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Maintenance Manual with Illustrated Parts Catalog

CESSNA 172S Skyhawk · Systems Description

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Overview

This document is a Maintenance Manual with Illustrated Parts Catalog specifically for the Cessna Model 172 equipped with a Keith Products air-conditioning system. It provides maintenance technicians with detailed instructions for servicing, troubleshooting, and maintaining the air-conditioning system. The manual includes a comprehensive overview of the air-conditioning system's components, operation, and maintenance procedures, ensuring that technicians can effectively manage the system's performance and reliability. It also contains safety warnings and operational guidelines to prevent accidents during maintenance activities.

  • The air-conditioning system uses R134a refrigerant and operates from the main 28 VDC electrical bus.
  • To activate the air-conditioning system, the engine must be running and the control switch set to AIR COND.
  • Regular inspections of the air-conditioning system should occur every 600 hours or annually, whichever comes first.
  • Troubleshooting charts are provided for diagnosing insufficient cooling and other common issues.
  • Maintenance procedures include checking refrigerant levels and inspecting components for wear or damage.

Document

Source

Originally published by acethermalsystems.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Systems Description
Year
2007
Pages
68
File size
2.1 MB
Publisher
acethermalsystems.com
How rare is it?
43CESSNA 172S Skyhawk registered worldwide · 0 active

Common. Rarer than 2% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the CESSNA 172S Skyhawk.

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In this document

Air-Conditioning System Description

The air-conditioning system utilizes R134a refrigerant to cool the aircraft cabin. Key components include a compressor, condenser, receiver/drier, expansion valve, and evaporator. The compressor is driven by the engine and compresses low-pressure gas into high-pressure gas, which is then cooled in the condenser before entering the evaporator to cool the cabin air.

System Operation

To operate the air-conditioning system, the engine must be running. The system is activated by placing the control switch in the AIR COND position. For maximum cooling, the fan switch should be set to HI, and cabin doors should be closed. The system can be turned off by switching the control to OFF.

Troubleshooting

The manual includes troubleshooting charts for diagnosing issues with the air-conditioning system. Common problems include insufficient cooling, which may be caused by low refrigerant levels, a faulty expansion valve, or a blocked condenser. The manual provides corrective actions for each identified issue.

Maintenance Procedures

Maintenance procedures cover the inspection and servicing of the air-conditioning system. This includes checking refrigerant levels, inspecting components for dirt or damage, and ensuring proper operation of the compressor and blowers. Specific tools and equipment required for maintenance are also listed.

Inspection/Checks

Regular inspections are recommended to maintain system efficiency. Inspections should include checking for dirt or damage to components, ensuring proper refrigerant levels, and verifying the condition of the compressor belt. The manual specifies intervals for these inspections.

Safety notes

  • Do not operate the air-conditioning system with the condenser air outlet blocked.
  • Always wear safety goggles when servicing the refrigerant system to prevent contact with eyes.
  • Liquid R134a can cause frostbite; avoid contact with skin.

Full document text

Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 Record of Revisions Page ii December 11, 2007 RECORD OF REVISIONS REV DATE DESCRIPTION BY APPV NC 7/29/02 Initial Release BCS MAK A 9/20/02 Added 21-50-06 to List of Effective Pages Reason: ER2000 RCG MAK B 6/1/06 Revised I/B’s to section 21-50-06: Pg. 101 & added “Inactive after January 11, 2006." Added to section 21-50-06: Pg. 103 renumber I/N’s 6-15, added I/N’s 6, 13, 14, 15 & added “Use 172-0251-1 for spares replacement.” Listed all pages #’s in section 21-50-06 to the List of Effective Pages & Table of Contents Revised section 21-50-01 page 2 was 172-0250 evaporator assembly now 172-0251-1 Added a page to List of Effective Pages Deleted a page from Table of Contents Added to section 21-50-06 page vii to IPC, Evaporator, Compressor, Condenser, Electrical, Plumbing Revised Table of Contents & Introduction page #’s Reason: Product Improvement per ER3084 CDW MAK C 3/14/07 Revised Section 21-50-06, I/N 6 on pg 403 WAS JBS75-7 NOW ES51000-1 Revised Section 21-50-06, I/N 15 on pg 505 WAS JBS6009-2 NOW JBS6009-9 Added pgs: 601-604 to Section 21-50-06 Reason: Drafting Error per ER3418 AJ MAK D 12/14/07 Added I/B’s: 3, 4, 5, 6, 8, 10, 11, 15, 16, 20, 27, 28, 29, 30, 31, 32, 33, 34, 35, & 36 to pg 501 Added I/B’s: 3, 4, 6, 23, 41, 44, 48, & 55 to pg 502 Added I/B’s: 3, 4, 5, 6,16, & 32 to pg 503 Added I/B’s: 7, 9, 14, 24, 37, 39, 40, 41, 43, 44, 45, 48, 49, 50, 51, & 54 to pg 504 Added pages 505-507 and page 509 Added I/N’s 20-41 to page 508 Edited I/N 2 WAS 172-0801-1 hose assembly Qty 1 Edited I/N 3 WAS 172-0802-1 hose assembly Qty 1 Edited I/N 4 WAS 172-0803-1 hose assembly Qty 1 Edited I/N 5 WAS 172-0804-1 hose assembly Qty 1 Edited I/N 6 WAS 172-0805-1 hose assembly Qty 1 Edited I/N 7 WAS 172-0806-1 hose assembly Qty 1 Reason: Drafting Error per ER3684 AJ MAK Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 List of Service Bulletins Page iv July 29, 2002 LIST OF SERVICE BULLETINS SB No. DATE SUBJECT REV DATE INCORP. Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 List of Effective Pages Page v October 14, 2009 LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE Title i Oct 14, 2009 List Of Revisions ii Dec 11, 2007 iii Oct 14, 2009 List of Service Bulletins iv Oct 14, 2009 List of Effective Pages v Oct 14, 2009 vi Oct 14, 2009 vii Oct 14, 2009 Table of Contents viii Oct 14, 2009 Introduction ix Oct 14, 2009 x Oct 14, 2009 21-50-00 A/C System, System Description 1 July 29, 2002 2 July 29, 2002 3 July 29, 2002 Troubleshooting 101 July 29, 2002 102 July 29, 2002 103 July 29, 2002 104 July 29, 2002 105 July 29, 2002 Maintenance Practices 201 July 29, 2002 202 July 29, 2002 System Servicing 301 July 29, 2002 302 July 29, 2002 303 July 29, 2002 304 July 29, 2002 Inspection 601 July 29, 2002 602 July 29, 2002 603 July 29, 2002 Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 List of Effective Pages Page vi October 14, 2009 CHAPTER SECTION SUBJECT PAGE DATE 21-50-01 Electrical Description and Operation 1 2 July 29, 2002 Oct 14, 2009 Troubleshooting 101 July 29, 2002 102 July 29, 2002 103 July 29, 2002 104 July 29, 2002 105 July 29, 2002 106 July 29, 2002 107 July 29, 2002 21-50-02 Plumbing Description and Operation 1 July 29, 2002 Maintenance Practices 201 July 29, 2002 21-50-03 Compressor Description and Operation 1 July 29, 2002 Maintenance Practices 201 July 29, 2002 21-50-04 Condenser Description and Operation 1 July 29, 2002 Maintenance Practices 201 July 29, 2002 21-50-05 Evaporator Description and Operation 1 July 29, 2002 Maintenance Practices 201 July 29, 2002 21-50-06 Illustrated Parts Catalog 1 July 29, 2002 101 Oct 14, 2009 102 Oct 14, 2009 103 March 17,2006 201 July 29, 2002 202 July 29, 2002 301 July 29, 2002 302 July 29, 2002 401 Oct 14, 2009 402 July 29, 2002 403 March 14, 2007 501 Dec 11, 2007 502 Dec 11, 2007 503 Dec 11, 2007 504 Dec 11, 2007 Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 List of Effective Pages Page vii October 14, 2009 CHAPTER SECTION SUBJECT PAGE DATE 505 Dec 11, 2007 506 Dec 11, 2007 507 Dec 11, 2007 508 Dec 11, 2007 509 Dec 11, 2007 602 March 14, 2007 603 March 14, 2007 604 March 14, 2007 Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 Introduction Page viii October 14, 2009 TABLE OF CONTENTS SUBJECT SECTION PAGE Introduction ix Air-conditioning System 21-50-00 Description and Operation 1 Troubleshooting 101 Maintenance Practices 201 System Servicing 301 Inspection 601 Electrical 21-50-01 Description and Operation 1 Troubleshooting 101 Plumbing 21-50-02 Description and Operation 1 Maintenance Practices 201 Compressor 21-50-03 Description and Operation 1 Maintenance Practices 201 Condenser 21-50-04 Description and Operation 1 Maintenance Practices 201 Evaporator 21-50-05 Description and Operation 1 Maintenance Practices 201 Illustrated Parts Catalog 21-50-06 1 Evaporator 101 Compressor 201 Condenser 301 Electrical 401 Plumbing 501 Cabin Air Duct 601 Exhaust / Intake 701 Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 Introduction Page ix October 14, 2009 INTRODUCTION 1. PURPOSE The purpose of this System Service Manual is to provide detailed instructions for the servicing, troubleshooting, checking and maintaining of the Cessna Model 172 with Keith Products, Inc. air-conditioning system. The System Service Manual supplements the Maintenance Manual supplied by Cessna for your particular aircraft. 2. SCOPE The scope of the System Service Manual provides the maintenance technician with detailed information covering: - Overall system level description and theory of operation. - Component level description and theory of operation.

