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CFM56-ALL TRAINING MANUAL Published by CFMI CFMI Customer Training Center CFMI Customer Training Services Snecma Services GE Aircraft Engines Site de Melun-Montereau, Customer Technical Education Center Aérodrome de Villaroche 123 Merchant Street Chemin de Viercy, B.P. 1936, Mail Drop Y2 77019 - Melun Cedex Cincinnati, Ohio 45246 FRANCE...
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY Page 2 GENERAL ALL CFM56 ENGINES Issue 01 CFMI PROPRIETARY INFORMATION...
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For authorized maintenance practices and specifications, consult pertinent maintenance publications. The information (including technical data) contained in this document is the property of CFM International (GE and SNECMA). It is disclosed in confidence, and the technical data therein is exported under a U.S. Government license.
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY Page 4 GENERAL ALL CFM56 ENGINES Issue 01 CFMI PROPRIETARY INFORMATION...
CFM56-ALL TRAINING MANUAL LEXIS EFFECTIVITY Page 5 LEXIS ALL CFM56 ENGINES Issue 02 CFMI PROPRIETARY INFORMATION...
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CFM56-ALL TRAINING MANUAL AIR TRANSPORT ASSOCIATION AIRCRAFT AUTOTHROTTLE COMPUTER ALTERNATING CURRENT ATHR AUTO THRUST ACARS AIRCRAFT COMMUNICATION ABORTED TAKE OFF ADRESSING and REPORTING SYSTEM AVM AIRCRAFT VIBRATION MONITORING ACAU AIR CONDITIONING ACCESSORY UNIT ACMS AIRCRAFT CONDITION MONITORING SYSTEM BITE BUILT IN TEST EQUIPMENT ACS AIRCRAFT CONTROL SYSTEM BMC BLEED MANAGEMENT COMPUTER ADC AIR DATA COMPUTER...
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CFM56-ALL TRAINING MANUAL CFMI JOINT GE/SNECMA COMPANY (CFM DAR DIGITAL ACMS RECORDER INTERNATIONAL) DIRECT CURRENT CENTER OF GRAVITY DCU DATA CONVERSION UNIT Ch A channel A DCV DIRECTIONAL CONTROL VALVE BOEING Ch B channel B DEU DISPLAY ELECTRONIC UNIT CHATV...
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CFM56-ALL TRAINING MANUAL EFH ENGINE FLIGHT HOURS FDAMS FLIGHT DATA ACQUISITION & EFIS ELECTRONIC FLIGHT INSTRUMENT SYSTEM MANAGEMENT SYSTEM EGT EXHAUST GAS TEMPERATURE FDIU FLIGHT DATA INTERFACE UNIT EHSV ELECTRO-HYDRAULIC SERVO VALVE FDRS FLIGHT DATA RECORDING SYSTEM EICAS ENGINE INDICATING AND CREW FDU FIRE DETECTION UNIT ALERTING SYSTEM FEIM FIELD ENGINEERING INVESTIGATION MEMO...
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CFM56-ALL TRAINING MANUAL FWD FORWARD HPTC HIGH PRESSURE TURBINE CLEARANCE HPTCCV HIGH PRESSURE TURBINE CLEARANCE CONTROL VALVE g.in GRAM X INCHES HPTN HIGH PRESSURE TURBINE NOZZLE GENERAL ELECTRIC HPTR HIGH PRESSURE TURBINE ROTOR GEAE GENERAL ELECTRIC AIRCRAFT HERTZ (CYCLES PER SECOND) ENGINES GEM GROUND-BASED ENGINE MONITORING GROUND IDLE (G/I)
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CFM56-ALL TRAINING MANUAL KILOGRAMS PER HOUR MCT MAXIMUM CONTINUOUS MDDU MULTIPURPOSE DISK DRIVE UNIT MEC MAIN ENGINE CONTROL LEFT milsD.A. Mils DOUBLE AMPLITUDE LEFT HAND MILLIMETERS lbs. POUNDS, WEIGHT MMEL MAIN MINIMUM EQUIPMENT LIST LCD LIQUID CRYSTAL DISPLAY AIRCRAFT SPEED MACH NUMBER LOW CYCLE FATIGUE MPA MAXIMUM POWER ASSURANCE LE (L/E)
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CFM56-ALL TRAINING MANUAL NAC NACELLE PS13 FAN OUTLET STATIC AIR PRESSURE NVM NON VOLATILE MEMORY PS3HP COMPRESSOR DISCHARGE STATIC AIR PRESSURE (CDP) POUNDS PER SQUARE INCH OUTSIDE AIR TEMPERATURE PSIA POUNDS PER SQUARE INCH ABSOLUTE OUTLET DIAMETER PSID POUNDS PER SQUARE INCH DIFFERENTIAL OGV OUTLET GUIDE VANE psig POUNDS PER SQUARE INCH GAGE...
