conditioning equipment functioning as a complete and installed system in prototype civil aircraft for the purpose of:
-
A
Demonstrating the safety of the installation and equipment.
-
B
Demonstrating performance of the installation and equipment.
-
a
Source of heat
-
b
Source of fresh air and/or ventilation
-
c
The cooling system
-
d
Distribution system including ducting, joints, etc.
-
e
Water separator
-
f
Exhaust system
-
g
Temperature control system.
-
h
Cabin pressurisation system including flow and pressure controls.
-
a
-
C
Obtaining data for future design and to aid in the analysis of in-service performance of the systems and equipment.
Recommended Content
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AC-9 Aircraft Environmental Systems Committee
Furthers the advancement of technology related to the research, design, test and utilization of aircraft environmental and anti-icing/deicing systems. Develops and updates standards, recommended practices, and information reports contributing to the quality, economy, and safety of commercial and military aircraft.
Reference
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