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AirComm Corporation Bell Air Conditioner 206L4 Installation Instructions with TORQLOK Plumbing

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    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
    Revision H   January 19, 2015 
    1575 W. 124th Ave., Westminster CO 80234 Tel 303-440-4075 | Fax 303-440-6355 http://www.aircommcorp.com/ | [email protected] 
     
     
     
     
     
     
     
     
    AIR COMM CORPORATION  
    1575 W. 124th Avenue 
    WESTMINSTER, CO. 80234 
    PHONE: 303-440-4075 FAX: 303-440-6355 
    [email protected] 
     
     
     
    INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 
    BELL HELICOPTER 206L4 
    AIR CONDITIONING SYSTEM  
     
     
     
     
    THIS HANDBOOK INCLUDES THE MAINTENANCE INFORMATION REQUIRED TO 
    BE AVAILABLE BY FAR PART 27 
     
     
     
    NOTE 
    206L4 service Instructions are applicable to 206L1 rotorcraft that have been modified IAW BHT-206-
    SI-2050 engine upgrade and BHT-206-SI-2052 increased gross weight Mod and 206L3 rotorcraft that 
    have been modified IAW BHT-206-SI-2052 increased gross weight Mod. 
     
     
      
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page ii 
     
     
     
     
     
     
     
     
     
     
     
    RESTRICTED DISCLOSURE NOTICE 
     
    THIS PUBLICATION IS THE PROPRIETARY INTELLECTUAL PROPERTY OF AIR COMM 
    CORPORATION AND IS DELIVERED TO THE RECIPIENT WITH THE EXPRESS CONDITION 
    THAT IT AND THE INFORMATION CONTAINED HEREIN ARE NOT TO BE USED, DISCLOSED 
    OR REPRODUCED IN PART OR IN WHOLE, FOR ANY PURPOSE WITHOUT THE EXPRESS 
    WRITTEN CONSENT OF AIR COMM CORPORATION. NO RIGHT IS GRANTED TO THE 
    RECIPIENT TO DISCLOSE OR SO USE ANY INFORMATION CONTAINED IN THIS 
    DOCUMENT OUTSIDE THE PURPOSE FOR WHICH IT WAS DELIVERED. THESE 
    RESTRICTIONS DO NOT OPERATE TO NULLIFY OR LIMIT ANY RIGHTS GRANTED BY 
    CONTRACT.  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page iv 
     
    LIST OF EFFECTIVE PAGES 
     
    LIST OF EFFECTIVE PAGES 
    Title Page(s) Revision No. 
    Record of Revisions iii H 
    List of effective Pages  iv H 
    Table of Contents v-vi H 
    Chapter 1 Introduction 1-6 H 
    Chapter 2 Airworthiness Limitation Section  7 H 
    Chapter 3 Inspections  8-12 H 
    Chapter 4 Location and Access 13-20 H 
    Chapter 5 Placards and Markings 21-23 H 
    Chapter 6 Servicing 24-26 H 
    Chapter 7 Standard Practices  27-42 H 
    Chapter 8 Troubleshooting  43-46 H 
     
    Appendix A  
    Weight and Balance information  47  H  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page v 
     
