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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT

In document Aircrft Engine (Page 21-85)

COMPONENT IDENTIFICATION

SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT

EEC shock mount Supplies electronic data that gives information

to the EEC for engine configuration.

EEC identification plug (P11) Holds the Electronic Engine Control (EEC) or (ECU)

Air sense line P25 Sends air pressure information to the EEC at

station 13 and is optional.

Air sense line PS13 Sends ambient air pressure information to the

EEC from station 0.

Air sense line PS3 Sends air pressure information to the EEC from

station 25 and is optional.

Air sense line PO Sends air pressure information to the EEC from

station 3.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

ITEM NO.

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Upper exciter box Supplies the exciter boxes with aircraft electrical

power.

Lower exciter box Supplies the RH igniter plug with electrical

power to start combustion.

RH ignition lead Supplies the LH igniter plug with electrical

power to start combustion.

LH ignition lead Supplies a path for the electrical energy to

reach the RH igniter plug to cause a spark.

115 Vac power supply connection Supplies a path for the electrical energy to reach the LH igniter plug to cause a spark.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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LH fan cowl Mechanical fastener to hold the fan cowls.

LH fan cowl latches Gives access to service the IDG.

IDG access door Supplies protection and aerodynamic airflow

over the engine LH fan module area.

EEC air inlet duct Discharge hot airflow from the engine inlet cowl.

Outlet for the inlet anti-ice system Air discharge for the starter.

Fan cowl airflow outlet Supplies cooling air to the EEC.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Integrated drive generator (IDG) Points air into the engine.

Low pressure turbine major module Supplies electricity for the aircraft.

Inlet cowl Supplies the energy to operate the engine.

Core major module Changes the energy to turn the fan and LPC.

Fan major module Supplies 80% of the thrust to operate the

engine.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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QAD ring Supplies an electrical connection for the cockpit

oil pressure signal.

Oil level sight glass Gives access to service the IDG oil filter.

IDG Supplies cool oil from the IDG oil coolers to IDG

for lubrication.

Phase lead terminal Mechanical fastener to hold the IDG

Disconnect reset ring Supplies the electrical connections for the

aircraft electrical systems from the engines.

Electrical connector Lets servicing of the IDG be done from a

remote oil supply system.

Charge filter Disconnects and resets the IDG shaft after

maintenance.

Pressure fill adapter Supplies access to check oil quantity in the

IDG.

IDG oil inlet port Supplies the primary electrical energy for the

aircraft electrical systems from the engine.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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IDG fuel/oil cooler

Electrical connection for the differential pressure switch for the engine scavenge oil filter.

IDG fuel/oil cooler IN line Decreases the temperature of the IDG hot oil with fuel from the LP side of the pump.

IDG fuel/oil cooler OUT line Sends cool oil back to the IDG.

Fan frame Sends hot oil to the IDG oil coolers to decrease

the temperature.

Differential pressure switch electrical connector Lets the AGB alignment be adjusted.

AGB turnbuckle The support structure for the forward engine

mount and the engine.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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IDG air/oil cooler Decreases engine noise.

Aft acoustical panels Uses fan air in a heat exchanger to supply cool

air for the IDG oil

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Hydraulic pump Supplies hydraulic fluid to the hydraulic pump.

Hydraulic pump IN line Supplies hydraulic fluid pressure to the airplane

systems.

Hydraulic pump OUT line Supplies hydraulic pump operation electrical

information to the airplane.

Hydraulic pump electrical connection Sends hydraulic fluid from the hydraulic pump.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Starter Uses air pressure during engine start to supply

N2 rotation

Starter air supply duct Supplies core speed to the EEC and to the

airplane systems.

N2 speed sensor Supplies electrical power to the electronic

engine control box.

Hand cranking pad Supplies air pressure to the starter.

EEC alternator Supplies N2 rotation by the manual method.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Starter air valve manual drive Supplies normal supply air pressure to the

starter.

Starter air valve Lets the starter air valve be opened manually.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Hydraulic connector for the pressure line Supplies fuel to the engine fuel pump.

Fuel supply line to the engine Supplies hydraulic fluid to the hydraulic pump.

Electrical connector for the thrust reversers Supplies hydraulic fluid to the airplane.

Hydraulic connector for the supply line Supplies hydraulic fluid to the hydraulic filter.

Thrust reverser actuator Operates the thrust reverser to deploy and

stow.

Hydraulic connector for the hydraulic fluid filter. Supplies electrical feedback information about the thrust reversers position.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Thrust reverser hold open actuator Opens/closes the T/R doors for maintenance.

Thrust reverser opening actuator safety lock collar

Supplies electrical information path to the airplane for fuel flow indication, etc.

Fuel flow transmitter Secures and safeties the actuator.

Fuel flow transmitter electrical connector Gives downstream protection to fuel nozzles.

In-line fuel filter Gives fuel flow information to the airplane for

indication.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Oil temperature sensor electrical connection Supplies electrical path to the aircraft for engine

oil temperature indication.