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- System level checking and troubleshooting procedures. - Procedures for servicing the air-conditioning system refrigerant. - The identification of special equipment to accomplish the specific tasks. Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 Introduction Page x October 14, 2009 3. GLOSSARY Nonstandard abbreviations and symbols used in the Maintenance Manual are described below. A/C - Air-conditioning A/R - As Required Assy - Assembly Comm. Avail. - Commercially Available Evap - Evaporator Gnd - Ground GPU - Ground Power Unit SW - Switch VDC - Volts Direct Current Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 1 July 29, 2002 AIR-CONDITIONING SYSTEM SYSTEM DESCRIPTION 1. AIR-CONDITIONING SYSTEM DESCRIPTION The Keith Products vapor cycle air-conditioning system uses liquid refrigerant R134a to cool the aircraft cabin. The major components for the R134a air- conditioning system consist of a compressor, condenser, receiver/drier, expansion valve, and evaporator. The starter ring-gear pulley turns the compressor via a belt. Figure 1 shows an operational schematic of the air-conditioning system. The gas in the suction hose is pumped into the discharge hose and through the refrigerant system by the compressor. The compressor takes the low- temperature, low-pressure gas and compresses it to a high-temperature, high- pressure gas. After the high-temperature, high-pressure gas leaves the compressor it enters the condenser. A 28 VDC blower forces air from the left hand side of the aircraft in the inlet duct and through the condenser. The air exits the condenser and leaves the condenser through the exhaust duct on the right hand side of the tailcone. This air cools the high-temperature, high-pressure gas as much as 100ºF. The gas is cooled until it condenses to a medium-temperature, high-pressure liquid. After the medium-temperature, high-pressure liquid leaves the condenser it enters the receiver/drier. The receiver/drier stores liquid refrigerant and filters any moisture out of the refrigerant. After the medium-temperature, high-pressure liquid leaves the receiver/drier it enters the expansion valve. The expansion valve allows the medium-temperature, high-pressure liquid to expand to a low-temperature, low-pressure spray of liquid. After the low-temperature, low-pressure spray of liquid leaves the expansion valve it enters the evaporator. A 28 VDC blower forces air from the cabin through the evaporator. Since the refrigerant in the evaporator can be as cold as 30ºF, the air from the cockpit causes the low-temperature, low-pressure liquid spray to boil and then evaporate. This low-temperature, low-pressure gas passes through the suction hose into the compressor. The refrigerant cycle continues, cooling the aircraft cabin. Air from the cabin is cooled as it passes through the evaporator and comes into contact with the refrigerant. Since the air is cooled, moisture from the air condenses in the evaporator and liquid water is formed. The water then drains overboard through the floor of the aircraft. Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 2 July 29, 2002 Figure 1. Air-conditioning Vapor Cycle System Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 3 July 29, 2002 2. SYSTEM OPERATION The air-conditioning system is operated with the engine operating and power supplied to the aircraft electrical system. To operate the system proceed as follows: 1) Turn on air-conditioning system by placing left hand control switch in the AIR COND position. 2) For maximum cooling, place the FAN switch in the HI position, and close cabin and baggage doors. 3) Turn off air-conditioning system by placing left hand control switch in the OFF position. 4) Airflow may be varied by switching the FAN control switch between the LO and HI positions. 5) Cabin air may be re-circulated without the air-conditioning system operating by placing the left hand control switch in the FAN position. Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 101 July 29, 2002 AIR-CONDITIONING SYSTEM TROUBLESHOOTING 1. GENERAL The procedures below present troubleshooting charts for the air-conditioning system and the compressor. A diagnoses chart is presented for insufficient air- conditioning system cooling. The performance of the air-conditioning system varies with ambient temperature and humidity. The information below presents possible air-conditioning system problems and solutions. CAUTION: Do not operate air-conditioning system with condenser air outlet blocked. 2. AIR-CONDITIONING SYSTEM DIAGNOSIS CHART The following pages show a procedure for diagnosing air-conditioning system problems that will expedite the troubleshooting process. 21-50-00 Page 102 July 29, 2002 INSUFFICIENT COOLING SUCTION PRESSURE IS HIGH EXPANSIO0N VALVE IS OPEN EXCESSIVELY. CHECK SENSING BULB INSTALLATION. IF SECURE & WELL INSULATED, THEN REPLACE EXPANSION VALVE. IF NOT, THEN SECURE AND PROPERLY INSULATE AND RETEST. PLUMBING AT RECEIVER/DRIER OUTLET HAS LOW TEMPERATURE. RECEIVER/DRIER IS RESTRICTED. REPLACE RECEIVER/DRIER. BUBBLES IN SIGHT GLASS CHECK REFRIGERATION LINE FOR GAS LEAKS, AND REPAIR LEAKS IF ANY. CHARGE REFRIGERANT TO CORRECT LEVEL. IN CASE OF TOO MANY LEAKS, STOP COMPRESSOR, DISCHARGE THE SYSTEM, EVACUATE AND RECHARGE THE SYSTEM. AS NECESSARY, REPLACE RECEIVER/DRIER. AIR IN SYSTEM MAY CAUSE BUBBLES IN SIGHT GLASS. DISCHARGE PRESSURE IS HIGH CONDENSER AIR TEMP, TOO HIGH SYSTEM PRESSURES ARE ABNORMAL TEMPERATURE OF DISCHARGE AIR IS ABNORMAL, BUT SYSTEM PRESSURE IS NORMAL. OPERATE AIR-CONDITIONING SYSTEM. WITH MANIFOLD GAUGE, CHECK SYSTEM SUCTION AND DISCHARGE PRESSURES. MEASURE TEMPERATURE OF EVAPORATOR AND CONDENSER DISCHARGE AIR. NO BUBBLES IN SIGHT GLASS 1. OVERCHARGE OF REFRIGERANT DISCHARGE SOME OF REFRIGERANT TO CORRECT LEVEL 2. AIR IS MIXED IN. DISCHARGE SYSTEM, AND REPLACE RECEIVER/DRIER. EVACUATE AND RECHARGE SYSTEM 3. CONDENSER’S FINS ARE DENTED OR CLOGGED WITH DUST. CLEAN PER SERVICING INSTRUCTIONS SUCTION PRESSURE IS LOW FINS AND TUBES OF EVAPORATOR HAVE SOME DENTS. REPLACE OR REPAIR EXPANSION VALVE IS TOO RESTRICTIVE OR GAS LEAKAGE FROM SENSING ELEMENT. REPLACE EXPANSION VALVE. EVAPORATOR AIR TEMP TOO HIGH CLEAN OR REPLACE CONDENSER CLEAN OR REPLACE EVAPORATOR SUCTION PRESSURE IS HIGH WHILE DISCHARGE IS LOW REPAIR OR REPLACE COMPRESSOR FIGURE 2: AIR-CONDITIONING SYSTEM DIAGNOSIS CHART Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 103 July 29, 2002 3. AIR-CONDITIONING SYSTEM TROUBLESHOOTING CONDITION SERVICE PRESSURE GAUGE READING PROBABLE CAUSE CORRECTIVE ACTION INSUFFICIENT REFRIGERANT CHARGE Insufficient cooling. Bubbles appear in sight glass. SUCTION PRESSURE: below normal DISCHARGE PRESSURE: below normal Refrigerant is low, or leaking a little. 