Component Maintenance Manual RECORD OF REVISIONS DESCRIPTION OF CHANGE DATE APPROVAL ORIGINAL RELEASE 12/28/07 Updated Storage, Section 14. Updated information concerning 5/5/08 cold weather operations under General and System Off Season/On Aircraft Functional Testing. Delete page 2002 Subtask 21-00-22-99-002 9/19/08 This removes wiring diagram Figure 3, and removes 4.2 “Wiring Schematic”and4.2.1 "The following electrical schematic shows the system components and how they interrelate to each other."...
Component Maintenance Manual RECORD OF TEMPORARY REVISIONS DESCRIPTION OF CHANGE DATE APPROVAL EFFECTIVITY: ALL 21-00-22 Record of Temporary Revisions Page 2 JULY 21, 2011...
Component Maintenance Manual LIST OF SERVICE BULLETINS SERVICE DESCRIPTION DATE BULLETIN # RELEASED EFFECTIVITY: ALL 21-00-22 List of Service Bulletins Page 3 JULY 21, 2011...
Component Maintenance Manual LIST OF EFFECTIVE PAGES CHAPTER / SECTION PAGE DATE CHAPTER / SECTION PAGE DATE 12/28/07 5/5/08 9/19/08 07/21/11 EFFECTIVITY: ALL 21-00-22 List of Effective Pages Page 4 JULY 21, 2011...
Component Maintenance Manual TABLE OF CONTENTS RECORD OF REVISIONS...........................1 RECORD OF TEMPORARY REVISIONS......................2 LIST OF SERVICE BULLETINS .........................3 LIST OF EFFECTIVE PAGES..........................4 TABLE OF CONTENTS ............................5 LIST OF ILLUSTRATIONS ..........................7 LIST OF TABLES ..............................7 INTRODUCTION..............................8 MANUAL INTRODUCTION........................8 1.1 General introduction (How to Use): ....................8 1.2 Acronyms, Abbreviations, and Symbols:...................9 1.3 Standard Torque Values: ........................10 1.4 Documents Required:.........................10...
General introduction (How to Use): 1.1.1 This operating, servicing and component maintenance manual (OSCMM) covers the requirements for field servicing the R-12 air conditioning system for the Pilatus PC12 Aircraft. This document includes component descriptions, servicing, maintenance, inspection requirements and an illustrated parts list.
Component Maintenance Manual 1.1.6 A complete Illustrated Parts Listing (IPL) is supplied as additional documentation (Section 11) to provide service technicians access to exploded views and a parts list while performing maintenance, testing, disassembly and assembly procedures. Refer to the IPL for all figure and item numbers.
270-350 IN LBS CONNECTIONS Table 1 Standard Torque Values SUBTASK 21-00-22-99F-004 Documents Required: Illustrated Parts Listings (IPL) (included with this manual) Pilatus PC12 Aircraft Maintenance Manual SUBTASK 21-00-22-99F-005 Consumable Products: PART NUMBER DESCRIPTION REMARKS 11602 SEALANT RTV BLACK...
General: 2.1.1 The air conditioning system installed on the Pilatus PC12 Aircraft is not considered a primary flight system. However, an air conditioning system does perform the important function of providing passenger and flight crew comfort during aircraft movement on the ground and while in flight.
System Description and Operation: 2.2.1 The cabin cooling system installed in the Pilatus PC12 Aircraft operates using a closed vapor cycle concept using refrigerant R12 as the heat absorption media. The R12 air conditioning system cools the aircraft in a similar manner as systems found in an automobile or home.
Component Maintenance Manual SUBTASK 21-00-22-99F-008 System Component Description and Operation: 2.3.1 The R12 air conditioning system installed on the Pilatus PC12 Aircraft uses the following major system components: Compressor Condenser Module Assembly 1250900-4 Evaporator Module Assembly 1250200-42 (L) /-43 (C,R) 2.3.2...
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Component Maintenance Manual 2.3.3.3 CONDENSER COIL ASSEMBLY: The condenser coil assembly is a copper tube and aluminum fin configuration with 6061-T6 aluminum support brackets. The coil heat rejection is 26,000 BTUH based on a 117°F ambient day. Condenser cooling airflow and coil sizes are based on the design cooling capacity and compressor input horsepower.
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Component Maintenance Manual 2.3.5.2 BLOWER MOTOR: The blower motor (1250210-1) operates on 24 VDC with a current draw of 5 amps and has a design RPM of 5225. The blower motor is a four brush design with an integrated controller and was selected for its efficiency, excellent controllability, long life and low vibration at high speeds.
