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 |  موضوع: كتاب Training Manual CFM56-5C Engine Systems الأحد 09 أكتوبر 2022, 10:45 pm | |
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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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