1. Leak test. 2. Repair leak. 3. Charge system. Evacuate as necessary and recharge system. ALMOST NO REFRIGERANT No cooling action. A lot of bubbles or something like mist appears in sight glass. SUCTION PRESSURE: much below normal DISCHARGE PRESSURE: much below normal Serious refrigerant leak. Stop compressor immediately. 1. Leak test. 2. Discharge system. 3. Repair Leak(s). 4. Replace receiver/drier, if necessary. 5. Check oil level. 6. Evacuate and recharge system. FAULTY EXPANSION VALVE a) Slight cooling. Sweating or frosted expansion valve outlet. b) Insufficient cooling. Sweated suction line. c) No cooling. Sweating or frosted suction line. a) SUCTION PRESSURE: below normal DISCHARGE PRESSURE: below normal b) SUCTION PRESSURE: above normal DISCHARGE PRESSURE: above normal c) SUCTION PRESSURE: above normal DISCHARGE PRESSURE: below normal a)Expansion valve restricts refrigerant. Or, expansion valve is clogged. Or, expansion valve is inoperative. Or, valve stuck closed. Thermal bulb has lost charge. b)Expansion valve allows too much refrigerant through evaporator. Sensing bulb on suction line not well insulated or properly attached to line. c) Faulty expansion valve. a) Replace expansion valve. b) 1. Check valve for operation. If suction side does not show a pressure decrease, replace valve. 2. Check security and insulation on sensing bulb. c) 1. Discharge system. 2. Replace valve. 3. Evacuate and replace system. Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 104 July 29, 2002 CONDITION SERVICE PRESSURE GAUGE READING PROBABLE CAUSE CORRECTIVE ACTION AIR IN SYSTEM Insufficient cooling. Sight glass shows occasional bubbles. SUCTION PRESSURE: above normal DISCHARGE PRESSURE: above normal Air mixed with refrigerant in system. 1. Discharge system. 2. Replace receiver/drier. 3. Evacuate and charge system. MOISTURE IN SYSTEM After operation for a while, pressure on suction side may show vacuum pressure reading. During this condition, discharge air will be warm. As warning of this, reading shows approx. 6 psi oscillation. SUCTION PRESSURE: below normal DISCHARGE PRESSURE: above normal Drier is saturated with moisture. Moisture has frozen at expansion valve. Refrigerant flow is restricted. 1. Discharge system. 2. Replace receiver/ drier (twice if necessary). 3. Evacuate system completely. (Repeat 30 minute evacuating three times.) 4. Recharge system. FAULTY CONDENSER Insufficient cooling. Bubbles appear in sight glass of drier. Suction line is very hot. SUCTION PRESSURE: above normal DISCHARGE PRESSURE: above normal Condenser air or refrigerant flow is restricted. Check condenser for dirt accumulation or bent fins. Clean/ replace as necessary. Check for refrigerant overcharge. If pressure remains high in spite of all above actions taken, remove and inspect the condenser for possible oil clogging. HIGH PRESSURE LINE BLOCKED Insufficient cooling. Frosted high pressure liquid line. SUCTION PRESSURE: much below normal DISCHARGE PRESSURE: much above normal Drier clogged, or restriction in high pressure line. 1. Discharge system. 2. Replace receiver/drier. 3. Evacuate and charge system Products, Inc. Maintenance Manual with Illustrated Parts Catalog CR-172-15 21-50-00 Page 105 July 29, 2002 CONDITION SERVICE PRESSURE GAUGE READING PROBABLE CAUSE CORRECTIVE ACTION FAULTY COMPRESSOR a) Insufficient cooling. b) Insufficient cooling. c) Rough running. a) SUCTION PRESSURE: much below normal DISCHARGE PRESSURE: much below normal b) SUCTION PRESSURE: much above normal DISCHARGE PRESSURE: much below normal a) Internal problem in compressor, or damaged gasket and valve. b) Internal problem with compressor body. c) Internal problem with compressor body. 1. Discharge system. 2. Remove and check compressor. 3. Repair or replace compressor. 4. Check oil level. 5. Replace receiver/ drier. 6. Evacuate and charge system. TOO MUCH OIL IN SYSTEM (Excessive) Insufficient cooling. SUCTION PRESSURE: above normal DISCHARGE PRESSURE: above normal Too much oil circulates with refrigerant, causing the cooling capacity of the system to be reduced. Refer to Oil Level Check for correcting oil level. WATER BEING BLOWN OUT OF EVAPORATOR SUCTION PRESSURE: normal DISCHARGE PRESSURE: normal Blocked evaporator drain. Check evaporator drain for downhill routing and repair any kinks or blockage in drain tubing. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 201 July 29, 2002 AIR-CONDITIONING SYSTEM MAINTENANCE PROCEDURES A. General The following procedures are used to perform typical maintenance on the air- conditioning system plumbing. Procedures are provided for making connections to components, and replacing the expansion valve. Keith Products air- conditioning systems use swaged hose fittings with "o-ring" type connections. B. Tools and Equipment Designation Ref. No. Qty Remarks Polyolester Oil Comm. Avail. A/R Viscosity ISO 68 Sealant ES49000-1 A/R None C. Connection to Components - O-Ring Replacement 1. Place the appropriate o-ring over the tube "O" end of the fitting. 2. Lubricate o-ring with polyolester oil viscosity ISO 68 or ES49000-1 sealant prior to assembly. 3. Apply sealant to all fitting-mating surfaces prior to assembly. D. Expansion Valve Removal and Installation The following procedure is used to remove or install the air-conditioning system expansion valve, located on the inlet side of the evaporator coil. 1. Discharge system in accordance with instructions included in this manual. 2. Disconnect and cap the liquid hose from the expansion valve inlet. 3. Remove the insulation covering the thermal sense bulb on the suction tubing. 4. Cut the tie wraps binding the sense bulb to the suction tubing. 5. Disconnect the fitting that connects the expansion valve to the coil, and remove the expansion valve. 6. Discard the old expansion valve and o-ring. 7. Install new ES26104-1 expansion valve and ES49011–2 o-ring. 8. Lubricate o-ring with polyolester oil viscosity grade ISO 68 or apply ES49000-1 sealant to fitting mating surfaces prior to assembly. 9. Install the thermal sense bulb such that it makes contact with the suction tube along its entire length with two or more cable ties as shown in Figure 3. 