AirComm Corporation Bell 407 Air Conditioner Installation Documents User Manual

							INSTALLATION DOCUMENTS 407EC-200D 
 
 
 
 
 
 
 
 
 
AIR COMM CORPORATION 
1575 W. 124th Avenue 
Westminster, Colorado 80234 
 
 
 
 
 
 
 
 
 
 
 
DOCUMENTS FOR THE INSTALLATION OF THE 
BELL MODEL 407 CABIN AIR CONDITIONING SYSTEM 
 
 
 
 
 
 
 
 
 
 
 
 
 
Revision 4        1 September, 2015 
 
  
						

							INSTALLATION DOCUMENTS 407EC-200D 
 
 
 
RECORD OF REVISION 
 
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2 01/30/06 01/30/06 GP     
3 01/09/12 01/09/12 RL     
4 9/1/2015 9/1/2015 KM     
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
 
 
 
 
 
 
 
 
 
 
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Revision 4           
  
						

							INSTALLATION DOCUMENTS 407EC-200D 
 
 
 
TABLE OF CONTENTS 
 
Identification  Title       Page  
  
Chapter 1  Introduction       1 
    
Chapter 2    General Installation Procedure &  Reference Doc.  2     
   
Chapter 3  Flight Manual Supplement     3 
   
Chapter 4    Supplemental Type Certificate    4 
 
 
 
 
 
 
 
 
 
 
 
 
 
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INSTALLATION DOCUMENTS 407EC-200D 
 
 
CHAPTER 1 
 
INTRODUCTION 
 
This document contains information which is required for the installation and operation 
of the Air Comm Corporation’s air conditioning system installed in the Bell 407 series 
helicopter. After completion of the installation of the air conditioner system the Flight 
Manual Supplement and 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 Bell 407 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 Bell Helicopter models 407 that are equipped with the 
Air Comm Corporation kit number 407EC-201, 407EC-202 and 407EC-203 air 
conditioner systems. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
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INSTALLATION DOCUMENTS 407EC-200D 
 
 
CHAPTER 2 
 
GENERAL INSTALLATION PROCEDURE & REFERENCE DOCUMENT 
 
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. Instructions for installation are provided on the installation 
drawing where appropriate and are not repeated in this document. 
 
It will be necessary to remove transmission cowlings, main cabin headliner, and 
chin bubbles to facilitate the installation of this kit. 
 
System components and associated hardware are packaged separately. Prior to 
beginning installation it is recommended that 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 plumbing assemblies and system components should not be removed 
until just prior to installation of the part. Exception to this procedure is installation 
of the receiver drier bottle. The receiver drier bottle 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. 
 
The approval basis of the system covered by this document is Supplemental 
Type Certificate SR00222DE. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
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INSTALLATION DOCUMENTS 407EC-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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