Component Maintenance Manual TESTING AND FAULT ISOLATION TASK 21-00-22-70-801 R12 AIR CONDITIONING SYSTEM COMPONENT – TESTING AND FAULT ISOLATION SUBTASK 21-00-22-99F-009 General: 3.1.1 Testing and Fault Isolation of the R12 Air Conditioning System may be necessary if the system does not operate and/or perform in accordance with information contained herein. Therefore it is necessary for the service personnel to diagnose the discrepancy by troubleshooting the system and its components.
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Component Maintenance Manual Verify that there is a distinct and noticeable change in sound of blower motor when changing from low to high speed positions. This indicates that the cockpit selector switch is functioning properly and that the blower motor is responding accordingly. ...
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Component Maintenance Manual 3.4.3.1 Remove, if required, all panels, doors, shrouds, etc, to gain access to system/component being leak checked (refer to aircraft maintenance manual). 3.4.3.2 Remove, if required, any enclosures or access doors to expose all tubing, hoses, fittings, etc. to the system components. 3.4.3.3 Verify all plumbing connections are tight.
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Component Maintenance Manual 3.4.3.12 Using a wire brush and cleaning solvent, completely remove old thread sealant. Apply a thin layer of thread sealant primer to fitting threads. CAUTION: WHEN APPLYING THREAD SEALANT, TAKE EXTREME CARE TO KEEP SEALANT OFF FIRST 2 OR 3 THREADS. 3.4.3.13 Apply Loctite thread sealant on all male fitting threads sparingly.
Component Maintenance Manual NOTE: Refer to Refrigerant Flow (Figure 2) INDICATION PROBABLE CAUSE POSSIBLE SOLUTION A. No System Power 1. Ground power not connected 1. Plug in ground power cart 2. Aircraft power switch off 2. Energize power switch 1. Air conditioner breaker off 1.
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Component Maintenance Manual INDICATION PROBABLE CAUSE POSSIBLE SOLUTION C. System Operates But Does 1. Low refrigerant charge 1.Charge as required Not Cool 2. Overcharged system cutout 2. Reclaim refrigerant as required 3. Failed Compressor 3. Replace 4. Failed Drive Motor 4.
Component Maintenance Manual INDICATION PROBABLE CAUSE POSSIBLE SOLUTION 1. Circuit Breaker failed or off 1. Energize or replace G. Compressor Assembly Will Not Operate 2. Relay failed 2. Replace 3. Pressure switch failed 3. Replace 4. Drive motor failed 5. Replace 5.
Component Maintenance Manual SCHEMATIC AND WIRING DIAGRAMS 21-00-22-99-801 R12 AIR CONDITIONING SYSTEM SCHEMATIC AND WIRING DIAGRAMS SUBTASK 21-00-22-99-001 R12 Refrigerant Flow Schematic: 4.1.1 The following schematic shows an air conditioning system and its associated components as well as the flow of the R12 refrigerant. Figure 2 R12 Refrigerant Flow Schematic EFFECTIVITY: ALL 21-00-22...
Component Maintenance Manual DISASSEMBLY TASK 21-00-22-00-801 R12 AIR CONDITIONING SYSTEM COMPONENT - DISASSEMBLY SUBTASK 21-00-22-99F-010 General: WARNING: SERVICE TECHNICIANS ARE ADVISED TO OBSERVE STANDARD SAFETY PRECAUTIONS, SUCH AS WEARING PERSONAL SAFETY GEAR, TO PREVENT INJURY WHILE PERFORMING SERVICE TO THE UNIT. CAUTION: SERVICE TECHNICIANS MUST PREVENT CONTAMINATION OF INTERNAL SYSTEM PLUMBING DURING ANY SERVICING AND/OR MAINTENANCE OPERATION.
Component Maintenance Manual 5.1.7 Tools, fixtures, equipment, or consumable items required: Small hand tools and socket set Scribe or wire hook Volt or OHM meter (digital) Shop air, 40 PSIG max Respiration mask SUBTASK 21-00-22-00-001 Compressor Condenser Module Disassembly Procedures (refer to Figure 10001): 5.2.1...
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Component Maintenance Manual 5.2.3.2 Slightly loosen the upper compressor mounting bolts. 5.2.3.3 Loosen lower compressor rod end tensioning adjustment nut. 5.2.3.4 Loosen drive motor pulley set screws. 5.2.3.5 Slide lower compressor in towards drive motor, slide drive pulley and belt from motor shaft, while at the same time sliding the drive belt off the compressor pulley.