10. Insulate the bulb thoroughly with insulation to suction tubing. NOTE: Always utilize two wrenches as not to twist or bend the soft copper lines. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 202 July 29, 2002 Figure 3 Correct expansion valve and sense bulb orientation Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 301 July 29, 2002 AIR-CONDITIONING SYSTEM SYSTEM SERVICING 1. GENERAL The air-conditioning system uses refrigerant R134a and the compressor lubricating oil used is Polyolester Oil viscosity grade (ISO) 68. No other refrigerant or compressor oil should be used. Refrigerant R134a is non-explosive, non-flammable, non-corrosive, has practically no odor, and is heavier than air. Although R134a is classified as a safe refrigerant, certain precautions must be observed to personnel and property when working with R134a refrigerant. WARNING: A. Liquid R134a, at normal atmospheric pressure and temperature, evaporates so quickly that it tends to freeze anything that it contacts. Care must be taken to prevent any liquid refrigerant from coming into contact with skin. B. Always wear safety goggles when servicing any part of the refrigerant system to prevent refrigerant from coming into contact with the eyes. C. The refrigerant containers and the air-conditioning components are under pressure. Do not expose the air-conditioning system or refrigerant containers to heat. Do not puncture the air-conditioning components or the refrigerant containers. CAUTION: Do not operate air-conditioning system with condenser air outlet blocked. 2. DISCHARGING SYSTEM A. General The air-conditioning system refrigerant must be discharged prior to disconnecting or removing any components in the refrigerant loop. Federal law prohibits discharging refrigerant into the atmosphere. Use only an R134a compatible recycling/recovery unit when discharging the air-conditioning system. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 302 July 29, 2002 B. Tools and Equipment Designation Ref. No. Qty Remarks R134a Compatible Recycling/Recovery Unit Comm. Avail. 1 None C. Discharging Procedure 1) Connect R134a compatible recycling/recovery unit to the R134a service valves located near the evaporator installation on the right hand side of the aircraft. 2) Empty the recycling/recovery unit of oil. 3) Discharge the air-conditioning system in accordance with the recovery unit's instructions. 4) Empty the oil from the recycling/recovery unit. Note the amount of oil removed during the system discharge. This amount of oil must be added to the air-conditioning system prior to charging. Only use polyolester oil viscosity grade ISO 68. 3. EVACUATING SYSTEM A. General The air-conditioning system must be evacuated prior to charging the system with refrigerant. Evacuating the system removes any moisture and air that may be in the system. Use only an R134a compatible recycling/recovery unit when evacuating the air-conditioning system. B. Tools and Equipment Designation Ref. No. Qty Remarks R134a Compatible Recycling/Recovery Unit Comm. Avail. 1 None Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 303 July 29, 2002 C. Evacuating Procedure 1) Connect R134a compatible recycling/recovery unit to the R134a service valves on the aircraft's air-conditioning system. 2) Empty the oil from the recycling/recovery unit. 3) Evacuate the air-conditioning system in accordance with the recovery unit's instructions for a minimum of 15 minutes. 4) Empty the oil from the recycling/recovery unit. Note the amount of oil removed during the vacuum. This amount of oil must be added to the air- conditioning system prior to charging. Only use polyolester oil viscosity grade ISO 68. 5) Once the air-conditioning system has been evacuated, it is then ready for charging with new/recycled R134a refrigerant. 4. CHARGING SYSTEM A. General Use only R134a refrigerant when charging air-conditioning system. Federal law prohibits discharging refrigerant into the atmosphere. Use only R134a compatible recycling/recovery unit when charging the air-conditioning system. B. Tools and Equipment Designation Ref. No. Qty Remarks R134a Compatible Recycling/Recovery Unit Comm. Avail. 1 None R134a refrigerant Comm. Avail 2.5 lbs. None Polyolester Oil Comm. Avail 5 fl. oz. Viscosity ISO 68 C. Charging Procedure 1) Connect R134a compatible recycling/recovery unit to the R134a service valves on the aircraft's air-conditioning system. If recovery unit does not have pressure gauges, connect service pressure gauges to air-conditioning system. 2) Evacuate the air-conditioning system for 15 minutes in accordance with the instructions in this report. 3) Close the low side and open the high side on the recycling/recovery unit. 4) Add polyolester oil viscosity ISO 68 to the high side service tee using the refrigerant recycling/recovery unit while the system is under a vacuum. NOTE: Adding refrigerant or oil from the recycling/recovery unit directly to the low-pressure service tee will allow liquid refrigerant or oil to enter the compressor. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 304 July 29, 2002 The compressor is only designed to compress gas refrigerant, and liquid refrigerant or oil may damage/destroy the compressor. Always close the low side of the recycling/recovery unit during charging. 5) Charge the air-conditioning system in accordance with the recovery unit's instructions except as noted. 6) If bubbles are present at the sight glass after the system has been running for a minimum of 5 minutes, add refrigerant as necessary. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 601 July 29, 2002 AIR-CONDITIONING SYSTEM INSPECTION/CHECKS 1. GENERAL General service procedures are provided to keep the air-conditioning system operating at peak efficiency. Procedures are provided for inspection intervals, refrigerant charge inspection, refrigerant leak inspection, and compressor oil level inspection. CAUTION: Do not operate air-conditioning system with condenser air outlet blocked. A. Tools and Equipment Designation Ref. No. Qty Remarks Service Pressure Gage Comm. Avail. 