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CFM56-ALL TRAINING MANUAL RTD RESISTIVE THERMAL DEVICE SMP SOFTWARE MANAGEMENT PLAN RTO REFUSED TAKE OFF SERIAL NUMBER RTV ROOM TEMPERATURE VULCANIZING SNECMA SOCIETE NATIONALE D’ETUDE ET DE (MATERIAL) CONSTRUCTION DE MOTEURS D’AVIATION RVDT ROTARY VARIABLE DIFFERENTIAL SOL SOLENOID TRANSFORMER SOV SHUT-OFF VALVE STANDARD TEMPERATURE AND PRESSURE SVR SHOP VISIT RATE SERIAL NUMBER...
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CFM56-ALL TRAINING MANUAL TC(TCase) HP TURBINE CASE TEMPERATURE UTC UNIVERSAL TIME CONSTANT TCC TURBINE CLEARANCE CONTROL TCCV TURBINE CLEARANCE CONTROL VALVE TEMPERATURE COLD JUNCTION VOLTAGE, ALTERNATING CURRENT TRAILING EDGE VBV VARIABLE BLEED VALVE TECU ELECTRONIC CONTROL UNIT INTERNAL VDC VOLTAGE, DIRECT CURRENT TEMPERATURE VDT VARIABLE DIFFERENTIAL TRANSFORMER TEO ENGINE OIL TEMPERATURE...
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CFM56-ALL TRAINING MANUAL IMPERIAL / METRIC CONVERSIONS METRIC / IMPERIAL CONVERSIONS 1 mile = 1,609 km 1 km = 0.621 mile 1 ft 30,48 cm = 3.281 ft. or 39.37 in. 1 in. 25,4 mm 1 cm = 0.3937 in. 1 mil.
CFM56-ALL TRAINING MANUAL INTRODUCTION EFFECTIVITY Page 17 INTRODUCTION ALL CFM56 ENGINES Sep 03 BORESCOPE INSPECTION CFMI PROPRIETARY INFORMATION...
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CFM56-ALL TRAINING MANUAL ON CONDITION MAINTENANCE CFM56 engines use a maintenance concept called ‘On - Any obvious incidents that may have contributed to, Condition Maintenance’. This means that engines have or immediately preceded, an event. no periodic overhaul schedules and can remain installed under the wing until something important occurs, or when Lubrication particles analysis.
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CFM56-ALL TRAINING MANUAL SCHEDULED / UNSCHEDULED INSPECTION These are the 2 basic types of borescope inspections. Unscheduled - Scheduled inspection - Unscheduled inspection The purpose of the unscheduled inspection is to find defects inside the engine at abnormal time intervals, or Scheduled after an engine event, such as FOD, hot start, overspeed, vibration, etc...
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CFM56-ALL TRAINING MANUAL CFM56 MAIN CHARACTERISTICS Combustor Section CFM56 engines consist of two independent rotating systems: (-2, -3, -5A, -5C) : Annular SAC - The low pressure system, with a rotational speed (-5B, -7B) : designated N1. Annular SAC (option DAC) - The high pressure system, with a rotational speed designated N2.
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : Booster spool rotating air seals rub against the inner After entering the air inlet cowl, the total engine airflow shroud, and rotor blades rub against the outer shrouds. passes through fan rotor blades, which form stage 1 of Booster rotor.
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CFM56-ALL TRAINING MANUAL ��������������� ������������������� ���� �� �� ��� ��� ��������������� ��������������������������� ���� ��� ��� FAN AND BOOSTER CTC-229-005-00 BASIC ENGINE EFFECTIVITY Page 27 PARTICULARS ALL CFM56 ENGINES Sep 03 BORESCOPE INSPECTION CFMI PROPRIETARY INFORMATION...
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CFM56-ALL TRAINING MANUAL THE HIGH PRESSURE COMPRESSOR (HPC) (ALL) : The HPC is a 9-stage compressor mounted between the The case has internal machined circumferential slots that fan frame and the combustor case. hold the fixed vanes of stages 6, 7 and 8. The vanes are It consists of a rotor and front and rear stators.
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CFM56-ALL TRAINING MANUAL THE HIGH PRESSURE COMPRESSOR (HPC) (ALL) : Special tools. Borescope ports. Deep-well socket. There are 9 plugged borescope ports on the lower stator In case the shaft of borescope plugs S7, S8 or S9 case, at approximately the 5 o’clock position, and they are numbered S1 thru S9, where S1 is the most forward.
