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AirComm Corporation Airbus EC135 Cabin Air Conditioner Instructions for Continued Airworthiness User Manual
AirComm Corporation Airbus EC135 Cabin Air Conditioner Instructions for Continued Airworthiness User Manual
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INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 25 SYSTEM DESCRIPTION REFRIGERANT CHARGE OIL CHARGE EC135 Air Conditioner system Single Fwd Evaporator 3.8 lbs 1.73 Kg 8.0 oz. 238 ml EC135 Air Conditioner system Dual Fwd Evaporator 4.0 lbs 1.82 Kg 8.0 oz. 238 ml 3. Lubrication Information CAUTION This system is serviced with either Polyester Based Refrigerant Oil (POE) or Double end capped Polyalkylene oil (DEC PAG, aka Ultra PAG). The use of Mineral Oil or Polyalkylene (PAG) in this system will cause damage to the air conditioner compressor and expansion valves. A. The total system oil charge is 8.0 fl oz. (238 ml.) of Double End Capped Polyalkylene Glycol (DEC PAG). The oil is initially contained within the compressor as shipped from the factory so no additional oil is required when installing a new system. B. If oil is spilled during installation/maintenance, or is lost due to a leak in the system, it is necessary to approximate the amount of lost oil and add this amount to the system. C. The oil charge is continuously circulated by the refrigerant during the operation of the system. A quantity of oil is trapped by the compressor. NOTE Maintaining the correct amount of refrigerant and refrigerant oil in the system is critical for ensuring the long life of the compressor. D. The Service Ports for this system are located in the upper aft right-hand corner of the baggage compartment adjacent to the condenser assembly (Figure 13). E. This system may be serviced with either Polyolester (POE) or Double End Capped Polyalkylene Glycol (DEC PAG). Polyalkylene Glycol is preferred due to its superior lubricating properties and improved compressor service life. There are several types of PAG available. Only the “Double End Capped” type is permissible in Air Comm Corporation air conditioning systems. Double End Capped PAG oil is available from Air Comm Corporation in 8 ounce bottles (P/N ES94006-13). Mixing of POE and PAG is acceptable. Disregard previous statements to the contrary. They referenced PAG oil that was not “Double End Capped”. Current versions of compressors are designed to be operated using PAG oil. Testing by Air Comm Corporation has shown that “Double End
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 26 Capped” PAG is compatible with POE and can therefore be mixed. “Double End Capped” is a reference to the chemical structure of the molecule and not to the container. Do not use Mineral oil in this system with R134a refrigerant. Do not use any refrigerant oil other than Double End Capped Polyalkylene Glycol (also known as “ULTRA PAG”) or Polyolester (also POE). Containers of DEC PAG or POE will absorb moisture if left open (hygroscopic). Keep containers tightly capped when not in use and keep all system components capped while servicing system. The quantity of lubrication in the system is critical. If too little lubrication is in the system the compressor life may be reduced. No other component in the A/C system requires lubrication. Too much lubricant in the system will retard heat transfer in the evaporator and condenser coils and reduce the cooling capacity of the system. F. The following chart may be used to calculate the amount of oil to be added in case a component is being replaced with a new part. Component Oil Amount Compressor See Instructions Evaporator 1.0 oz. per evaporator Condenser 1.5 oz. Receiver Drier 1.5 oz. Hose - Vapor 1.0 oz. per 10 foot Hose – Liquid 1.0 oz. per 20 foot 4. System Leak Check A. It is important to identify and eliminate refrigerant leaks at system connections to ensure trouble free operation of the air conditioning system. A new or empty system can be pressurized with R134a at 50 psi (3.5 kgcm) to conduct a leak survey. Do not pressurize the system with compressed air. Compressed air will introduce moisture into the system, which will degrade the operation of the system. The preferred method is to use an electronic leak detector in conjunction with a small charge of R134a refrigerant. All checks done in this manner should be conducted with the air conditioner off. Since the refrigerant is heavier than air, leaks are most likely to be detected on the underside of hoses and fittings. In
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 27 some cases, leaking refrigerant gas may collect in low areas of the aircraft and provide erroneous leak detection. A stream of compressed air from a nozzle may be useful in clearing the area just prior to conducting a leak test. B. If a leak is detected at an O-Ring fitting, check to insure proper torque has been applied to the fitting. If the system continues to leak, reclaim the refrigerant and install a new O-Ring. NOTE Be sure that the O-Ring is lubricated with refrigerant oil prior to its installation. A small amount of leakage (approximately one ounce per year) past the compressor shaft seal is normal. Most leak detectors are sensitive enough to show a leak of this magnitude. 