1 None Electronic Leak Detector Comm. Avail. A/R Type H-10G Polyolester Oil Comm. Avail. A/R Viscosity ISO 68 2. INSPECTION INTERVALS A. General Periodic inspections of the air-conditioning system will keep the system operating at peak efficiency. The inspections are simple visual inspections requiring a minimal amount of time. B. Inspection Intervals *Or every annual inspection, which ever comes first. ITEM INSPECT FOR INTERVAL ACTION AIR-CONDITIONING SYSTEM COMPONENTS DIRT, DAMAGE EVERY 600 HOURS* CLEAN OR REPLACE COMPONENTS AS NECESSARY COMPRESSOR BELT TENSION, WEAR WITHIN 5 HOURS OF INSTALLING A NEW BELT, THEN EVERY 600 HOURS* TENSION OR REPLACE AS NECESSARY SIGHT GLASS PROPER REFRIGERANT LEVEL WHEN PROBLEM IS SUSPECTED* DISCHARGE/CHARGE AS NECESSARY EVAPORATOR AND CONDENSER COILS DIRT EVERY 600 HOURS* CLEAN OR REPLACE AS NECESSARY Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 602 July 29, 2002 3. REFRIGERANT LEVEL INSPECTION To be performed when improper refrigerant charge is suspected. A. Select air-conditioning system switch to AIR COND position. B. Set the fan speed switch to the HI position. C. Run system for five (5) minutes minimum. D. Check that the receiver/drier inlet and outlet fitting temperatures are the same. If the outlet is considerably colder, the receiver/drier screen may be clogged and may need replacement. E. Check the sight glass for bubbles. No bubbles should be visible after 5 minutes of operation. NOTE: The refrigerant bubbles are more difficult to see at ambient temperatures below 65ºF. Always re-check refrigerant level when ambient temperature is above 65ºF for proper level. F. Add/Remove refrigerant as necessary. 4. REFRIGERANT SYSTEM LEAKAGE INSPECTION To be performed when refrigerant leak is suspected. A. The system leakage check is to be performed in an area with an ambient temperature of 65ºF or above. B. Install service pressure gage to low and high pressure R134a service valves. C. On systems that have not been operated for 2 weeks or longer, operate the system for a minimum of 15 minutes. This will lubricate the compressor shaft seal and ensure a more accurate leakage check of the shaft seal. D. With the system off, and using a type H-10G electronic leak detector or equivalent, check all connections, compressor shaft seal, and fabricated components for leakage. No leakage is acceptable. 5. COMPRESSOR OIL LEVEL CHECK NOTE: It is not necessary to check the compressor oil level during routine maintenance. It only needs to be checked when a system component is replaced or when incorrect oil level is suspected. Only polyolester oil viscosity grade ISO 68 should be used. 1. Operate air-conditioning system for 10 minutes. This will collect as much oil as possible in the compressor. 2. Discharge air-conditioning system in accordance with the discharging instructions in this manual. 3. Remove either discharge or suction port hose fitting. 4. Remove oil drain plug and allow all oil to drain. 5. Add 5 ounces of oil to the compressor. 6. Clean oil drain area and install drain plug. Torque to 6 - 9 ft-lbs. 7. Install hose fitting. Products, Inc. CR-172-15 System Service Manual 21-50-00 Page 603 July 29, 2002 8. Charge air-conditioning system in accordance with the charging instructions in this manual. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 1 July 29, 2002 ELECTRICAL DESCRIPTION AND OPERATION 1. GENERAL The electrical system of the Cessna 172 air-conditioning system operates from the main 28 VDC buss. The major components of the electrical system are: Evaporator Blower: Blows cold air into the cabin. Condenser Blower: Removes heat from the refrigerant Compressor Clutch: Engages/disengages the compressor 2. SAFETY FEATURES During certain flight configurations the compressor clutch and condenser blower are disabled to supply electrical power to more critical systems. Depending on the aircraft model and type, automatic load shedding removes power to the compressor clutch and condenser blower when high load systems are engaged. The evaporator blower will remain available to re-circulate cockpit air during all flight configurations. Before electrical current reaches the compressor clutch it passes through the JBS2020- 5 Pressure Switch and the JBS60-2 Freeze Switch. In the event of excessive refrigerant pressure during flight (caused by failed or blocked condenser blower) or inadequate refrigerant pressure (caused by a leak in the plumbing) the JBS2020-5 pressure switch will open and disable the compressor clutch. In the event of extremely low temperature air exiting the evaporator (which may cause the coil to freeze) the JBS60-2 Freeze Switch will open and disable the compressor clutch. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 2 Oct 14, 2009 GENERAL ELECTRIC LAYOUT Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 101 July 29, 2002 ELECTRICAL TROUBLESHOOTING 1. GENERAL The following procedures are used for troubleshooting the electrical system and the electrical interface with the other assemblies of the air-conditioning system. The procedures systematically check every reasonable cause of the failure, starting from the power source that might result in the in operation of the evaporator blower, condenser blower, and compressor clutch. If the problem causing the component to fail is suspected, the suspected cause should be checked first. The sequence of checks may be varied to increase the convenience of the checker as desired. A. TOOLS AND EQUIPMENT DESIGNATION REF. NO. QTY. REMARKS Service pressure gauge Comm. Avail 1 None Multi-meter Comm. Avail 1 None 28 VDC source A/R None 2. Evaporator Blower Doesn’t Operate ‰ With the engine inoperative turn on the battery power ‰ Turn the AIR COND/OFF/FAN switch to FAN. ‰ Set the fan speed to high. ‰ Disconnect the ES53026-1 Electrical Connector from the blower. ‰ Check for power at pin 3. Terminal should have a voltage reading between 26.0V and 29.0V. Use a suitable aircraft ground when checking the power. ‰ If correct power is present at Pin 3, and Pin 4 (when selected to low), and ground is present at Pin 5, the problem lies with the evaporator/blower assembly. ‰ If power is not present at pin 3 and Pin 4, the problem is due to a failed electrical component, a broken electrical connection, or a broken wire on the power side of the connector. 1. Check the 30 Amp fuse, located in the J box (if applicable) for continuity. Replace as necessary 2. Check for power at the Circuit breaker. If power is not present, check the KAC-MBA-10 wire for continuity. Replace/repair as necessary. 3. Check the 20 Amp Circuit Breaker for continuity between the two wire terminals. Check the wire terminals for good connections to the wires. Replace/repair as necessary. ES53026-1 ELECTRICAL CONNECTOR Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 102 July 29, 2002 4. Check for power at the AIR COND/OFF/FAN Switch. If power is not present, check the KAC-MBB-16 wire for continuity. Replace/repair as necessary. 