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CFM56-ALL TRAINING MANUAL COMBUSTOR SECTION (ALL) : The combustor section, consisting of the combustion Single Annular Combustor (SAC). case and chamber, is located between the HPC and the LPT. The combustion chamber is housed in the combustion It produces the necessary energy to drive the turbine case and is installed between the HPC stator stage 9 and rotors.
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CFM56-ALL TRAINING MANUAL COMBUSTOR SECTION (-5B, -7B) : Double Annular Combustor (DAC). The combustion case has 20 double-tip fuel nozzles The outer and inner liners are designed with panel overhangs which have closely spaced holes providing mounting pads and accommodates 3 fuel supply manifolds.
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CFM56-ALL TRAINING MANUAL COMBUSTOR SECTION (ALL) : Borescope ports. There are 4 borescope ports located around the combustor case to enable inspection of the combustion chamber. The ports are numbered S12 to S15 and accommodate a simple plug with a hexagonal head. Ports S12, S13, S14 and S15 have a 10mm diameter.
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CFM56-ALL TRAINING MANUAL THE HIGH PRESSURE TURBINE (HPT) & STAGE 1 LPT NOZZLE (ALL) : The HPT converts the kinetic energy of gasses from the The HPT shroud and stage 1 LPT nozzle assembly forms combustion chamber into torque to drive the HPC and it the connection between the core section and the LPT is housed in the combustion case.
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CFM56-ALL TRAINING MANUAL THE HIGH PRESSURE TURBINE (HPT) & STAGE 1 LPT NOZZLE (ALL) : (-5B, 5C, -7B) : Borescope ports. CAUTION : DO NOT MIX PLUGS S16 & S17 WITH PLUGS S12 TO S15. INSTALLING THEM IN THE WRONG PLACE MAY CAUSE ENGINE DAMAGE. The HPT section / stage 1 LPT nozzle borescope ports are located around the combustor case.
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CFM56-ALL TRAINING MANUAL THE LOW PRESSURE TURBINE (LPT) The LPT drives the fan and booster through the LPT (-5B, -7B) : shaft. The LPT rotor/stator has: 5 ports are available to inspect the LPT. (-2, -3, -5A, -5B, -7B) : 4 stages (-5C) : 5 stages.
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CFM56-ALL TRAINING MANUAL ACCESSORY DRIVE SYSTEM (-2) : (ALL) : For maintenance tasks, the core can be turned manually At engine start, the accessory drive system transmits through a handcranking pad on left side of the TGB. external power from the engine air starter to drive the core engine.
CFM56-ALL TRAINING MANUAL REQUIREMENTS EFFECTIVITY Page 47 REQUIREMENTS ALL CFM56 ENGINES Sep 03 BORESCOPE INSPECTION CFMI PROPRIETARY INFORMATION...
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CFM56-ALL TRAINING MANUAL BORESCOPE ACCESS LIMITATIONS (ALL) : There are two limitation factors that have to be considered when preparing for borescope inspection on CFM56 engines. These considerations are : - the size of the borescope probe to be inserted into the engine.
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CFM56-ALL TRAINING MANUAL WITHOUT MOTORING TIME TO PORT No. ENGINE PORT SIZE WRENCH REACH AREAS VIEWED LOCATION (MM) SIZE -2/-3/-5A -5B/-5C 100°F(38°C) 200°F(93°C) BOOSTER STAGE 3 T/E STAGE 4 L/E STAGE 5 T/E HPC CASE 10 MM 1/2 HEX STAGE 1 L/E 30 mn 8 MM 1/2 HEX...
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CFM56-ALL TRAINING MANUAL BORESCOPE ACCESS LIMITATIONS (ALL) : Probe 1 diameter limitation. To speed up the engine cool down time after shutdown, the engine starter may be used to dry motor the engine, Consult the table for port diameters where probe 1 can (Refer to the AMM).
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CFM56-ALL TRAINING MANUAL WITHOUT MOTORING TIME TO PORT No. ENGINE PORT SIZE WRENCH REACH AREAS VIEWED LOCATION (MM) SIZE -2/-3/-5A -5B/-5C 100°F(38°C) 200°F(93°C) COMBUSTION 10 MM 1 1/4 HEX COMBUSTOR 3.5 hrs 2.0 hrs CASE HPT NOZZLE L/E & T/E 4.5 hrs 3.0 hrs 10 MM...
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CFM56-ALL TRAINING MANUAL DOCUMENTATION (ALL) : AMM. The Aircraft Maintenace Manual (AMM) provides comprehensive instructions on how to perform a borescope inspection and provides the limits for the various engine parts. There are no definitive measurement devices for the borescope. Evaluating inconsistencies is not an easy task because all measurements by borescope are comparative.