    TABLE OF CONTENTS 
     
    CHAPTER PAGE 
     
    CHAPTER 1 ..................................................................................................................................... 1 
    INTRODUCTION .......................................................................................................................... 1 
    1. SCOPE................................................................................................................................ 1 
    2. PURPOSE ........................................................................................................................... 1 
    3. ARRANGEMENT ................................................................................................................ 1 
    4. APPLICABILITY .................................................................................................................. 1 
    5. DEFINITIONS ..................................................................................................................... 1 
    6. ABBREVIATIONS ............................................................................................................... 2 
    7. PRECAUTIONS .................................................................................................................. 3 
    8. UNITS OF MEASUREMENT ............................................................................................... 3 
    9. INFORMATION ESSENTIAL TO THE CONTINUED AIRWORTHINESS OF THE AIR 
    CONDITIONER. .................................................................................................................. 3 
    10. REFERENCE DOCUMENTS .............................................................................................. 3 
    11. DISTRIBUTION ................................................................................................................... 3 
    12. CHANGES TO INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ........................... 4 
    13. SYSTEM DESCRIPTION AND OPERATION ..................................................................... 4 
    14. DESCRIPTION OF THE VAPOR CYCLE AIR CONDITIONER AND ITS INSTALLATION . 4 
    15. Refrigeration Cycle Schematic ............................................................................................ 6 
    CHAPTER 2 ..................................................................................................................................... 7 
    AIRWORTHINESS LIMITATION SECTION ................................................................................. 7 
    CHAPTER 3 ..................................................................................................................................... 8 
    INSPECTIONS ............................................................................................................................. 8 
    1. INSPECTION REQUIREMENTS: ....................................................................................... 8 
    2. INSPECTION PROCEDURES. ........................................................................................... 9 
    3. COMPONENT OVERHAUL / REPLACEMENT SCHEDULE ............................................ 12 
    CHAPTER 4 ................................................................................................................................... 13 
    LOCATION AND ACCESS ......................................................................................................... 13 
    1. LOCATION OF AIR CONDITIONER FEATURES ............................................................. 13 
    CHAPTER 5 ................................................................................................................................... 21 
    PLACARDS AND MARKINGS .................................................................................................... 21 
    CHAPTER 6 ................................................................................................................................... 24 
    SERVICING ................................................................................................................................ 24 
    1. CHARGING PROCEDURE ............................................................................................... 24 
    2. REFRIGERANT PRESSURE ............................................................................................ 24 
    3. SAFETY PRECAUTIONS ................................................................................................. 24 
    4. TOOLS, EQUIPMENT, AND CONSUMABLES ................................................................. 25 
    CHAPTER 7 ................................................................................................................................... 27 
    STANDARD PRACTICES .......................................................................................................... 27 
    1. O-RING TYPE FITTINGS .................................................................................................. 27 
    2. SYSTEM LEAK CHECK. ................................................................................................... 28 
    3. TORQUE SEAL. ................................................................................................................ 28 
    4. INSTALLATION & REPLACEMENT OF THE WIRE HARNESS ELECTRICAL 
    CONNECTORS FOR THE EVAPORATOR AND CONDENSER BLOWERS ................... 28 
    5. REMOVE AND REPLACE COMPRESSOR (Figure 11) ................................................... 30  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page vi 
    6. REMOVE AND REPLACE COMPRESSOR DRIVE BELT (Figure 12). ............................ 31 
    7. REMOVE AND REPLACE COMPRESSOR DRIVE PULLEY (Figure 12) ........................ 35 
    8. REMOVE AND REPLACE FORWARD EVAPORATOR (Figure 14) ................................. 35 
    9. REMOVE AND REPLACE AFT EVAPORATOR (Figure 15) ............................................ 36 
    10. REMOVE AND REPLACE AFT EVAPORATOR BLOWER (Figure 15) ............................ 37 
    11. REMOVE AND REPLACE CONDENSER BLOWER ASSEMBLY (Figure 16 and Figure 
    17). .................................................................................................................................... 38 
    12. REMOVE AND REPLACE CONDENSER HEAT EXCHANGER (Figure 18). ................... 38 
    13. REMOVE AND REPLACE BYPASS VALVE (Figure 19). ................................................. 41 
    14. REMOVE AND REPLACE BINARY SWITCH (Figure 19)................................................. 41 
    CHAPTER 8 ................................................................................................................................... 43 
    TROUBLESHOOTING ................................................................................................................ 43 
    1. System Troubleshooting ................................................................................................... 43 
    2. ELECTRICAL .................................................................................................................... 43 
    3. SYSTEM CHARGE ........................................................................................................... 44 
    4. EXPANSION VALVE MALFUNCTION .............................................................................. 44 
    5. COMPRESSOR MALFUNCTION ..................................................................................... 44 
    6. SYSTEM LEAK CHECK .................................................................................................... 44 
    APPENDIX A .................................................................................................................................. 47 
    WEIGHT AND BALANCE DATA ................................................................................................. 47  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page 1 
     
