AirComm Corporation Airbus AS350 Air Conditioner Installation Documents User Manual

							INSTALLATION DOCUMENTS AS350-200D 
 
 
 
 
 
 
 
 
 
AIR COMM CORPORATION 
3300 AIRPORT ROAD 
BOULDER, CO. 80301 
 
 
 
 
 
 
 
 
 
 
 
DOCUMENTS FOR THE INSTALLATION OF THE 
EUROCOPTER MODEL AS350 CABIN AIR CONDITIONING SYSTEM 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
Revision 4        2 April 2015 
  
						

							 
INSTALLATION DOCUMENTS AS350-200D 
 
 
 
RECORD OF REVISION 
 
REVISION 
NUMBER ISSUE 
DATE DATE 
INSERTED  BY Description of Change 
1  01/07/09  01/07/09  GP  Addition of Poly-V belt configuration option. 
2  03/19/10  03/19/10  BD  Updated FMS from rev: 0 to rev: 1, Added Changes 
(Item 5) to Introduction 
3 06/20/14 06/20/14 BD  Updated FMS from rev: 1 to rev: 5.  
4  04/02/15  04/02/15  BD  Added AS350-204 applicability and Updated W&B page 
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
      
 
 
 
 
 
 
 
 
 
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Revision 4         Page i  
						

							 
 
INSTALLATION DOCUMENTS AS350-200D 
 
LIST OF EFFECTIVE PAGES 
 
LIST OF REVISIONS: Revision 0 (Original Issue)…,20 July 2007 
          Revision 1 
(addition of Poly-V belt compressor drive) 7 January 2009 
      
LIST OF EFFECTIVE PAGES 
Title         Page(s) Revision No. 
Record of Revisions       i   4 
List of Effective Pages      ii   1 
Table of Contents       iii   0 
Chapter 0 Introduction      0-1   3 
Chapter 1 General installation procedure &      1-1      0 
Reference Document 
Chapter 2 Weight & Balance Information       2-1      2 
Chapter 3 Flight Manual Supplement    3-1   3 
Chapter 4 Supplemental Type Certificate   4-1   0 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
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INSTALLATION DOCUMENTS AS350-200D 
 
TABLE OF CONTENTS 
 
Identification  Title       Page   
Chapter 0  Introduction       0-1 
   1. Scope       0-1 
   2. Purpose       0-1  
   3. Arrangement      0-1 
   4. Applicability      0-1  
    
Chapter 1    General installation procedure &        1-1 
   Reference Document. 
1. General installation procedure    1-1 
2. Reference Document     1-1 
 
Chapter 2    Weight & Balance Information        2-1 
 
Chapter 3    Flight Manual Supplement     3-1 
   
Chapter 4    Supplemental Type Certificate    4-1 
 
 
 
 
 
 
 
 
 
 
 
 
 
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							INSTALLATION DOCUMENTS AS350-200D 
 
CHAPTER 0 
INTORDUCTION 
 
This document contains information, which is required for the installation and operation 
of the Air Comm Corporation’s air conditioning system installed in the Eurocopter 
EC130B series helicopter. After completion of the installation of the air conditioner 
system the Weight & Balance Information, Flight Manual Supplement, and the 
Supplemental Type Certificate must be removed from this document and placed with 
the appropriate existing aircraft documents. 
 
1. SCOPE 
 
The scope of this document encompasses the general procedures and reference 
documentation necessary to install the Air Comm Corporation air conditioning 
system in the Eurocopter AS350 series helicopter. 
 
2. PURPOSE 
 
The purpose of this document is to provide the aircraft mechanic in the field the 
necessary information and documentation to install the air conditioning system. 
 
3. ARRANGEMENT 
 
This document is arranged by chapters, which are broken down into paragraphs and 
sub-paragraphs. All of the chapters and paragraphs are listed in the front of this 
document in the Table of Contents, and are further identified by their individual page 
number. 
 
4. APPLICABILITY 
 
This document is applicable to Eurocopter Helicopter models AS350 that are 
equipped with the Air Comm Corporation kit number AS350-200, AS350-202 & 
AS350-204 air conditioner system. 
 
5. Changes 
 
 
 
 
 
 
 
 
 
 
Revision 3        Page 0-1 
  
						

							INSTALLATION DOCUMENTS AS350-200D 
 
CHAPTER 1 
GENERAL INSTALLATION PROCEEDURE & REFERANCE DOCUMENT 
 
1.  GENERAL INSTALLATION PROCEEDURE 
 
This section is intended to supplement the information contained on the 
installation drawings. All details and notes contained on the drawings should be 
reviewed carefully. As instructions for installation are provided on the installation 
drawing where appropriate, and are not repeated in this document. 
 
It will be necessary to remove the transmission cowlings, the main cabin 
headliner, Chin bubbles, to facilitate the installation of this kit. 
 
The system components and associated hardware are packaged separately. 
Prior to beginning the installation it is recommended that the hardware be 
inventoried and placed in separate (labeled) boxes to prevent mixing. 
 
Care should be taken to prevent contamination of the air conditioner system!  
All plugs on the plumbing assemblies and system components should not be 
removed until just prior to installation of the part. The exception to this procedure 
is the installation of the receiver / drier bottle. The receiver / drier should be left 
capped and not installed until just prior to servicing the system with refrigerant. 
This prevents the desiccant inside the bottle from becoming saturated with water. 
 
2. REFERANCE DOCUMENT 
 
The approval basis of the system covered by this document is Supplemental 
Type Certificate  
 
 
 
 
 
 
 
 
 
 
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Revision 0         Page 1-1  
						

							 
INSTALLATION DOCUMENTS AS350-200D 
 
CHAPTER 2 
WEIGHT & BALANCE INFORMATION 
 
This page must be removed and placed with the appropriate existing aircraft documents. 
 
Weight breakdown – Eurocopter AS350 series air conditioning system: 
Dwg. AS350-200 (Flat Belt Configuration) AS350-202 (Poly-V Belt Configuration) 
 
Weight & Balance 
 
Item  Wt. (lbs)  X-Arm (in)  X-M (in-lb)  Y-Arm (in)  Y-M (in-lb) 
 94.71 112.3 10,640 13.1 1245 
 
 
Weight breakdown – Eurocopter AS350 series air conditioning system: 
Dwg. AS350-204 (Flat Belt Configuration) AS350-204 (Poly-V Belt Configuration) 
 
Weight & Balance 
 
Item  Wt. (lbs)  X-Arm (in)  X-M (in-lb)  Y-Arm (in)  Y-M (in-lb) 
 97.5 141.9* 13839 6.7* 654 
*RH is positive, X=airframe station (0.0 is forward of the airframe), Y=aircraft butt line (0.0 is airframe centerline) 
 
 
 
 
 
 
 
 
 
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INSTALLATION DOCUMENTS AS350-200D 
 
CHAPTER 3 
FLIGHT MANUAL SUPPLEMENT 
 
1.  FLIGHT MANUAL SUPPLEMENT 
 
The following document must be removed and placed with the appropriate existing 
aircraft documents. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
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