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CFM56-ALL TRAINING MANUAL ---------------------------------------------------------------------------------------------------------------------------------------------- INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS ---------------------------------------------------------------------------------------------------------------------------------------------- Stages 1-4 compressor blade airfoil leading and trailing edge, upper 75 percent: A.Tears Not serviceable Replace the engine Ref. TASK 71-00-00-000- 042) or repair (Ref. TASK 72-31-00-300-004). B.Nicks, missing Any number 0.04 in. (1.0 See limit extensions material and mm) max depth...
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CFM56-ALL TRAINING MANUAL DOCUMENTATION (ALL) : NDTM. Words such as nicks, dents and scratches, for example, The records and maps will remain in the engine folder are often used in the AMM. until the damaged parts are repaired, or replaced. The NDTM (Non Destructive Test Manual) provides a Note : When defect/damage maps are used, accomplish comprehensive list and an explanation of these words in...
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CFM56-ALL TRAINING MANUAL MATERIALS AND EQUIPMENT (ALL) : Rigid borescope probe set. CFMI have designed their own light source 856A1322 and rigid borescope set 856A1320, including various probes, adapters and extensions. Optional equipment is available for cameras, computers, VCR’S, and special tools that attach to the equipment. Other borescope systems may be acceptable if they meet CFMI specifications.
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CFM56-ALL TRAINING MANUAL MATERIALS AND EQUIPMENT (ALL) : Rigid borescope probe set. There are 4 rigid borescope probes for inspection of the internal areas of the engine and each probe is used for a specific purpose : - Probe 1 (black) : Magnification, close inspection, detailed evaluation and confirmation of defects (cannot be used in every hole due to its diameter).
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CFM56-ALL TRAINING MANUAL MATERIALS AND EQUIPMENT (ALL) : Flexible probe set. Flexible borescope set 856A1321 and guide tube 856A1310 (blue) or 856A1351 (red), are designed to be used on CFM56 engines and meet CFMI specifications. (-5B, -7B) : Guide tube 856A1702 (red) is used for DAC engines. (ALL) : Optional equipment is available for cameras, computers, VCR’S, and special tools that attach to the borescope...
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CFM56-ALL TRAINING MANUAL EQUIPMENT CHECKS (ALL) : The borescope resolution monitor. Before starting any inspection inside the engine, the inspector should ensure that the viewing definition of the rigid and flexible borescope probes is as precise as possible. Borescope resolution monitor 856A1323 allows both rigid and flexible probes to be checked against a calibrated display.
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CFM56-ALL TRAINING MANUAL EQUIPMENT CHECKS (ALL) : The resolution target. Rigid probes. The resolution target is divided into group and element For rigid probes with a 1:1 magnification at 2in., the numbers, which gradually diminish in size towards the 6 individual lines (3 vertical and 3 horizontal) of group 3, center of the display.
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CFM56-ALL TRAINING MANUAL CORE ENGINE ROTATION (ALL) : (-5A, -5B, -5C) : Manual method: Two pads on the accessory gearbox (AGB) are used to rotate the core engine: - Insert a 3⁄4 inch square drive socket attached to a 2ft. long breaker bar into the handcranking drive pad.
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CFM56-ALL TRAINING MANUAL CORE ENGINE ROTATION (ALL) : Air drive method: The N2 rotor can also be turned with a pneumatic motor. Install the pneumatic motor assembly on the pad. (-2) : The direction of rotation and speed of the core engine Pneumatic motor 856A1142 is installed on the rotor can be selected through a hand, or foot control handcranking pad on the left side of the TGB.
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CFM56-ALL TRAINING MANUAL CORE ENGINE ROTATION (ALL) : Another way of turning the core is through Electronic Turning Tool (ETT) Sweeney, P/N 18946, which adapts on the same pad as the pneumatic motor. ETT method: Install the plate adapter, drive shaft and ETT motor assembly on the adequate pad, with a QAD clamp.
CFM56-ALL TRAINING MANUAL INSPECTION OF FAN AND BOOSTER FAN AND EFFECTIVITY Page 73 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : N1 rotor indexing. Setting a reference angular position for the rotor provides an easy method to return quickly and accurately to a defect found earlier. The following procedure enables the reference point for the N1 rotor to be obtained.
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CFM56-ALL TRAINING MANUAL �������������� ���������� ����������������� CTC-229-025-00 FAN AND EFFECTIVITY Page 75 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : Visual inspection of the fan blades is performed on a regular basis depending on the MRB, or MPD. If defects are found, then an unscheduled inspection is required. Possible defects: - missing material, tip curl. - nicks, dents, pits or scratches, usually due to ingestion of small foreign objects such as sand, stones, dust, tarmac, etc.