5. Check the operation of the AIR COND/OFF/FAN Switch. Check the wire terminals for good connections. Replace/repair as necessary. 6. Check for power at the Fan Speed Switch. If power is not present, replace/repair the connecting wire as necessary. 7. If power is present at the Fan Speed Switch and not at pin 3 or 4 (depending on switch positioning) of the evaporator blower connector, check the KAC-EFB-16 or KAC-EFA-16 wire for continuity. Replace/repair as necessary. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 103 July 29, 2002 3. Condenser Blower Doesn’t Operate ‰ With the engine inoperative turn on the battery power. ‰ Turn the AIR COND/OFF/FAN switch to AIR COND. ‰ Turn the landing light and pitot heat off. ‰ Check for power between the terminals of the EMI filter on the Condenser Blower Assembly. ‰ If the voltage measured at the EMI filter terminals is between 24.0-29.0 VDC and the blower is not operating, the blower needs to be returned for replacement/repair. ‰ If no voltage is measured at the EMI filter terminals, the problem is due to a failed electrical component, a broken electrical connection, or a broken wire. 1. Check the 30 Amp fuse for continuity in J box. Replace as necessary 2. Check for power at the Circuit breaker. If power is not present, check the KAC-MBA-10 wire for continuity. Replace/repair as necessary. 3. Check the 20 Amp Circuit Breaker for continuity between the two wire terminals. Check the wire terminals for good connections to the wires. Replace/repair as necessary. 4. Check for power at the ES56052-1 Relay, located in the pedestal. If power is not present, Check the KAC-LSB-16 wire for continuity. Replace/repair as necessary. 5. Check the terminals of the ES56052-1 Relay. If there is no continuity between the KAC-LSB-16 and KAC-LSA-16 (NC and COM) wires, check for power at the relay terminal that connects to wires KAC- LSE-16, and KAC-LSD-16. There should be no power at this terminal. If there is no power, check the relay for correct wiring and replace if necessary. 6. Check for power at the AIR COND/OFF/FAN Switch. If power is not present, check the KAC-LSA-16 wire for continuity. Replace/repair as necessary. 7. Check the operation of the AIR COND/OFF/FAN Switch. Check the wire terminals for good connections. Replace/repair as necessary. 8. Check for continuity from the AIR COND/OFF/FAN Switch to the positive terminal of the EMI filter. Repair/replace as necessary. 9. Check for continuity from the Negative terminal of the EMI filter to ground. Repair/replace as necessary. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 104 July 29, 2002 Condenser Electrical Schematic Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 105 July 29, 2002 4. Compressor Clutch Doesn’t Engage NOTE: If the ambient temperature is less than 45ºF the freeze switch may disable the compressor clutch. In order to troubleshoot an inoperative compressor clutch at ambient temperatures below 45ºF, use a short wire as a jumper between Pin 1 and Pin 2 of the ES53025-1 Electrical Connector on the evaporator assembly. This will bypass the temperature probes. NOTE: The clutch will not engage with out a system charge. ‰ With the engine inoperative turn on the battery power. ‰ Turn the AIR COND/OFF/FAN switch to AIR COND. ‰ Turn the landing light and pitot heat off. ‰ Check the voltage at the positive terminal of the compressor clutch. ‰ If the voltage measured at the positive terminal of the compressor clutch is between 24.0-29.0 VDC, and the clutch does not engage, (it can be rotated without the compressor pulley rotating) the clutch and coil need to be returned for replacement/repair. ‰ If no voltage is measured at the positive terminal of the compressor clutch, the problem is due to a failed electrical component, a broken electrical connection, a broken wire, or low temperature measured by the temperature probes. 1. Check the 30 Amp fuse (at J box) for continuity. Replace as necessary 2. Check for power at the Circuit breaker. If power is not present, check the KAC-MBA-10 wire for continuity. Replace/repair as necessary. 3. Check the 20 Amp Circuit Breaker for continuity between the two wire terminals. Check the wire terminals for good connections to the wires. Replace/repair as necessary. 4. Check for power at the ES56052-1 Relay. If power is not present, Check the KAC-LSB-16 wire for continuity. Replace/repair as necessary. 5. Check the terminals of the ES56052-1 Relay. If there is no continuity between the KAC-LSB-16 and KAC-LSA-16 (NC and COM) wires, check for power at the relay terminal that connects to wires KAC- LSE-16 and KAC-LSD-16. There should be no power at this terminal. If there is no power, and NC to COM is an open circuit, check the relay for correct wiring and replace if necessary. 6. Check for power at the AIR COND/OFF/FAN Switch. If power is not present, check the KAC-LSA-16 wire for continuity. Replace/repair as necessary. 7. Check the operation of the AIR COND/OFF/FAN Switch. Check the wire terminals for good connections. Replace/repair as necessary. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 106 July 29, 2002 8. Check for power at the JBS2020-5 Pressure Switch. If power is not present, check the KAC-CCB-16 wire for continuity. Replace/repair as necessary. 9. Check for continuity of the pressure switch. If there is no continuity at the pressure switch, check the refrigerant pressure. If the discharge pressure is between 35 and 340 PSIG, discharge the air-conditioning system and replace the JBS2020-5 Pressure Switch. If the pressure is less than 35 PSIG or greater than 340 PSIG add/remove refrigerant to the proper level. 10. Check for power at the Freeze Switch (Pin 2) on the evaporator assembly. If power is not present, check the KAC-CCA-16 wire for continuity. Replace/repair as necessary. 11. Check for continuity between Pin 1 and Pin 2. If there is no continuity between Pin 1 and Pin 2, and the ambient air temperature is greater than 45ºF, replace the Freeze Switch. 