    CHAPTER 1 
    INTRODUCTION 
    1. SCOPE 
    The scope of this manual encompasses the scheduled and unscheduled maintenance 
    procedures for the continued airworthiness of the Air Comm Corporation air conditioning 
    system installed in the Bell 206L4 series helicopter. 
    2. PURPOSE  
    The purpose of this manual is to provide the aircraft mechanic in the field the necessary  
    information to maintain the air conditioning system.  
    3. ARRANGEMENT 
    This manual 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 manual in the 
    Table of Contents, and are further identified by their individual page number.   
    4. APPLICABILITY  
    This manual is applicable to Bell Helicopter 206L4 models that are equipped with the Air 
    Comm Corporation kit number 206EC-210 air conditioner system. 
    NOTE 
    206L4 service Instructions are applicable to 206L1 rotorcraft that 
    have been modified IAW BHT-206-SI-2050 engine upgrade and 
    BHT-206-SI-2052 increased gross weight Mod and 206L3 rotorcraft 
    that have been modified IAW BHT-206-SI-2052 increased gross 
    weight Mod. 
     
    5. DEFINITIONS 
    The following terms are provided to give a ready reference to the meaning of some of the 
    words contained within this manual. These definitions may differ from those given by a 
    standard dictionary. 
    Ambient air temperature: The temperature of the air surrounding a person or object. 
    Charging station: An air conditioning system service unit capable of evacuating and 
    charging an air conditioner. 
    Condensation: The process of changing a vapor into a liquid. 
    Desiccant: A material used in the receiver/drier bottle, designed to absorb moisture from 
    the refrigerant. 
    Glazing: A shiny coating caused by excessive heat. 
    Heat load: The amount of heat which the air conditioner is required to remove from the 
    aircraft cabin. 
    Inches of mercury: A measurement of pressure, normally used for pressures below 
    atmospheric, one inch of mercury is equal to approximately one half pound per square inch.  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page 2 
     
    Pressure, ambient: The pressure of the air surrounding a body, normally measured in 
    Pounds Per Square inch gauge, or PSIG. 
    Refrigerant: A fluid which is used in an air conditioning system to absorb heat from the 
    cabin and carry it outside the helicopter where it can be transferred to the outside air. 
    Relative humidity: The ratio of the amount of water vapor in the air to the amount of water 
    vapor required to saturate the air at the existing temperature. 
    Thermostat: An air conditioning control which senses the temperature of the evaporator 
    coil and causes the system to cycle or by-pass to maintain the proper temperature of 
    cooling air. 
    Vacuum: A negative pressure, or pressure below atmospheric; it is usually expressed in 
    inches of mercury. 
    Vapor: The gaseous state of a material. 
    6. ABBREVIATIONS 
    InHg: Inches of Mercury 
    Lbs: Pounds 
    oz: Ounces 
    Psig: Pounds Per Square Inch (gauge) 
    gr: Grams 
    kg: Kilograms 
    Kg/cm: Kilograms Per Centimeter 
    ml: Milliliters 
    mm: Millimeters 
    Nm: Newton-meters  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page 3 
     