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CFM56-ALL TRAINING MANUAL ������� ������ ���� ���� ����� ���������� �������� ���� ������� ���� ������� ����������� �������� �������������� �������������������������������������� CTC-229-026-00 FAN AND EFFECTIVITY Page 77 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : Visual inspection of the outlet guide vanes (OGV) is performed on a regular basis depending on the MRB, or MPD. If defects are found, then an unscheduled inspection is required. Possible defects: - missing material.
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CFM56-ALL TRAINING MANUAL ����� ���������� ���� ������������ �������� ���� ���� ����������������� ��������� ���������������������������������� CTC-229-064-00 FAN AND EFFECTIVITY Page 79 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : Rigid probe No 2 (yellow), installed on a long right angle adapter, can be used to reach the front of the splitter fairing area in order to inspect the booster. From this position the following are visible: - Stator vane stage 1 - Rotor stage 2 leading edge through stator stage 1.
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CFM56-ALL TRAINING MANUAL ���� ������������������������������������������ ����������� ��������� ������������ � � ����������� � ����� ����������������������������������� CTC-229-027-00 FAN AND EFFECTIVITY Page 81 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (-2, -3, -5A, -7B) : To inspect the booster, unplugged borescope port S0 can be accessed with a probe installed on a long right angle adapter. (-5B, -5C) : To inspect the booster, unplugged borescope port S03 can be accessed with a probe installed on a long right angle adapter.
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CFM56-ALL TRAINING MANUAL ���� ������������������������������������������ ����������� ��������� ������������ ������������� � � � ������������������������������������������ CTC-229-028-00 FAN AND EFFECTIVITY Page 83 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (-5B, -5C) : After inspection through port S03, continue inspection of the booster through port S05, using probe No 2 (yellow), installed on a long right angle adapter. Port S05 is located at approximately 4 o’clock. Insert the borescope probe into the port and go through the 2 cases to reach the inspection area.
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CFM56-ALL TRAINING MANUAL ������������ ���� �������� ����������� ��������� ������������������������������������������ � � � � ������������������������������������������������������ CTC-229-029-00 FAN AND EFFECTIVITY Page 85 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : Area E : Booster rotor damage may occur after the engine - This area of the blade starts from the top of the experienced an abnormal problem. The following list platform and extends toward the blade tip for provides examples of conditions where a complete approximately 10 mm.
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CFM56-ALL TRAINING MANUAL ����� ��� ������������������ � ����� ����������������� ������������� �������� ���� ������� � ���� ����� ���������� ����� �������� ������������������������������ CTC-229-030-00 FAN AND EFFECTIVITY Page 87 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL FAN AND BOOSTER (ALL) : During an inspection of the booster, any defects should be assessed against the serviceability limits in the Aircraft Maintenance Manual. Possible defects: - Cracks or tears. - Nicks and scratches. - Dents. - Erosion.
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CFM56-ALL TRAINING MANUAL ���� ������� ������� �������� ��� ���� ���������� ����� ����� ���� ������� ���� ������������������������������ CTC-229-031-00 FAN AND EFFECTIVITY Page 89 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK FAN AND EFFECTIVITY Page 90 BOOSTER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
CFM56-ALL TRAINING MANUAL INSPECTION OF HIGH PRESSURE COMPRESSOR HIGH PRESSURE EFFECTIVITY Page 91 COMPRESSOR ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE COMPRESSOR (HPC) (ALL) : General inspection method. HPC rotor blade damage may occur after the engine experienced an abnormal operating problem. The To inspect the blades, it is necessary to open the VSV’s. following list provides examples of conditions where Refer to the appropriate procedure in the AMM.
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CFM56-ALL TRAINING MANUAL �� �� �� �� �� �� �� �� ��� � ������������������ ������������� ������������������������������ ������������������������������ ������������������������� �������� �������������� CTC-229-032-00 HIGH PRESSURE EFFECTIVITY Page 93 COMPRESSOR ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL N2 ROTOR INDEXING (ALL) : Stage 4 of the High Pressure Compressor is the first 5. The next blade is blade No 1. Position the leading stage where the blades are retained in position with blade edge of blade No 1 in line with the leading edge of locks.
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE COMPRESSOR (HPC) Inspection areas: - The outer third of the rotor blade tip area and the anti-erosion hard coating on the concave side. - The squealer tips. - The stage 1 blade stiffener near the tip of the blade. - The blade locks on stages 4 to 9, which maintain the blades in the circumferential slots.
