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| موضوع: كتاب Training Manual CFM56-5C Engine Systems الأحد 9 أكتوبر 2022 - 22:45 | |
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أخواني في الله أحضرت لكم كتاب Training Manual CFM56-5C Engine Systems
و المحتوى كما يلي :
Table of contents 1 to 4 Lexis 1 to 10 Intro 1 to 12 ECU 73-21-60 Electronic control unit 1 to 24 Sensors 1 to 40 Harnesses 73-21-50 Engine wiring harnesses 1 to 10 Starting & ignition 80-00-00 Starting system 1 to 14 80-11-20 Starter air valve 1 to 10 80-11-10 Pneumatic starter 1 to 8 74-00-00 Ignition 1 to 14 Power management & fuel control 1 to 14EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL CONTENTS ENGINE SYSTEMS Page 3 Jan 03 EFG Chapter Section Page Fuel 73-11-00 Fuel distribution 1 to 8 73-11-10 Fuel pump 1 to 22 79-21-20 Main oil / fuel heat exchanger 1 to 6 73-11-20 Servo fuel heater 1 to 6 73-21-18 Hydromechanical unit 1 to 50 73-30-11 Fuel flow transmitter 1 to 8 73-11-45 Fuel nozzle filter 1 to 4 73-11-70 Burner staging valve 1 to 14 73-11-40 Fuel nozzle 1 to 12 73-11-64 IDG oil cooler 1 to 8 73-11-50 Fuel return valve 1 to 20 Geometry controL 75-30-00 Variable geometry control system 1 to 4 75-31-00 Variable bleed valve 1 to 18 75-32-00 Variable stator vane 1 to 12 Clearance control 75-26-00 Rotor active clearance control/start bleed 1 to 8 75-21-00 High pressure turbine clearance control 1 to 12 75-22-00 Low pressure turbine clearance control 1 to 10EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL CONTENTS ENGINE SYSTEMS Page 4 Jan 03 EFG Chapter Section Page Oil 79-00-00 Oil general 1 to 14 79-11-00 Oil tank 1 to 6 79-20-00 Anti-siphon 1 to 4 79-21-10 Lubrication unit 1 to 16 79-21-50 Master chip detector 1 to 6 79-30-00 Oil indicating components 1 to 4 79-31-00 Oil quantity transmitter 1 to 4 79-32-00 Oil temperature sensor 1 to 4 79-33-00 Oil pressure transmitter and oil low pressure switch 1 to 6 Vibration sensing 77-31-00 Vibration sensing 1 to 12 A A/C AIRCRAFT AC ALTERNATING CURRENT ACARS AIRCRAFT COMMUNICATION ADRESSING and REPORTING SYSTEM ACMS AIRCRAFT CONDITION MONITORING SYSTEM ACS AIRCRAFT CONTROL SYSTEM ADC AIR DATA COMPUTER ADEPT AIRLINE DATA ENGINE PERFORMANCE TREND ADIRS AIR DATA AND INERTIAL REFERENCE SYSTEM ADIRU AIR DATA AND INERTIAL REFERENCE UNIT AGB ACCESSORY GEARBOX AIDS AIRCRAFT INTEGRATED DATA SYSTEM ALF AFT LOOKING FORWARD ALT ALTITUDE ALTN ALTERNATE AMB AMBIENT AMM AIRCRAFT MAINTENANCE MANUAL AOG AIRCRAFT ON GROUND A/P AIR PLANE APU AUXILIARY POWER UNIT ARINC AERONAUTICAL RADIO, INC. (SPECIFICATION) ASM AUTOTHROTTLE SERVO MECHANISM A/T AUTOTHROTTLE ATA AIR TRANSPORT ASSOCIATION ATC AUTOTHROTTLE