AirComm Corporation Cabin Air Conditioner A119 Installation Documents User Manual

							INSTALLATION DOCUMENTS A119-200D 
          
AIR COMM CORPORATION 
1575 West 124th Ave 
Westminster, CO 80234         
DOCUMENTS FOR THE INSTALLATION OF THE 
AGUSTA MODEL A119 / AGUSTA WESTLAND AW119 MKII   
CABIN AIR CONDITIONING SYSTEM 
  
   
Revision 6               4 November 2015 
   
						

							 
INSTALLATION DOCUMENTS A119-200D  
   
RECORD OF REVISION   
REVISION NUMBER  ISSUE 
DATE  DATE 
INSERTED 
 
BY  Description of Change 
1  02/01/06  02/01/06  GP  Added -206 weight and balanc e info. 
2  05/05/06  05/05/06  GP  Added -208 weight and balance info. 
3  12/15/06  12/15/06  GP  Added -210 weight and balance info. 
4  07/02/07  07/02/07  GP  Added Agusta Westland AW119  MKII 
5  10/12/09  10/12/09  GP  Added -212 weight and balance info. 
6  11/04/15  11/04/15  BD  Updated address on cover & FMS to Revision 6 
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
        
           
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							 INSTALLATION DOCUMENTS A119-200D  
LIST OF EFFECTIVE PAGES   
LIST OF REVISIONS    Revision 0 (Original Issue)…11 O ctober, 2001 
          Revision 1 ……………………1 February 2006  
          Revision 2 …………………….5 May 2006 
          Revision 3 …………………….15 December 2006 
          Revision 4 ……………………. 2 July 2007 
          Revision 5 ……………………. 12 October 2009 
          Revision 6……………………….4 November 2015  
LIST OF EFFECTIVE PAGES 
Title                  Page(s)  Revision No. 
Record of Revisions             i      6  
List of Effective Pages            ii      5 
Table of Contents              iii      0 
Chapter 0 Introduction            0-1      5 
Chapter 1 General installation procedure &      1-1      0 
Reference Document 
Chapter 2 Weight & Balance Information       2-1      5 
Chapter 3 Flight Manual Supplement        3-1      6 
Chapter 4 Supplemental Type Certificate      4-1      0                  THIS AREA INTENTIONALLY LEFT BLANK 
               
						

							Revision 5                  Page ii   INSTALLATION DOCUMENTS A119-200D  
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                THIS AREA INTENTIONALLY LEFT BLANK 
                
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							   INSTALLATION DOCUMENTS A119-200D  
CHAPTER 0 
INTRODUCTION   
This document contains information, which is requir ed for the installation and operation 
of the Air Comm Corporation’s air conditioning syst em installed in the Agusta A119 & 
Agusta Westland AW119 MKII series helicopter. After  completion of the installation of 
the air conditioner system the Weight & Balance Inf ormation, Flight Manual 
Supplement, and the Supplemental Type Certificate m ust be removed from this 
document and placed with the appropriate existing a ircraft documents. 
 
1.  SCOPE   The scope of this document encompasses the general  procedures and reference 
documentation necessary to install the Air Comm Cor poration air conditioning 
system in the Agusta A119 & Agusta Westland AW119 M KII series helicopter. 
 
2.  PURPOSE   The purpose of this document is to provide the airc raft 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 br oken 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 Agusta Helicopter mo dels A119 that are equipped 
with the Air Comm Corporation kit number A119EC-212  air conditioner system. 
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							   INSTALLATION DOCUMENTS A119-200D 
  CHAPTER 1 
GENERAL INSTALLATION PROCEDURE & REFERENCE DOCUMENT  
  1.  GENERAL INSTALLATION PROCEDURE 
  This section is intended to supplement the informat ion contained on the 
installation drawings. All details and notes contai ned on the drawings should be 
reviewed carefully. As instructions for installatio n are provided on the installation 
drawing where appropriate, and are not repeated in  this document. 
 
It will be necessary to remove the transmission cow lings, the main cabin 
headliner, Chin bubbles, to facilitate the installa tion of this kit. 
 
The system components and associated hardware are p ackaged separately. 
Prior to beginning the installation it is recommend ed that the hardware be 
inventoried and placed in separate (labeled) boxes  to prevent mixing. 
 
Care should be taken to prevent contamination of th e air conditioner system!  
All plugs on the plumbing assemblies and system com ponents should not be 
removed until just prior to installation of the par t. 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 servic ing the system with refrigerant. 
This prevents the desiccant inside the bottle from  becoming saturated with water. 
  2.  REFERENCE DOCUMENT 
  The approval basis of the system covered by this do cument is Supplemental 
Type Certificate  SR00463DE 
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CHAPTER 2 
WEIGHT & BALANCE INFORMATION   
This page must be removed and placed with the appro priate existing aircraft documents. 
 
Weight & Balance / Weight breakdown – Agusta A119 A ir Conditioner System: 
 Ref. Dwg. A119-212 
English Units 
Item Wt. (lbs) 
 
X-Arm (in) 
 
X-M (in-lb) 
 
Y-Arm (in) 
 
Y-M (in-lb) 
 
 
Total  
A119-212  99.67  134.9  13,444.9  -1.88  -187.6   
 
Metric Units 
 
Item Wt.  
(kg) 
X-Arm  
(mm) 
X-M  
(kg-mm) 
Y-Arm  
(mm) 
Y-M  
(kg-mm) 
 
Total  
A119-212  45.30  3426  155227  -47.8  -2165   
 
Weight Breakdown (Dual Forward Evaporator Blowers)   
English Units 
Item Wt.  
(lbs) 
X-Arm  
(in) 
X-M  
(in-lb) 
Y-Arm  
(in) 
Y-M  
(in-lb) 
 
Total  
A119-212  105.8  129.2  13,669.4  -1.56  -165.5   
 
Metric Units 
 
Item Wt.  
(kg) 
X-Arm  
(mm) 
X-M  
(kg-mm) 
Y-Arm  
(mm) 
Y-M  
(kg-mm) 
 
Total  
A119-212  50.0  3257.6  156,241.2  -50.4  -1,891.7   
  
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							   INSTALLATION DOCUMENTS A119-200D  
CHAPTER 3 
FLIGHT MANUAL SUPPLEMENT   
1.  FLIGHT MANUAL SUPPLEMENT   The following document must be removed and placed w ith the appropriate existing 
aircraft documents. 
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