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CFM56-ALL TRAINING MANUAL ��� ����� ��������� �������������� ����������������� ����������������� ������������� ������������ ������������� ������� �������������� ����������� �������������������� CTC-229-034-00 HIGH PRESSURE EFFECTIVITY Page 97 COMPRESSOR ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE COMPRESSOR (HPC) (ALL) : Refer to the AMM for the precise dimensions of the Rotor blades specific inspection areas. following critical areas: HPC rotor blade stages are all different. The lower area of the airfoil. This is the airfoil root radius area, plus the area From stage 1 to stage 9, they become smaller and are which extends toward the blade tip over approximately...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE COMPRESSOR (HPC) (ALL) : Possible defects: When the HPC blades are inspected, the following defects should be evaluated with the AMM serviceability limits : - Cracks, or tears. - Nicks and scratches. - Dents. - Erosion. - Tip curl.
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK HIGH PRESSURE EFFECTIVITY Page 102 COMPRESSOR ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
CFM56-ALL TRAINING MANUAL INSPECTION OF COMBUSTOR SECTION COMBUSTION EFFECTIVITY Page 103 CHAMBER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (ALL) : Single Annular Combustor (SAC). The combustor is inspected through ports S12, S13, S14, Probe 1 (black, hi-mag) is recommended for viewing the S15 and igniter ports S10 and S11, using probes 1, 2, 3 aft end of the inner and outer liners.
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CFM56-ALL TRAINING MANUAL ������������ ���������������������������� ���������������������������������������������� ������������������������������������������������������������ ���������������������������� ��������������������������� ����������������������������������� CTC-229-038-00 COMBUSTION EFFECTIVITY Page 105 CHAMBER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (ALL) : Inspection of SAC inner liner. Borescope inspection of the combustion section may be required for a visual assessment as part of the on- The inner liner has a dome band and 4 panels. condition maintenance plan.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (ALL) : Possible defects on SAC liners. Carbon deposits are often misinterpreted as defects (holes, burn-through, cracks, etc.). Use the high magnification probe, and higher light intensity to confirm the type of defect. The aft panel of the inner liner is prone to distortion and cracking.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (ALL) : Inspection of the SAC dome area. The following areas of the combustion chamber also need to be inspected: - Fuel nozzle tips. - Fuel nozzle stems outside the combustor dome. - Sleeves with 2 concentric swirlers. - Deflectors.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (ALL) : Possible defects in the SAC dome area. The following defects should be assessed with the AMM serviceability limits : - Cracks, or tears. - Erosion. - Distortion of internal parts. - Missing material. - Dirt buildup.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION Inspection of SAC chamber after birdstrike/FOD. Insert a rigid probe into the left igniter position and examine the position of the fuel nozzle tips in relation to the bore of the inner and outer ferrules to make sure they are in the bore of the ferrules.
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CFM56-ALL TRAINING MANUAL ������ ������������������� ������������������ ���������������� ������������ ��������������������� ��������������������� ��������������������������������� CTC-229-065-00 COMBUSTION EFFECTIVITY Page 115 CHAMBER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (-5B, -7B) : Double Annular Combustor (DAC). Probe 1 (black) is recommended for viewing the aft ends of the inner and outer liners. It is also used for evaluating defects that were found when using probes 2, 3, or 4. The combustor is inspected through ports S12, S13, S14, S14.5, S15 and igniter ports S10 and S11.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (-5B, -7B) : Inspection of DAC outer liner. The outer liner has a dome band and 4 panels. Panel 1 features 2 igniter holes (with ferrules), and small dilution holes. Panel 2 features 5 borescope holes and 2 small dilution holes near the igniters.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (-5B, -7B) : Inspection of DAC dome area. The following areas of the combustion chamber also need to be inspected: - Fuel nozzle tips. - Fuel nozzle stems outside the combustor dome. - Spectacle plate and inner and outer deflectors. - Inner and outer liners.
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (-5B, -7B) : Possible defects in the DAC dome area. Possible defects on the DAC outer and inner liners. Whenever the combustion chamber is inspected, the Carbon deposits are often misinterpreted as defects following defects should be assessed with the AMM (holes, burn-through, cracks, etc.).
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CFM56-ALL TRAINING MANUAL COMBUSTION SECTION (-5B, -7B) : Inspection of DAC chamber after birdstrike/FOD. Insert a rigid probe into the left igniter position and examine the position of the fuel nozzle tips in relation to the bore of the inner and outer ferrules to make sure they are in the bore of the ferrules.
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK COMBUSTION EFFECTIVITY Page 126 CHAMBER ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
CFM56-ALL TRAINING MANUAL INSPECTION OF HIGH PRESSURE TURBINE HIGH PRESSURE EFFECTIVITY Page 127 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Inspection with rigid probe. Inspect the HPT nozzles through ports S13 and S15. Use probe No 1 (black, high magnification) to inspect the nozzle segments. The high intensity light source is used to accurately inspect the nozzles.