5. Suggested Equipment for Servicing Recovery / Recycling / Recharging Station (Example: Snap-on Model ACT 3340, Robinair Model 34700, or equivalent) Electronic Leak Detector (R134a compatible) (Example: Micro-Tech III, Robinair, Snap-on, or equivalent) Manifold and gauge set (R134a compatible) (Example: Robinair, Snap-on, or equivalent) 6. Consumable Materials A. O-Rings: This system utilizes the refrigerant HFC R134a. Consequently, the system must also utilize Highly Saturated Nitrile (HSN O-Rings) the insert O-Ring fittings (as previously described in this manual) require the use of Green HSN O- Rings while the TORQ LOK® Fittings (As previously described in this manual) require the use of the Black HSN O-Rings. B. Loctite thread sealer 554 (or equivalent). C. Torque-Seal Anti Sabotage Lacquer.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 28 7. Suggested Spares List ITEM PART NUMBER Blower Motor – Aft Evaporator ES61142-3 Blower Motor – Forward Evaporator ES61064-1 Compressor Assembly EC135-3040-1 Compressor Drive Belt ES35135-1 Receiver / Drier Bottle ES43030-6 Binary Switch ES57178-1 By-pass Valve ES26194-24 Condenser Blower ES73186-9 Compressor Drive Bearings ES33100-3 HSN O-Rings; Insert Type (Green) # 6 O-Ring ES44010-2 # 8 O-Ring ES44010-3 # 10 O-Ring ES44010-4 HSN O-Rings; TORQ LOK® Type (Black) #6 O-Ring ES44012-2 #8 O-Ring ES44012-3 #10 O-Ring ES44012-4
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 29 CHAPTER 7 STANDARD PRACTICES AND INFORMATION 1. Fitting Torque Procedures and Values INSERT O-RING FITTINGS TORQ-LOK® FITTINGS Apply a thin coating of refrigerant oil to O-Ring and Female side of fitting. Confirm there is no damage (nicks, dirt, etc.) on fittings. Slide B-nut back away from the end of the tube so you can see the O-Ring as you slide the fitting together. Be careful not to pinch O-Ring during assembly. Engage the male end into the female fitting being careful to maintain alignment. The male flange should seat fully against the female fitting without the O-Ring being pinched. It is important to hold the fitting together while sliding the B-nut forward and engaging the threads. Tighten the B-nut by hand and then torque as follows: a. TORQ LOK® Fittings: Must be hand snug (metal to metal) and then add an additional 30 degrees (one half flat). b. Insert O-Ring Fittings: Must be hand snug against O-ring, and then an additional 60 degrees (one flat). CAUTION: Excessive torque will damage fitting. DO NOT OVER TORQUE ALWAYS USE BACK UP WRENCH INSERT O-RING FITTINGS TORQ-LOK® FITTINGS
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 30 2. Torque Seal. Once system is charged, check each fitting with an electronic leak detector. Once fittings have been checked and are leak free, torque Seal as appropriate. 3. General Information A. Refer to Airbus Model EC135 Maintenance Manual for general removal and installation procedures associated with basic aircraft equipment and components. B. Prepare helicopter for maintenance. Disconnect battery and/or electrical power supply. C. It may be necessary to evacuate (discharge) refrigerant from the system to remove or replace certain components. Instructions for servicing are found in CHAPTER 7. D. All openings and ports in components, hoses, and tubes disconnected or removed to facilitate removal and replacement procedures must be capped or plugged to prevent contamination. E. Retain all parts and attaching hardware for reassembly, unless otherwise noted. F. Always use a back-up wrench on lines and fittings when removing and installing refrigerant plumbing. G. Perform functional checks and/or ground runs to verify component/system operation. 4. Removal and Replacement of Forward Evaporator Assembly (LH or RH) (Figure 8 and Figure 9) Removal A. Discharge refrigerant. See Chapter 6 Servicing for instructions. B. Disconnect refrigerant plumbing from evaporator tube and fittings once refrigerant is evacuated. C. Remove outlet flex duct from the outlet adapter on evaporator by removing cable ties. D. Disconnect drain line from bottom of evaporator by removing cable tie. E. Disconnect blower motor electrical connector. F. Remove attaching hardware securing evaporator assembly to mounting brackets and supports. G. Remove forward evaporator assembly. Installation/Replacement A. Install forward evaporator assembly and secure with retained attaching hardware to mounting brackets and supports.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 31 B. Connect blower motor electrical connector and secure as needed. C. Connect drain line at bottom of evaporator and secure with cable tie. D. Replace all O-Rings before connecting refrigerant plumbing to evaporator tube and fittings. Torque refrigerant line connections per tightening instructions pg.29. E. Connect outlet flex ducts to the outlet adapter on the evaporator and secure with cable ties. F. Service air conditioning system with refrigerant. 5. Removal and Replacement of Forward Evaporator Blower Motor Assembly (LH or RH, Figure 8 and Figure 9) Removal A. Disconnect blower motor electrical connector and cut cable ties to free motor wiring from cable tie mounts on evaporator. B. Remove attaching hardware securing blower motor assembly to evaporator enclosure. Remove blower motor and wheel assembly. C. Cut wire leads at splices and retain wire and connector lead for reuse on new motor. Record correct polarity of connections. D. Loosen retaining set screw and remove blower wheel from blower motor shaft. Retain blower wheel. NOTE It may be necessary to apply heat to the set screw of the blower wheel in order to separate the two parts. Installation/Replacement A. Install retained blower wheel on new motor. Press the blower wheel onto the motor shaft until it stops against motor. Back blower wheel away to achieve a .030” – .040” clearance between blower wheel and new motor. Apply one drop of low strength Loctite to set screw and tighten against flat portion of motor shaft to lock wheel in place (Figure 17). Figure 17: Fwd Evap Blower Motor and Wheel Assembly