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Component Maintenance Manual 5.2.6 Removal of Fan 5.2.6.1 Remove motor shaft retaining nut and washer. 5.2.6.2 Loosen fan hub set screw. 5.2.6.3 Slide fan assembly and 2 washers from motor shaft. 5.2.7 Removal of Fan Shroud 5.2.7.1 Remove four shroud mounting screws, washers, and nuts. 5.2.7.2 Cut RTV between shroud and coil using a putty knife.
Component Maintenance Manual CLEANING TASK 21-00-22-10-801 R12 AIR CONDITIONING SYSTEM COMPONENT – CLEANING PROCEDURES SUBTASK 21-00-22-99F-011 General: 6.1.1 This section details the procedures required to perform certain cleaning functions. The components listed have certain cleaning procedures associated with them, however these procedures are in no way an all encompassing list of what may be required.
Component Maintenance Manual SUBTASK 21-00-22-10-001 Compressor Condenser Module Cleaning Procedures: 6.2.1 The following components of the Compressor Condenser Module will require periodic cleaning (refer to the Inspection Schedule in section 7 for time intervals). This is in no way an all encompassing list. If at any time during the inspection process a component is found to be dirty, use a soft cloth to remove all contaminants from external surfaces (refer to Figure 10001).
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Component Maintenance Manual Expansion Valve CAUTION: USE EXTREME CARE TO PREVENT DAMAGE OR BENDING OF COIL FINS 6.3.1.1 EVAPORATOR COIL AIR INLET: The coil fins will, over time, become clogged with dirt, dust and other foreign matter. It is essential that the coil fins remain clear for proper operation of the evaporator module assembly.
Component Maintenance Manual CHECK (INSPECTION SCHEDULE) TASK 21-00-22-21-801 R12 AIR CONDITIOING SYSTEM COMPONENT – INSPECTION SCHEDULE SUBTASK 21-00-22-21-001 Compressor Condenser Module Inspection Schedule: NOTE: This is the recommended visual inspection schedule for the Compressor Condenser Module Assembly. Adherence to this schedule will ensure that all components of the assembly are in accordance with the manufacturer’s specifications and is necessary to detect structural failure, deterioration or damage, and to determine the need for corrective action.
Component Maintenance Manual SUBTASK 21-00-38-21-002 Evaporator Module Inspection Schedule: NOTE: This is the recommended visual inspection schedule for the Evaporator Module Assembly. Adherence to this schedule will ensure that all components of the assembly are in accordance with the manufacturer’s specifications and is necessary to detect structural failure, deterioration or damage, and to determine the need for corrective action.
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Component Maintenance Manual REPAIRS TASK 21-00-22-30-801 R12 AIR CONDITIONING SYSTEM COMPONENT – REPAIR PROCEDURES SUBTASK 21-00-22-99F-012 General: 8.1.1 Refer to Illustrated Parts Listing (IPL) for figure/item numbers (Section 11). WARNING: SERVICE TECHNICIANS ARE ADVISED TO OBSERVE STANDARD SAFETY PRECAUTIONS, SUCH AS WEARING PERSONAL SAFETY GEAR, TO PREVENT INJURY WHILE PERFORMING SERVICE TO THE UNIT.
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Component Maintenance Manual 8.2.1.1 DRIVE BELT/COVER/PULLEYS: The drive belt and the associated pulleys will, over time, become worn or damaged, or may simply be out of alignment. It is essential that the drive belt and the pulleys are in excellent condition for proper operation of the Compressor Condenser Module assembly.
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Component Maintenance Manual 8.2.1.5 ELECTRICAL WIRING: The electrical wiring can, over time, become worn and damaged. If the wiring insulation is showing signs of abrasion or damage of any other kind, replace wiring as required 8.2.1.6 RECEIVER DRYER ASSEMBLY: The receiver dryer assembly can, over time, become damaged.
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(refer to aircraft maintenance manual). Contact Pilatus Aircraft Customer Service for replacement component. If Pilatus cannot support a replacement for the 1134200-42 (L) /-43 (C,R) evaporator, contact Enviro Systems for replacement. Replacement evaporator will be 1134200-60 (L)/-61(R)/-63 (C) and is not compatible with older evaporator 1134200-42/-43.
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Component Maintenance Manual 8.3.1.5 EXPANSION VALVE: The expansion valve can, over time, become damaged and/or not operate correctly. If the expansion valve shows signs of damage or does not function properly, remove and replace (refer to Disassembly, Section 5 and Assembly, Section 9).