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CFM56-ALL TRAINING MANUAL ������������ �������������� ������������ ����������������� ����� ��������������� �������������������� ����� ���������� ����� �������� �������������������������������������� CTC-229-048-00 HIGH PRESSURE EFFECTIVITY Page 129 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Inspection with flexible probe. Carefully push the flexible probe into the guide tube to Use the flexible probe with a guide tube to inspect the HPT nozzle segments on the convex sides, the trailing inspect the next HPT nozzle segment.
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Inspection of the HPT nozzle is usually carried out in conjunction with the combustion chamber inspection. HPT nozzle inspection areas. The HPT nozzle vanes are cast shells and internally divided into forward and aft cooling compartments. CDP cooling air enters the vane compartments through the inner and outer ends of the vanes and exits through holes in the vanes’s leading edge and slots in the trailing...
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CFM56-ALL TRAINING MANUAL ���� ������� ����������������������� ����� ����� �������������� ���� ����� �������������� ������������ ���� ������������� ������������������� �������������� ����������� �������������������������������������� CTC-229-050-00 HIGH PRESSURE EFFECTIVITY Page 133 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Possible defects. Leading edge damage : - cracks. Whenever the HPT nozzle is inspected, the following - burns and/or bulges. - blocked cooling air passages. defects should be assessed with the AMM serviceability limits: Concave and convex surfaces : - Discoloration (anywhere).
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Inspection with a rigid probe. (-2, -3, -5A) : Inspect the HPT rotor blade T/E and the rear portion of the HPT shroud, through ports S17 and S18. (-5B, -5C, -7B) : Inspect the HPT rotor blade T/E and the rear portion of the HPT shroud, through ports S16 and S17.
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CFM56-ALL TRAINING MANUAL ������������ ���������� ����������� �������������� �������� �������� ������������� ����������� ���������������������������������� ������������������������������������ ������������������������������������ ������������������������������ ����������������������������������������������������������� CTC-229-052-00 HIGH PRESSURE EFFECTIVITY Page 137 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Inspection with a flexible probe. Use the flexible probe with the guide tube to inspect the HPT blade L/E and the forward part of the HPT shroud. Insert the guide tube 856A1310, or 856A1351, through the S10, or S11 ports and position it between two nozzle vanes.
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : (ALL) : HPT rotor damage may occur after engine abnormal Individual replaceable shroud segments face the blade operation. tips and are cooled with CDP air. They can be checked during inspection of the HPT rotor leading edge and nozzle guide vane trailing edge.
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Specific rotor blades inspection areas. Specific inspection areas for the HPT blades are defined as follows: Area C : - All around the blade, extending from the first T/E slot just above the root fillet, toward the tip of the blade, up to the sixth T/E slot.
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CFM56-ALL TRAINING MANUAL HIGH PRESSURE TURBINE (HPT) (ALL) : Possible defects. The following defects may be observed and should be assessed with the serviceability limits in the AMM. Trailing edge : - cracks. Tip area : - cracks. - bent, curled, or missing pieces. - tip trailing edge wear.
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK HIGH PRESSURE EFFECTIVITY Page 146 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
CFM56-ALL TRAINING MANUAL INSPECTION OF LOW PRESSURE TURBINE LOW PRESSURE EFFECTIVITY Page 147 TURBINE ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL LOW PRESSURE TURBINE (LPT) (ALL) : (-2, -3, -5A, -5B, -7B) : Stage 2 thru 4 blades. The LPT features long span blades. Moving the probe in and out enables a full-length inspection, which always (-5C) : starts at the blade platform.
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CFM56-ALL TRAINING MANUAL LOW PRESSURE TURBINE (LPT) (ALL) : Inspection areas. LPT rotor blade damage may occur after the engine experienced an abnormal operating condition. The On the LPT blades, there are 2 specific areas which are following list provides examples of the conditions where dimensionally defined through section letters: a complete LPT borescope inspection should be Area E (tip of the blade):...
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CFM56-ALL TRAINING MANUAL LOW PRESSURE TURBINE (LPT) (ALL) : Possible defects. Whenever the LPT blades are inspected, the following defects should be assessed against the AMM serviceability limits : - Cracks in the airfoil surface, platform, or tip shroud. - Convex and/or concave surfaces nicks and dents. - Leading edge distortion and melting, due to overtemperature.
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CFM56-ALL TRAINING MANUAL LOW PRESSURE TURBINE (LPT) (ALL) : Possible defects on last stage blades. In addition to the regular defects previously described, the following can also be found on the last stage blades: - No more axial preload on the tip shroud assembly. - Tip shroud interlock wear.
CFM56-ALL TRAINING MANUAL APPENDIX : NUMBER OF BLADES PER ROTOR APPENDIX EFFECTIVITY Page 157 BORESCOPE ALL CFM56 ENGINES Sep 03 INSPECTION CFMI PROPRIETARY INFORMATION...