COMPUTER ATHR AUTO THRUST ATO ABORTED TAKE OFF AVM AIRCRAFT VIBRATION MONITORING B BITE BUILT IN TEST EQUIPMENT BMC BLEED MANAGEMENT COMPUTER BPRV BLEED PRESSURE REGULATING VALVE BSI BORESCOPE INSPECTION BSV BURNER STAGING VALVE (SAC) BSV BURNER SELECTION VALVE (DAC) BVCS BLEED VALVE CONTROL SOLENOID CC CELSIUS or CENTIGRADE CAS CALIBRATED AIR SPEED CBP (HP) COMPRESSOR BLEED PRESSURE CCDL CROSS CHANNEL DATA LINK CCFG COMPACT CONSTANT FREQUENCY GENERATOR CCU COMPUTER CONTROL UNIT CCW COUNTER CLOCKWISE CDP (HP) COMPRESSOR DISCHARGE PRESSURE CDS COMMON DISPLAY SYSTEM CDU CONTROL DISPLAY UNIT CFDIU CENTRALIZED FAULT DISPLAY INTERFACE UNIT CFDS CENTRALIZED FAULT DISPLAY SYSTEM EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 2 Nov 02 EFGCFMI JOINT GE/SNECMA COMPANY (CFM INTERNATIONAL) CG CENTER OF GRAVITY Ch A channel A Ch B channel B CHATV CHANNEL ACTIVE CIP(HP) COMPRESSOR INLET PRESSURE CIT(HP) COMPRESSOR INLET TEMPERATURE cm.g CENTIMETER X GRAMS CMC CENTRALIZED MAINTENANCE COMPUTER CMM COMPONENT MAINTENANCE MANUAL CMS CENTRALIZED MAINTENANCE SYSTEM CMS CENTRAL MAINTENANCE SYSTEM CODEP HIGH TEMPERATURE COATING CONT CONTINUOUS CPU CENTRAL PROCESSING UNIT CRT CATHODE RAY TUBE CSD CONSTANT SPEED DRIVE CSI CYCLES SINCE INSTALLATION CSN CYCLES SINCE NEW CTAI COWL THERMAL ANTI-ICING CTEC CUSTOMER TECHNICAL EDUCATION CENTER CTL CONTROL Cu.Ni.In COPPER.NICKEL.INDIUM CW CLOCKWISE D DAC DOUBLE ANNULAR COMBUSTOR DAMV DOUBLE ANNULAR MODULATED VALVE DAR DIGITAL ACMS RECORDER DC DIRECT CURRENT DCU DATA CONVERSION UNIT DCV DIRECTIONAL CONTROL VALVE BOEING DEU DISPLAY ELECTRONIC UNIT DFCS DIGITAL FLIGHT CONTROL SYSTEM DFDAU DIGITAL FLIGHT DATA ACQUISITION UNIT DFDRS DIGITAL FLIGHT DATA RECORDING SYSTEM DISC DISCRETE DIU DIGITAL INTERFACE UNIT DMC DISPLAY MANAGEMENT COMPUTER DMD DEMAND DMS DEBRIS MONITORING SYSTEM DMU DATA MANAGEMENT UNIT DOD DOMESTIC OBJECT DAMAGE DPU DIGITAL PROCESSING MODULE DRT DE-RATED TAKE-OFF E EAU ENGINE ACCESSORY UNIT EBU ENGINE BUILDUP UNIT ECA ELECTRICAL CHASSIS ASSEMBLY ECAM ELECTRONIC CENTRALIZED AIRCRAFT MONITORING ECS ENVIRONMENTAL CONTROL SYSTEM ECU ELECTRONIC CONTROL UNIT EE ELECTRONIC EQUIPMENT EEC ELECTRONIC ENGINE CONTROL EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 3 Nov 02 EFGEFH ENGINE FLIGHT HOURS EFIS ELECTRONIC FLIGHT INSTRUMENT SYSTEM EGT EXHAUST GAS TEMPERATURE EHSV ELECTRO-HYDRAULIC SERVO VALVE EICAS ENGINE INDICATING AND CREW ALERTING SYSTEM EIS ELECTRONIC INSTRUMENT SYSTEM EIU ENGINE INTERFACE UNIT EIVMU ENGINE INTERFACE AND VIBRATION MONITORING UNIT EMF ELECTROMOTIVE FORCE EMI ELECTRO MAGNETIC INTERFERENCE EMU ENGINE MAINTENANCE UNIT EPROM ERASABLE PROGRAMMABLE READ ONLY MEMORY (E)EPROM(ELECTRICALLY) ERASABLE PROGRAMMABLE READ ONLY MEMORY ESN ENGINE SERIAL NUMBER ETOPS EXTENDED TWIN OPERATION SYSTEMS EWD/SD ENGINE WARNING DISPLAY / SYSTEM DISPLAY FF FARENHEIT FAA FEDERAL AVIATION AGENCY FADEC FULL AUTHORITY DIGITAL ENGINE CONTROL FAR FUEL/AIR RATIO FCC FLIGHT CONTROL COMPUTER FCU FLIGHT CONTROL UNIT FDAMS FLIGHT DATA ACQUISITION & MANAGEMENT SYSTEM FDIU FLIGHT DATA INTERFACE UNIT FDRS FLIGHT DATA RECORDING SYSTEM FDU FIRE DETECTION UNIT FEIM FIELD ENGINEERING INVESTIGATION MEMO FF FUEL FLOW (see Wf) -7B FFCCV FAN FRAME/COMPRESSOR CASE VERTICAL (VIBRATION SENSOR) FI FLIGHT IDLE (F/I) FIM FAULT ISOLATION MANUAL FIN FUNCTIONAL ITEM NUMBER FIT FAN INLET TEMPERATURE FLA FORWARD LOOKING AFT FLX TO FLEXIBLE TAKE-OFF FMC FLIGHT MANAGEMENT COMPUTER FMCS FLIGHT MANAGEMENT COMPUTER SYSTEM FMGC FLIGHT MANAGEMENT AND GUIDANCE COMPUTER FMGEC FLIGHT MANAGEMENT AND GUIDANCE ENVELOPE COMPUTER FMS FLIGHT MANAGEMENT SYSTEM FMV FUEL METERING VALVE FOD FOREIGN OBJECT DAMAGE FPA FRONT PANEL ASSEMBLY FPI FLUORESCENT PENETRANT INSPECTION FQIS FUEL QUANTITY INDICATING SYSTEM EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 4 Nov 02 EFGFRV FUEL RETURN VALVE FWC FAULT WARNING COMPUTER FWD FORWARD G g.in GRAM X INCHES GE GENERAL ELECTRIC GEAE GENERAL ELECTRIC AIRCRAFT ENGINES GEM GROUND-BASED ENGINE MONITORING GI GROUND IDLE (G/I) GMM GROUND MAINTENANCE MODE GMT GREENWICH MEAN TIME GND GROUND GPH GALLON PER HOUR GPU GROUND POWER UNIT GSE GROUND SUPPORT EQUIPMENT H HCF HIGH CYCLE FATIGUE HCU HYDRAULIC CONTROL UNIT HDS HORIZONTAL DRIVE SHAFT HMU HYDROMECHANICAL UNIT HP HIGH PRESSURE HPC HIGH PRESSURE COMPRESSOR HPCR HIGH PRESSURE COMPRESSOR ROTOR HPRV HIGH PRESSURE REGULATING VALVE HPSOV HIGH PRESSURE SHUT-OFF VALVE HPT HIGH PRESSURE TURBINE HPT(A)CC HIGH PRESSURE TURBINE (ACTIVE) CLEARANCE CONTROL HPTC HIGH PRESSURE TURBINE CLEARANCE HPTCCV HIGH PRESSURE TURBINE CLEARANCE CONTROL VALVE HPTN HIGH PRESSURE TURBINE NOZZLE HPTR HIGH PRESSURE TURBINE ROTOR Hz HERTZ (CYCLES PER SECOND) I I/O INPUT/OUTPUT IAS INDICATED AIR SPEED ID INSIDE DIAMETER ID PLUG IDENTIFICATION PLUG IDG INTEGRATED DRIVE GENERATOR IFSD IN FLIGHT SHUT DOWN IGB INLET GEARBOX IGN IGNITION IGV INLET GUIDE VANE in. INCH IOM INPUT OUTPUT MODULE IPB ILLUSTRATED PARTS BREAKDOWN IPC ILLUSTRATED PARTS CATALOG IPCV INTERMEDIATE PRESSURE CHECK VALVE IPS INCHES PER SECOND IR INFRA RED K °K KELVIN k X 1000 KIAS INDICATED AIR SPEED IN KNOTS kV KILOVOLTS EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 5 Nov 02 EFGKph KILOGRAMS PER HOUR LL LEFT L/H LEFT HAND lbs. POUNDS, WEIGHT LCD LIQUID CRYSTAL DISPLAY LCF LOW CYCLE FATIGUE LE (L/E) LEADING EDGE LGCIU LANDING GEAR