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Component Maintenance Manual ASSEMBLY TASK 21-00-22-40-801 R12 AIR CONDITIONING SYSTEM COMPONENT - ASSEMBLY SUBTASK 21-00-22-99F-013 General: 9.1.1 Refer to Illustrated Parts Listing (IPL) during assembly procedures for figure/item numbers (Section 11). WARNING: SERVICE TECHNICIANS ARE ADVISED TO OBSERVE STANDARD SAFETY PRECAUTIONS, SUCH AS WEARING PERSONAL SAFETY GEAR, TO PREVENT INJURY WHILE PERFORMING SERVICE TO THE UNIT.
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Component Maintenance Manual Shop air, 40 PSIG max Micrometer Scribe or wire hook Inspection mirror Thermometer, 0-150°F Flash light or service lamp Leak check fluid (soapy) Thread sealant primer Thread sealant ...
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Component Maintenance Manual 9.2.2 Assembly of Fan / Outlet Shroud 9.2.2.1 After insuring that the shroud/coil mating surfaces have been cleaned in accordance with section 6, apply a 1/8 inch bead of RTV to fan/outlet shroud/coil mating surface. CAUTION: DO NOT TIGHTEN FAN SHROUD MOUNTING SCREWS UNTIL MOTOR AND FAN HAVE BEEN INSTALLED.
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Component Maintenance Manual 9.2.4.8 Tighten drive motor mounting bolts and torque (refer to table 1, Section 1.3 for torque specifications). 9.2.5 Assembly of Compressor 9.2.5.1 Position compressor in mounting bracket and install 3 mounting bolts. Finger tighten bolts only. 9.2.5.2 Rotate lower compressor towards drive motor by adjusting rod end adjustment bolts.
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Component Maintenance Manual 9.2.6.7 Secure drive pulley by tightening drive pulley set screws (refer to table 1, section 1.3 for torque specifications). 9.2.6.8 Tighten and secure compressor mounting bolts, washers, and lock nuts (refer to table 1, section 1.3 for torque specifications). 9.2.7 Assembly of Belt Cover 9.2.7.1...
Component Maintenance Manual Figure 7 Belt Tensioning Reference 9.2.9 Assembly of Power Relay 9.2.9.1 Carefully slide power relay into position and attach using mounting hardware. 9.2.9.2 Connect electrical connections and install boots for protection. 9.2.10 Assembly of Hour Meter 9.2.10.1 Carefully slide hour meter into hour meter opening and secure with attaching hardware (refer to table 1, Section 1.3 for torque specifications).
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Component Maintenance Manual SUBTASK 21-00-22-40-002 Evaporator Module Assembly Procedures (refer to Figure 10002): 9.3.1 Assembly of Expansion Valve CAUTION: APPLY THREAD SEALANT SPARINGLY TO MALE FITTING THREADS STAYING CLEAR OF FIRST 2-3 THREADS. 9.3.1.1 Set new valve adjustment screw to same position as failed valve. 9.3.1.2 Using a wire brush and cleaning solvent, completely remove old thread sealant.
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Component Maintenance Manual SPECIAL TOOLS, FIXTURES, AND EQUIPMENT TASK 21-00-22-99F-803 10.0 SPECIAL TOOLS/EQUIPMENT SUBTASK 21-00-22-99F-014 10.1 General: 10.1.1 This section describes the necessary tools and test equipment required to perform maintenance, functional testing, troubleshooting, and repair procedures. Equivalent test equipment may be substituted only if it meets the listed equipment specifications. ...
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Component Maintenance Manual Straight Edge Measuring Device Micrometer Scribe or Wire Hook Volt-OHM Meter Belt Tensioning Tool T1134610 Spring Scale Wagner FDK 10 EFFECTIVITY: ALL 21-00-22 Page 9002 JULY 21, 2011...
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Component Maintenance Manual ILLUSTRATED PARTS LIST TASK 21-00-22-98-801 11.0 R12 AIR CONDITIONING SYSTEM COMPONENT ILLUSTRATED PARTS LISTING SUBTASK 21-00-22-99F-015 11.1 Introduction: 11.1.1 This Illustrated Parts Listing (IPL) is intended for use during testing and isolation, disassembly, cleaning, check (inspection), repair, assembly, and issuing the replaceable equipment components as well as in identification of new and reclaimed parts.