12. Check for power at pin 1, If there id power at pin 1, but not at compressor, repair/replace the KAC-CCC-16 wire. Products, Inc. CR-172-15 System Service Manual 21-50-01 Page 107 July 29, 2002 Compressor Clutch Electrical Schematic Products, Inc. CR-172-15 System Service Manual 21-50-02 Page 1 July 29, 2002 PLUMBING DESCRIPTION AND OPERATION 1. GENERAL The plumbing system consists of flexible nylon lined refrigerant hose with permanent swaged on fittings. All connections are tube o-ring type with sealant on the fitting mating surfaces to ensure leak-free operation. Hose, o-ring material, and sealants are specially designed to work with refrigerant R134a and polyolester oil viscosity grade ISO 68. Two service valves are located on the right side of the aircraft near the evaporator installation. They are sized differently to avoid incorrect connection when servicing the system. A receiver/drier bottle is located downstream of the condenser to remove moisture from the liquid refrigerant. The receiver/drier bottle is mounted in the tailcone of the aircraft. A binary pressure switch monitors the refrigerant gas pressure. This switch will open at a compressor discharge over-pressure of 384 ±29 psi and under-pressure conditions of 30±5 psi. This will interrupt the power to the compressor clutch and stop the compressor. The second overpressure safety device is a fuse plug, which will vent the system refrigerant in the event of a system pressure in excess of 425 PSIG. The R134a gas would then be sucked into the condenser blower and forced out the exhaust duct on the right side of the aircraft. It is located on the receiver/drier. This section of the maintenance manual discusses maintenance practices used for the plumbing portion of the air-conditioning system. Refer to 172-0800 for parts list and schematics. Products, Inc. CR-172-15 System Service Manual 21-50-02 Page 201 July 29, 2002 PLUMBING MAINTENANCE PRACTICES 1.0 GENERAL The following procedures are used to perform typical maintenance on the air- conditioning system plumbing. CAUTION: Do not operate air-conditioning system with condenser air inlet or outlet blocked. A. Connection to components, o-ring replacement: 1. Place the appropriate o-ring (reference 172-0800 drawing) over the tube “O” end of the fitting. 2. Lubricate o-ring with polyolester oil or ES49000-1 sealant prior to assembly. 3. Apply sealant to all fitting-mating surfaces prior to assembly. 4. “Dry” torque recommendations for all fittings are as follows: Liquid hoses 11-13 ft/lbs Discharge hoses 15-20 ft/lbs Suction hoses 21-27 ft/lbs It is recommended to torque to the low side of the torque range to prevent fitting twisting or damage. B. Receiver/drier bottle replacement: 1. Replace receiver/drier bottle whenever the compressor is replaced or when the air-conditioning system plumbing is left open to the atmosphere for a period of time greater than one half (1/2) hour. Products, Inc. CR-172-15 System Service Manual 21-50-03 Page 1 July 29, 2002 COMPRESSOR DESCRIPTION AND OPERATION 1. GENERAL The compressor is mounted on brackets in the engine compartment and is driven by a belt running to the starter ring-gear pulley. The compressor compresses the refrigerant gas for condensing at ambient temperatures and pumps the refrigerant through the system. The compressor clutch is powered by 28 VDC. This section of the maintenance manual discusses maintenance practices used for the compressor assembly portion of the air-conditioning system. COMPRESSOR INSTALLATION Products, Inc. CR-172-15 System Service Manual 21-50-03 Page 201 July 29, 2002 COMPRESSOR MAINTENANCE PRACTICES 1. GENERAL The following procedures are used to perform typical maintenance on the compressor assembly. 2. TOOLS AND EQUIPMENT DESIGNATION REF. NO. QTY. REMARKS Polyolester oil Comm Avail A/R Viscosity ISO 68 3. COMPRESSOR ASSEMBLY MAINTENANCE PROCEDURES A. Compressor drive belt adjustment: 1. Adjust belt for moderate tension and then rotate large pulley through 2 revolutions. 2. Tension belt to deflect 0.25 inch with a 10 lb. force applied at mid- span location. The belt should deflect .5 inches with a 22 lb force applied at the mid-span location. 3. Rotate belt 5 revolutions. Re-tension as required. 4. Cessna alternator belt adjustment procedures should always take precedence over any recommendations here within. B. Compressor oil level check: NOTE: It is not necessary to check the compressor oil level at any time during routine maintenance as long as servicing instructions are properly followed. The compressor comes equipped with 5 oz. of polyolester oil viscosity grade ISO 68. If the amount of oil removed during system discharging and vacuuming is always added before charging, oil never needs to be added to the compressor. Products, Inc. CR-172-15 System Service Manual 21-50-04 Page 1 July 29, 2002 CONDENSER DESCRIPTION AND OPERATION 1. GENERAL The condenser assembly is located in the tailcone and is attached to support structure mounted to frames in the aircraft. The assembly consists of a condenser coil unit and shroud with associated brackets. The condenser converts the refrigerant from a gas to a liquid. The receiver/drier bottle removes moisture from the refrigerant. The condenser fan draws in cool (ambient) air from the intake duct on the left side of the aircraft and blows this air through the condenser coil where the refrigerant gas can be condensed to a liquid. The air is then exhausted overboard through the exhaust duct on the right side of the tailcone. This section of the maintenance manual discusses maintenance practices used for the condenser assembly portion of the air-conditioning system. Products, Inc. CR-172-15 System Service Manual 21-50-04 Page 201 July 29, 2002 CONDENSER MAINTENANCE PRACTICES 1. GENERAL The following procedures are used to perform typical maintenance on the condenser assembly. 2. TOOLS AND EQUIPMENT DESIGNATION REF. NO. QTY. REMARKS Vacuum Cleaner Comm Avail 1 None Coil Cleaner Comm Avail A/R Non-acid based 3. CONDENSER ASSEMBLY MAINTENANCE PROCEDURES A. Condenser coil cleaning procedure: 1. Remove condenser coil from aircraft and use vacuum cleaner to remove large debris from upstream and downstream coil faces. 2. Spray coil cleaner on both coil faces. Wash off with water (ends capped if not installed). 3. Allow coil to dry thoroughly prior to additional maintenance. Products, Inc. CR-172-15 System Service Manual 21-50-05 Page 1 July 29, 2002 EVAPORATOR DESCRIPTION AND OPERATION 1. GENERAL The evaporator assemblies are mounted aft of the cabin on the right side of the aircraft. The evaporator assemblies are made up of an evaporator coil, and blower. Cabin air is pulled through the evaporator coil, cooled and then distributed back to the cabin. This section of the maintenance manual discusses maintenance practices used for the evaporator assembly portion of the air-conditioning system. Products, Inc. CR-172-15 System Service Manual 21-50-05 Page 201 July 29, 2002 EVAPORATOR MAINTENANCE PRACTICES 4. GENERAL The following procedures are used to perform typical maintenance on the evaporator assembly. 