CONTROL INTERFACE UNIT LP LOW PRESSURE LPC LOW PRESSURE COMPRESSOR LPT LOW PRESSURE TURBINE LPT(A)CC LOW PRESSURE TURBINE (ACTIVE) CLEARANCE CONTROL LPTC LOW PRESSURE TURBINE CLEARANCE LPTN LOW PRESSURE TURBINE NOZZLE LPTR LOW PRESSURE TURBINE ROTOR LRU LINE REPLACEABLE UNIT LVDT LINEAR VARIABLE DIFFERENTIAL TRANSFORMER M mA MILLIAMPERES (CURRENT) MCD MAGNETIC CHIP DETECTOR MCDU MULTIPURPOSE CONTROL AND DISPLAY UNIT MCL MAXIMUM CLIMB MCR MAXIMUM CRUISE MCT MAXIMUM CONTINUOUS MDDU MULTIPURPOSE DISK DRIVE UNIT MEC MAIN ENGINE CONTROL milsD.A. Mils DOUBLE AMPLITUDE mm. MILLIMETERS MMEL MAIN MINIMUM EQUIPMENT LIST MO AIRCRAFT SPEED MACH NUMBER MPA MAXIMUM POWER ASSURANCE MPH MILES PER HOUR MTBF MEAN TIME BETWEEN FAILURES MTBR MEAN TIME BETWEEN REMOVALS mV MILLIVOLTS Mvdc MILLIVOLTS DIRECT CURRENT N N1 (NL) LOW PRESSURE ROTOR ROTATIONAL SPEED N1* DESIRED N1 N1ACT ACTUAL N1 N1CMD COMMANDED N1 N1DMD DEMANDED N1 N1K CORRECTED FAN SPEED N1TARGET TARGETED FAN SPEED N2 (NH) HIGH PRESSURE ROTOR ROTATIONAL SPEED N2* DESIRED N2 N2ACT ACTUAL N2 N2K CORRECTED CORE SPEED N/C NORMALLY CLOSED N/O NORMALLY OPEN EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 6 Nov 02 EFGNAC NACELLE NVM NON VOLATILE MEMORY O OAT OUTSIDE AIR TEMPERATURE OD OUTLET DIAMETER OGV OUTLET GUIDE VANE OSG OVERSPEED GOVERNOR OVBD OVERBOARD OVHT OVERHEAT P Pb BYPASS PRESSURE Pc REGULATED SERVO PRESSURE Pcr CASE REGULATED PRESSURE Pf HEATED SERVO PRESSURE P/T25 HP COMPRESSOR INLET TOTAL AIR PRESSURE/TEMPERATURE P/N PART NUMBER P0 AMBIENT STATIC PRESSURE P25 HP COMPRESSOR INLET TOTAL AIR TEMPERATURE PCU PRESSURE CONVERTER UNIT PLA POWER LEVER ANGLE PMC POWER MANAGEMENT CONTROL PMUX PROPULSION MULTIPLEXER PPH POUNDS PER HOUR PRSOV PRESSURE REGULATING SERVO VALVE Ps PUMP SUPPLY PRESSURE PS12 FAN INLET STATIC AIR PRESSURE PS13 FAN OUTLET STATIC AIR PRESSURE PS3HP COMPRESSOR DISCHARGE STATIC AIR PRESSURE (CDP) PSI POUNDS PER SQUARE INCH PSIA POUNDS PER SQUARE INCH ABSOLUTE PSID POUNDS PER SQUARE INCH DIFFERENTIAL psig POUNDS PER SQUARE INCH GAGE PSM POWER SUPPLY MODULE PSS (ECU) PRESSURE SUB-SYSTEM PSU POWER SUPPLY UNIT PT TOTAL PRESSURE PT2 FAN INLET TOTAL AIR PRESSURE (PRIMARY FLOW) PT25 HPC TOTAL INLET PRESSURE Q QAD QUICK ATTACH DETACH QEC QUICK ENGINE CHANGE QTY QUANTITY QWR QUICK WINDMILL RELIGHT R R/H RIGHT HAND RAC/SB ROTOR ACTIVE CLEARANCE/START BLEED RACC ROTOR ACTIVE CLEARANCE CONTROL RAM RANDOM ACCESS MEMORY RCC REMOTE CHARGE CONVERTER RDS RADIAL DRIVE SHAFT EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 7 Nov 02 EFGRPM REVOLUTIONS PER MINUTE RTD RESISTIVE THERMAL DEVICE RTO REFUSED TAKE OFF RTV ROOM TEMPERATURE VULCANIZING (MATERIAL) RVDT ROTARY VARIABLE