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 32 B. Install blower motor and wheel assembly in evaporator enclosure and secure with attaching hardware. C. Install M81824/1-3 or equivalent splices to motor wires and retained connector leads. Observe correct polarity of connections. D. Connect blower motor electrical connector and secure to cable tie mounts as required. 6. Removal and Replacement of Aft Evaporator Assembly (Figure 10) Removal A. Discharge the refrigerant. See chapter 6 Servicing for instructions. B. Remove belly panel below RH seat to gain access to the aft evaporator assembly. C. Disconnect electrical connector to evaporator freeze switch. D. Disconnect return air transition duct from adapter ring on the aft evaporator. E. Disconnect refrigerant plumbing from evaporator fittings once refrigerant is evacuated. F. Remove attaching hardware securing evaporator assembly to mounting brackets and supports. G. Remove aft evaporator assembly. Installation/Replacement A. Install aft evaporator assembly and secure with retained attaching hardware to mounting brackets and supports. B. Connect electrical connector to evaporator freeze switch. C. Connect return air transition duct to adapter ring on the aft evaporator. G. Replace all O-Rings before connecting refrigerant plumbing to evaporator tube and fittings. Torque refrigerant line connections per tightening instructions pg.29. D. Service air conditioning system with refrigerant. 7. Removal and Replacement of Aft Evaporator Blower Motor Assembly (Figure 10) Removal A. Remove belly panel to gain access to the aft evaporator blower assembly. B. Disconnect blower motor electrical connector. C. Remove attaching hardware securing blower motor assembly and mounting brackets. Remove blower motor and wheel assembly from blower housing. D. De-pin wire leads and retain connector for reuse on new motor. Record correct polarity of connections.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 33 E. Note the clearance between blower wheel and forward mount assembly on motor. Record clearance for reference (Figure 18). F. Loosen retaining set screw and remove blower wheel from blower motor shaft. Retain blower wheel. NOTE It may be necessary to apply heat to the set screw of the blower wheel in order to separate the two parts. G. Remove forward and aft mount assemblies and cooling tube from motor. Installation/Replacement A. Install forward and aft mount assemblies and cooling tube on new motor. B. Install retained blower wheel on new motor. Press the blower wheel onto the motor shaft until it stops against motor. Back blower wheel away to achieve the noted clearance between blower wheel and forward mount assembly on motor. Apply one drop of low strength Loctite to set screw and tighten against flat portion of motor shaft to lock wheel in place (Figure 18). Figure 18: Aft Evap Blower Motor and Wheel Assembly C. Install blower motor and wheel assembly in blower enclosure and secure with attaching hardware. D. Install retained connector to motor wires. Observe correct polarity of connections. E. Connect blower motor electrical connector to aircraft wiring and secure as required. Back blower wheel away to achieve .030-.040 clearance between blower wheel and forward mount assembly on motor Forward mount assembly
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS EC135-200M-1 Revision 8 Page 34 F. 8. Removal and Replacement of Condenser Assembly (Figure 11) Removal A. Discharge the refrigerant. See Chapter 6 Servicing for instructions. B. Remove LH aft engine fairing from aircraft to gain access to the condenser assembly. C. Disconnect both condenser blower assembly electrical connectors. D. Disconnect refrigerant plumbing from condenser and receiver drier fittings once refrigerant is evacuated. E. Remove attaching hardware securing condenser assembly to engine deck. F. Remove the condenser assembly. Installation/Replacement A. Install condenser assembly and secure with retained attaching hardware to engine deck. B. Connect electrical connectors to condenser blower assemblies. C. Replace all O-Rings before connecting refrigerant plumbing to condenser and receiver drier tube and fittings. Torque refrigerant line connections per fitting tightening instructions pg.29. D. Service air conditioning system with refrigerant. 9. Removal and Replacement of Condenser Blower Assembly (Figure 11) Removal A. Remove LH aft engine fairing from aircraft to gain access to the condenser assembly. B. Disconnect the appropriate condenser blower assembly electrical connector. C. Remove safety wire and attaching hardware securing blower assembly to the condenser assembly. D. Remove the blower assembly. Installation/Replacement A. Install blower assembly and secure with retained attaching hardware to condenser assembly and apply safety wire per MIL-P-8564, using MS20995C-32 safety wire. B. Connect electrical connector to the condenser blower.