5. TOOLS AND EQUIPMENT DESIGNATION REF. NO. QTY. REMARKS Vacuum Cleaner Comm Avail 1 None Coil Cleaner Comm Avail A/R Non-acid based 6. EVAPORATOR ASSEMBLY MAINTENANCE PROCEDURES B. Evaporator coil cleaning procedure: 1. Remove evaporator coil from aircraft and use vacuum cleaner to remove large debris from upstream and downstream coil faces. 2. Spray coil cleaner on both coil faces. Wash off with water (ends capped if not installed). 3. Allow coil to dry thoroughly prior to additional maintenance Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 1 July 29, 2002 ILLUSTRATED PARTS CATALOG Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 101 October 14, 2009 172-0200-1 Evaporator Installation (172-0250-1 Configuration) Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 102 October 14, 2009 172-0200-1 Evaporator Installation (172-0251-1 Configuration) Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 103 October 14, 2009 TEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0200-1 Evaporator Installation 2 172-0250-1 172-0251-1 Evaporator Assy. (Alternate Spare 172-0251-1) Evaporator Assy. (Alternate Spare 172-0250-1) 3 JBS862-6 Blower Assembly 1 4 ES73088-10 Blower Wheel 1 5 JBS276-1 ES61060-2 ES61027-10 Motor (Use Spare ES61060-2) Motor (For 172-0250-1 Only) Motor (For 172-0251-1 Only) 1 6 172-1250-1 172-1251-1 Bracket (For 172-0250-1 Only) Bracket (For 172-0251-1 Only) 1 7 JBS60-2 Thermostat 1 8 ES26104-1 Expansion Valve 1 9 ES49011-2 O-Ring 1 10 ES53025-1 Receptacle 1 11 ES53027-2 Pin 5 12 172-0252-1 Evaporator Coil Assembly 1 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 201 July 29, 2002 172-0400-1 Compressor Installation Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 202 July 29, 2002 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0400-1 Compressor Installation 2 JBS4172-1 Compressor Assembly Modification 1 3 ES20172-1 Belt 1 4 172-1400-1 Support Assembly 1 5 172-1400-9 Bracket 1 6 172-1400-6 Spacer 1 7 MS20995C32 Safety Wire A/R Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 301 July 29, 2002 172-0300-1 Condenser Installation 172-0300-2 Condenser Installation Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 302 July 29, 2002 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0300-1,-2 Condenser Installation 2 172-1300-1 Condenser Assembly (-1 only) 1 3 172-1300-3 Fan Assembly 1 4 ES30042-10 Clamp 2 5 ES70009-7 Flex Duct (in.) 15 6 172-1300-7 Condenser Assembly (-2 only) 1 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 401 October 14, 2009 172-0700-1 Electrical Installation Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 402 July 29, 2002 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 403 March 14, 2007 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0700-1 Electrical Installation 2 ES57016-5 Switch 1 3 ES57016-6 Switch 1 4 MS25041-10 Light Indicator 1 5 ES50162-1 Lamp 1 6 ES51000-1 Circuit Breaker (20A) 1 7 ES51172-1 Fuse (30A) 1 8 ES55079-1 Splice, Knife Disconnect 3 9 ES53026-1 Plug 1 10 ES53028-2 Socket 5 11 ES58161-15 Diode 3 12 ES56052-1 Relay 1 13 JBS64-13 Fuse (30A) 1 14 JBS7002-3 Panel, Switch 1 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 501 Dec 11, 2007 172-0800-1 Plumbing Installation Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 502 Dec 11, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 503 Dec 11, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 504 Dec 11, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 505 Dec 11, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 506 Dec 11, 2007 down nose a t f o k e nose up f Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 507 Dec 11, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 508 Dec 11, 2007 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0800-1 Plumbing Installation 2 ES48149-1 Hose (IN) 80 3 ES48149-2 Hose (IN) 406 4 ES48149-3 Hose (IN) 262 5 ES02126-1 Fire Sleeve (IN) 65 6 ES02126-2 Fire Sleeve (IN) 65 7 ES06022-1 Insulation Tape (IN) 720 8 AN6289-10D Nut 1 9 ES30015-6 Cable tie 20 10 ES49011-3 O-Ring 4 11 ES49011-2 O-Ring 5 12 ES49011-1 O-Ring 4 13 JBS2020-5 Pressure Switch Assembly 1 14 ES43030-2 Receiver Dryer 1 15 JBS6009-9 Fitting, Bulkhead O-Ring 1 16 JBS6009-3 Fitting, Bulkhead O-Ring 1 17 172-1800-2 Doubler 1 18 ES31101DS4-2 Rivet 10 19 AN6289-8D Nut 1 20 ES40158-2 Splicer, Beadlock 1 21 ES40158-3 Splicer, Beadlock 1 22 ES49000-1 Sealant 1 23 MS21919WDG16 Hose Clamp 2 24 MS21919WDG11 Hose Clamp 8 25 AN525-10R8 Screw 1 26 NAS43DD3-13 Spacer 1 27 ES40150-2 Fitting 2 28 ES40150-3 Fitting 2 29 ES40159-1 Fitting 1 30 ES40159-2 Fitting 1 31 AN960-4L Washer 1 32 ES30072-1 Band-It Clamp 4 33 ES40149-2 Fitting 1 34 ES40151-1 Fitting 3 35 JBS10-64 Placard 4 36 ES40150-1 Fitting 1 37 MS21919WDG14 Hose Clamp 5 38 NAS43DD3-25 Spacer 1 39 ES30013-2 Tie Block 1 40 MS9592-005 Bracket 2 41 MS20365-1032 Nut 9 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 509 Dec 11, 2007 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 42 ES40151-2 Fitting 1 43 MS21044N08 Nut 2 44 AN960-10 Washer 9 45 AN960-8 Washer 2 46 AN525-10R14 Screw 1 47 AN525-10R12 Screw 1 48 AN525-10R7 Screw 5 49 206-1357-8 Bracket 1 50 ES30042-6 Clamp, Aero-Seal 1 51 AN525-832R6 Screw 2 52 MS21919WDG12 Clamp 1 53 MS21919WDG20 Clamp 1 54 AN525-10R10 Screw 4 55 MS21266-1N Grommet Strip (IN) 12 56 ES30013-1 Tie Block 1 57 ES40151-3 Fitting 1 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 601 March 14, 2007 172-0600-1 Cabin Air Duct Installation Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 602 March 14, 2007 down nose a t f o k e nose up f Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 603 March 14, 2007 Products, Inc. CR-172-15 System Service Manual 21-50-06 Page 604 March 14, 2007 ITEM PART NUMBER NOMENCLATURE UNITS PER ASSEMBLY 1 172-0600-1 Cabin Air Ducting Installation 2 172-0650-1 Air Outlet Assembly 1 3 172-0650-2 Duct Assembly 1 4 172-0650-3 Center Duct Assembly 1 5 172-0650-4 AFT Duct Assembly 1 6 ES30015-1 Cable Tie 8 7 ES70009-4 Flex Duct (IN) 60 8 MS3367-2-0 Cable Tie 2 9 ES70009-2 Flex Duct (IN) 6 10 AN525-832R12 Screw 18 11 AN525-10R10 Screw 4 12 AN525-10R6 Screw 4 13 AN525-832R8 Screw 2 14 MS21266-1N Grommet, Plastic Edge (IN) 6 15 AN525-832R10 Screw 8