DIFFERENTIAL TRANSFORMER S S/N SERIAL NUMBER S/R SERVICE REQUEST S/V SHOP VISIT SAC SINGLE ANNULAR COMBUSTOR SAR SMART ACMS RECORDER SAV STARTER AIR VALVE SB SERVICE BULLETIN SCU SIGNAL CONDITIONING UNIT SDAC SYSTEM DATA ACQUISITION CONCENTRATOR SDI SOURCE/DESTINATION IDENTIFIER (BITS) (CF ARINC SPEC) SDU SOLENOID DRIVER UNIT SER SERVICE EVALUATION REQUEST SFC SPECIFIC FUEL CONSUMPTION SFCC SLAT FLAP CONTROL COMPUTER SG SPECIFIC GRAVITY SLS SEA LEVEL STANDARD (CONDITIONS : 29.92 in.Hg / 59°F) SLSD SEA LEVEL STANDARD DAY (CONDITIONS : 29.92 in.Hg / 59°F) SMM STATUS MATRIX SMP SOFTWARE MANAGEMENT PLAN SN SERIAL NUMBER SNECMA SOCIETE NATIONALE D’ETUDE ET DE CONSTRUCTION DE MOTEURS D’AVIATION SOL SOLENOID SOV SHUT-OFF VALVE STP STANDARD TEMPERATURE AND PRESSURE SVR SHOP VISIT RATE SW SWITCH BOEING SYS SYSTEM T T oil OIL TEMPERATURE T/C THERMOCOUPLE T/E TRAILING EDGE T/O TAKE OFF T/R THRUST REVERSER T12 FAN INLET TOTAL AIR TEMPERATURE T25 HP COMPRESSOR INLET AIR TEMPERATURE T3 HP COMPRESSOR DISCHARGE AIR TEMPERATURE T49.5 EXHAUST GAS TEMPERATURE T5 LOW PRESSURE TURBINE DISCHARGE TOTAL AIR TEMPERATURE TAI THERMAL ANTI ICE TAT TOTAL AIR TEMPERATURE EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 8 Nov 02 EFGTBC THERMAL BARRIER COATING TBD TO BE DETERMINED TBO TIME BETWEEN OVERHAUL TBV TRANSIENT BLEED VALVE TC(TCase) HP TURBINE CASE TEMPERATURE TCC TURBINE CLEARANCE CONTROL TCCV TURBINE CLEARANCE CONTROL VALVE TCJ TEMPERATURE COLD JUNCTION T/E TRAILING EDGE TECU ELECTRONIC CONTROL UNIT INTERNAL TEMPERATURE TEO ENGINE OIL TEMPERATURE TGB TRANSFER GEARBOX Ti TITANIUM TLA THROTTLE LEVER ANGLE AIRBUS TLA THRUST LEVER ANGLE BOEING TM TORQUE MOTOR TMC TORQUE MOTOR CURRENT T/O TAKE OFF TO/GA TAKE OFF/GO AROUND T/P TEMPERATURE/PRESSURE SENSOR TPU TRANSIENT PROTECTION UNIT TR TRANSFORMER RECTIFIER TRA THROTTLE RESOLVER ANGLE AIRBUS TRA THRUST RESOLVER ANGLE BOEING TRDV THRUST REVERSER DIRECTIONAL VALVE TRF TURBINE REAR FRAME TRPV THRUST REVERSER PRESSURIZING VALVE TSI TIME SINCE INSTALLATION (HOURS) TSN TIME SINCE NEW (HOURS) TTL TRANSISTOR TRANSISTOR LOGIC U UER UNSCHEDULED ENGINE REMOVAL UTC UNIVERSAL TIME CONSTANT V VAC VOLTAGE, ALTERNATING CURRENT VBV VARIABLE BLEED VALVE VDC VOLTAGE, DIRECT CURRENT VDT VARIABLE DIFFERENTIAL TRANSFORMER VIB VIBRATION VLV VALVE VRT VARIABLE RESISTANCE TRANSDUCER VSV VARIABLE STATOR VANE W WDM WATCHDOG MONITOR Wf WEIGHT OF FUEL OR FUEL FLOW WFM WEIGHT OF FUEL METERED WOW WEIGHT ON WHEELS WTAI WING THERMAL ANTI-ICING EFFECTIVITY ALL CFM56-5C ENGINES FOR A340 CFMI PROPRIETARY INFORMATION CFM56-5C TRAINING MANUAL LEXIS Page 9 Nov 02 EFGEFFECTIVITY
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