Component Maintenance Manual SPECIAL PROCEDURES TASK 21-00-22-82-801 12.0 SPECIAL PRODECURES SUBTASK 21-00-22-82-001 12.1 Expansion Valve Alignment: 12.1.1 The expansion valve is set at the factory, but there may be times when it must be adjusted to assure proper refrigerant flow at the desired evaporating temperature; for example, excessive pressure drop for long suction line runs.
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Component Maintenance Manual 12.1.4 Gain access to the Evaporator Coil Assembly (refer to the aircraft maintenance manual for removal of access panels and other hardware that might need to be removed) 12.1.5 Remove all shrouds, covers or enclosures which prevent access to the evaporator expansion valve adjustment knob.
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Component Maintenance Manual 12.2.5 Allow system to stabilize, recheck the evaporator outlet temperatures and repeat adjustment procedure if required. Evaporator outlet temperatures should be within 1-3° of each other. NOTE: Proper evaporator balancing should not result in a change of the compressor suction pressure. Verify system pressures are typical values as shown in table 5.
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Component Maintenance Manual CAUTION: CAREFULLY LAY BRUSH SHUNT LEADS IN A POSITION WHICH WILL PREVENT ANY POSSIBLE SHORTING PROBLEMS. LEADS MUST EASILY FOLLOW BRUSH AND SPRING MOVEMENT AS WEAR OCCURS. IMPROPER LEAD PLACEMENT MAY RESULT IN MOTOR DAMAGE. 12.4.7 If bearings rotate smoothly and are good, reinstall belt and brushes (refer to Assembly, Section 9).
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Component Maintenance Manual NOTE: Checking compressor oil quantity is only required if an excessive amount of oil is observed due to leaking or the system has been vented quickly thereby causing a loss of oil. An oil check can only be made with the system vented.
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Component Maintenance Manual SERVICING TASK 21-00-22-60-801 13.0 R12 AIR CONDITIONING SYSTEM SERVICING PROCEDURES SUBTASK 21-00-22-99F-016 13.1 General: 13.1.1 Reclaiming the system (R12) refrigerant charge is required on systems before system removal, after an accidental line break, component failure or when the system has excessive leaks.
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Component Maintenance Manual Reclaim/ Recycle Cart (R12) Hose adapter (1/2 in, male acme to ¼ female flare) SUBTASK 21-00-22-60-001 13.2 Evacuating The System (R12): NOTE: The system must be evacuated for a minimum of 45 minutes to remove air and moisture which can cause the system to have less than optimal performance.
Refer to the reclaim/recycle equipment manufacturer’s instruction manual for recovery unit handling and operation. Refrigerant charges for the system are as follows in Table 5. Aircraft Model Refrigerant Charge (lbs.) Pilatus PC12 2.0 lbs Table 5 Refrigerant Charge SUBTASK 21-00-22-60-003 13.4 Flushing The System (R12): 13.4.1 System flushing is required only when the system has experienced a catastrophic failure of...
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Component Maintenance Manual 13.4.5 Connect certified reclaim charging and recycle cart manifolds to system service ports (ensure reclaim cart is properly grounded) and recover remaining refrigerant (refer to the reclaim equipment manufacturer’s instruction manual for recovery unit handling and operation). 13.4.6 Remove expansion valve and install fittings and hoses to close loop after valve removal.
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Component Maintenance Manual STORAGE TASK 21-00-22-55-801 14.0 COMPRESSOR CONDENSER MODULE ASSEMBLY STORAGE PROCEDURES SUBTASK 21-00-22-99F-017 14.1 General: 14.1.1 This section defines the procedures and requirements necessary if the Compressor assembly is to be stored and not installed onto aircraft immediately. In addition, this section defines the procedures and requirements for operation on the aircraft during the cold winter months when the system is not typically needed or used.
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Component Maintenance Manual 14.2.4.2 Drain old oil into measuring cup to verify amount of oil being replaced. CAUTION: ONLY AN ENVIRO APPROVED TYPE OF OIL MAY BE USED IN THIS TYPE OF COMPRESSOR. CAUTION: DO NOT OVERFILL COMPRESSOR WITH OIL OR SYSTEM PERFORMANCE WILL BE AFFECTED.
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Component Maintenance Manual 14.4.1.3 If the component is removed from the original packaging and is not installed on the aircraft immediately, it is desirable that it be repackaged using the original Enviro Systems packaging. 14.4.1.4 If the component is removed from the original packaging and is not installed on the aircraft immediately and the original packaging is not available for repackaging, ensure that the component is packaged in the following manner.
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