    7. PRECAUTIONS 
    The following precautions are found throughout this manual, and will vary depending on the 
    seriousness of the Hazard or Condition: 
    WARNING: May  be a maintenance procedure, practice, condition, etc., which could result 
    in personal injury or loss of life. 
    CAUTION: May  be a maintenance procedure, practice, condition, etc., which could result 
    in damage or destruction of equipment. 
    NOTE: May  be a maintenance procedure, practice, condition, etc., or a statement which 
    needs to be highlighted. 
    8. UNITS OF MEASUREMENT 
     All measurements contained within this manual are generally given in the United States 
    standard measurement, with metric conversions in parentheses as needed. 
    9. INFORMATION  ESSENTIAL  TO  THE  CONTINUED  AIRWORTHINESS  OF  THE  AIR 
    CONDITIONER. 
     This manual provides information which is required for operation and maintenance of the 
    Air Comm air conditioning system installed in the Bell model 206L series helicopter. After 
    completion of the air conditioner installation this document must be placed with the 
    appropriate existing aircraft documents. 
    10. REFERENCE DOCUMENTS 
     The approval basis of the system covered by this ICA is Supplemental Type Certificate 
    SH2750NM 
    11. DISTRIBUTION 
     This document is to be placed with the aircraft maintenance records at the time of system 
    installation. 
     Changes will be made to this document in response to “Safety of Flight”, and or “Non-safety 
    of Flight” issues. Any changes will result in a revision to this document. Revisions shall be 
    noted in the Record of Revisions (page iii), and on the List of Effective Pages (page iv) of 
    this manual. 
     In addition to the revision of the manual, those changes categorized as “Safety of Flight” 
    shall have a Service Bulletin issued to the operator providing the necessary information to 
    comply with, and or to correct, the “Safety of Flight” issue. 
     Replacement, and or revised copies of this manual may be obtained by contacting: 
    Air Comm Corporation Service Department 
    1575 W. 124th Ave STE 210 
    Westminster, CO.80234 
    Phone No. 303-440-4075 Fax No. 303-440-6355 
    [email protected]  
    						
    							INSTRUCTIONS FOR CONTINUED AIRWORTHINESS - 206EC-270M-1 
     
    Revision H  Page 4 
     
    12. CHANGES TO INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 
     Changes made to a line or paragraph of this document will be indicated by a vertical bar in 
    the right hand margin, while a complete page change will be indicated by a vertical bar next 
    to the page number. 
    (Example: Any change will appear with a vertical bar next to that change). 
    13. SYSTEM DESCRIPTION AND OPERATION 
     The 206EC-206 system is a vapor cycle type Air Conditioner consisting of a Compressor, 
    Condenser, Dryer, By-pass valve, and Multiple Evaporator assemblies. 
     The Compressor is belt driven off of the tail rotor drive shaft, which is located in the engine 
    compartment. 
     The Condenser assembly is located below the baggage compartment floor. Cooling air is 
    forced through the condenser by a 28V DC electric blower, and an electrically actuated 
    scoop that opens and closes when the system is switched from OFF to ON to OFF. 
     Each evaporator assembly contains a 28V DC, two speed electric blower that allows the 
    system to be switched to ether a High or Low setting. 
     A refrigerant gas by-pass valve is located aft of the baggage compartment. The purpose of 
    this valve, (which is set at the factory) is to prevent evaporator heat exchanger freeze-up by 
    controlling the minimum evaporator pressure (temperature).  
     The system incorporates a binary high/low pressure “cut-out” switch. This switch is intended 
    to protect the compressor in case of system over-pressure or loss of refrigerant. The switch 
    is located adjacent to the system charging ports ( Aft of the baggage door on the L/H side of 
    the aircraft) and is wired in series with the compressor clutch. 
     Switch operating pressures: Low Pressure function – 
     Open @ 28 ± 2.8 psi 
     Close @ 29 ± 4.3 psi 
     High Pressure function – 
     Open @ 384 ± 30 psi 
     Close @ 289 ± 43 psi 
    14. DESCRIPTION  OF  THE  VAPOR  CYCLE  AIR  CONDITIONER  AND  ITS 
    INSTALLATION 
    This section contains a general overview of a Vapor-cycle air conditioning system and how 
    it functions. This type of system operates in a closed loop, in which the refrigerant absorbs 
    heat from the cabin, and rejects it into the outside air. The refrigerant then returns to the 
    cabin to repeat the cycle. The operation of the system is described below, and illustrated 
    schematically in Figure 1. 
    Liquid refrigerant is contained in the receiver-drier under pressure from the compressor. 
    The receiver-drier also filters the refrigerant through a material know as desiccant. The 
    desiccant ensures that the fluid leaving this component is free of any water or other 
    contaminants.  
    						
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