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CFM56-ALL TRAINING MANUAL BLADE QUANTITIES Here is a table giving the quantity of blades on the following rotors, for each engine model: - The fan and booster rotor, where Stage 1 is the fan rotor itself - The high pressure compressor rotor - The high pressure turbine rotor - The low pressure turbine rotor.
CFM56-ALL TRAINING MANUAL SERVICE BULLETINS SERVICE EFFECTIVITY Page 161 BULLETINS ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL SERVICE BULLETINS In addition to standard borescope inspection of the various engine sections, some areas necessitate particular attention. The following page provides a list of recommended Service Bulletins, classified by ATA chapter number, subject and engine applicability. SERVICE EFFECTIVITY Page 162...
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CFM56-ALL TRAINING MANUAL SB NUMBER AND APPLICABILITY PER ENGINE MODEL SERVICE BULLETIN TITLE CHAPTER Inspection of HPC Stage 1 Disk Bore 72-064 72-32-00 Compressor Front Stator - On-Wing 72-553 72-427 72-515 Borescope Inspection for HPC Stator to Rotor Contact On-Wing Borescope Inspection of the 72-850 72-445 72-591 72-897 72-536 72-246 72-366 72-304 Combustion Chamber Outer Cowl Borescope Inspection of Inner Liner...
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CFM56-ALL TRAINING MANUAL THIS PAGE INTENTIONALLY LEFT BLANK SERVICE EFFECTIVITY Page 164 BULLETINS ALL CFM56 ENGINES Sep 03 BORESCOPE CFMI PROPRIETARY INFORMATION INSPECTION...
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CFM56-ALL TRAINING MANUAL REFERENCE ILLUSTRATIONS EFFECTIVITY REFERENCE Page 165 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ���������������������� ������� CTC-229-004-1-00 EFFECTIVITY REFERENCE Page 166 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ���������������������� ������� CTC-229-004-2-00 EFFECTIVITY REFERENCE Page 167 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ���������������������� �������� CTC-229-004-3-00 EFFECTIVITY REFERENCE Page 168 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ������������������ ���������������������� �������� CTC-229-004-4-00 EFFECTIVITY REFERENCE Page 169 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ���������������������� �������� CTC-229-004-5-00 EFFECTIVITY REFERENCE Page 170 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��������������� ��� ��� ���������������������� �������� CTC-229-004-6-00 EFFECTIVITY REFERENCE Page 171 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CTC-229-010-1-00 EFFECTIVITY REFERENCE Page 185 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-5B AS AN EXAMPLE CTC-229-010-3-00 EFFECTIVITY REFERENCE Page 186 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��� ��� ������� CTC-229-010-4-00 EFFECTIVITY REFERENCE Page 187 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-ALL CTC-229-012-1-00 EFFECTIVITY REFERENCE Page 188 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��� ��� ��� ��� �������� CTC-229-013-6-1-00 EFFECTIVITY REFERENCE Page 202 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL 856A1320 CTC-229-017-1-00 EFFECTIVITY REFERENCE Page 203 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL �������� �������� �������� ���������� CTC-229-019-1-00 EFFECTIVITY REFERENCE Page 204 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-2 CTC-229-022-1-00 EFFECTIVITY REFERENCE Page 205 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-3 CTC-229-022-2-00 EFFECTIVITY REFERENCE Page 206 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��� ��������� CTC-229-022-3-00 EFFECTIVITY REFERENCE Page 207 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��� ��������� CTC-229-022-4-00 EFFECTIVITY REFERENCE Page 208 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
Page 210
CFM56-ALL TRAINING MANUAL CFM56-7B CTC-229-022-5-00 EFFECTIVITY REFERENCE Page 209 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ��� �� ��������������������� ������������������������ ������������������������ �� ��� ��� ��� CTC-229-025-1-00 EFFECTIVITY REFERENCE Page 210 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-5B AS AN EXAMPLE CTC-229-032-1-00 EFFECTIVITY REFERENCE Page 211 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-ALL CTC-229-041-1-00 EFFECTIVITY REFERENCE Page 212 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL CFM56-5B, -7B CTC-229-045-1-00 EFFECTIVITY REFERENCE Page 213 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ����������� ������������� CTC-229-055-1-00 EFFECTIVITY REFERENCE Page 214 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...
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CFM56-ALL TRAINING MANUAL ������������ ��������� CTC-229-060-1-00 EFFECTIVITY REFERENCE Page 215 ALL CFM56 ENGINES ILLUSTRATIONS Sep 03 CFMI PROPRIETARY INFORMATION BORESCOPE INSPECTION...