Oil temperature sensor Supplies electrical path to the aircraft for engine oil pressure indication.

Oil pressure sensor electrical connection Supplies electrical information to the aircraft for engine oil temperature indication.

Oil pressure sensor Supplies electrical information to the aircraft for

engine pressure indication.

Fan case Supplies fan blade containment and holds some

LRUs.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

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Accessory Gearbox (AGB) Supplies fuel to the fuel pump.

Transfer Gearbox (TGB) Holds and turns the accessories for the engine.

Main fuel/oil heat exchanger Supplies the N2 drive for the AGB.

Engine fuel supply line (port) Decreases temperature of the engine oil.

Servo fuel heater

Increases the temperature of the engine fuel to prevent ice particles entering the engine servo systems.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Channel B Supplies fuel from the LP fuel pump to the IDG

oil cooler.

Channel A Attaches the fuel pump to AGB.

Airframe shutoff (HPSOV) feedback Supplies the fuel to the engine fuel systems.

Hydromechanical Unit (HMU) Supplies the hydraulic muscle to operate the servo systems.

Fuel pump Transmits an HPSOV position signal to the

EEC, then to the ENGINE CLOSED light.

Fuel line Electrical connection for EEC channel B.

QAD ring Electrical connection for EEC channel A.

Low pressure stage fuel pump inspection plug LP stage pump impeller inspection access

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Oil scavenge filter Filters fuel from the LP pump.

Oil scavenge filter lock release Locks the oil filter and prevents rotation.

Fuel filter Gives pressure information to signal oil filter

clogging.

Fuel filter drain plug

Supplies pressure information to signal fuel filter clogging.

Fuel filter differential pressure switch Filters oil from the engine oil return.

Oil filter differential pressure switch Lets the AGB alignment be adjusted.

AGB turnbuckle Lets the engine fuel filter be drained.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

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Lubrication unit Filters the oil.

Magnetic chip detector bayonet slot Gives access to inspect for sumps debris

Magnetic chip detector Gives a clogging indication by a red pin that

pops out if the supply oil filter clogs.

Supply oil filter pop-out indicator Supplies alignment for proper installation.

Pressure oil supply filter Supplies the oil for the engine AGB.

AGB oil supply line Gives the oil supply and return for the engine oil

system.

Scavenge oil filter unlocking lugs Lets the scavenge oil filter be removed with a tool

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Engine oil supply line Sends oil from the engine aft sump.

Rear sump scavenge oil line Sends oil from the engine forward sump.

Forward sump scavenge oil line Sends oil from the engine AGB and TGB.

AGB TGB scavenge oil line Supplies the oil to the engine sumps and

accessories.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Debris monitoring system chip detector

Supplies the CDU information on oil system contamination in the AGB, TGB, forward and aft sumps.

Debris monitoring system chip detector lead Supplies the electrical path to the junction box then to the airplane CDU.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Debris monitoring system junction box (optional) Oil tank scupper drain.

Debris monitoring system chip detector lead

Sends the CDU data on oil system

contamination in the AGB, TGB, forward and aft sumps.

Drain line The electrical path to the junction box then to

the airplane CDU.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Anti-leakage valve Supplies the lubrication unit with oil.

Oil supply line Lets removal of the lubrication unit occur

without draining the oil tank.

Oil pressure line Supplies pressurized oil to keep the

anti-leakage valve open.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT RH VBV actuator drain line

LH VBV actuator drain line RH VSV actuator drain line LH VSV actuator drain line Transient bleed valve drain line HPTACC valve drain line LPTACC valve drain line

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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VBV open line Supplies the fuel pressure to operate the TBV.

VBV close line Supplies the fuel pressure to close the VBV

doors.

VSV rod line Holds the forward part of the engine.

VSV head line Supplies the fuel pressure to operate the

LPTACC valve.

Transient bleed valve line Supplies the fuel pressure to operate the HPTACC valve.

HPTACC valve line Supplies the fuel pressure to open the VSV’.

LPTACC valve line Supplies the fuel pressure to close the VSVs.

HMU Supplies the reference pressure to operate

some valve.

PCR line Supplies the fuel pressure to close the BSV.

Burner staging valve line Supplies the fuel pressure to open the VBV

doors.

HPSOV electrical connector

Supplies servo system fuel input to operate engine components and regulates fuel for nozzles.

Fan frame Supplies the electrical input to operate the

HPSOV.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

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Forward sump vent line Supplies the housing for the 9 o’clock tube

bundle.

Transfer Gearbox Supplies the air signal to operate the engine oil

pressure indicator.

Fan frame strut fairing Relays the N2 drive for the AGB.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Engine high pressure bleed air regulator Supplies the high pressure customer bleed air

control.

LH VBV actuator Supplies the mechanical drive power to operate

the VBVs.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

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Fan duct panel Supplies the attachment support for the thrust

reverser system and core cowl air sealing.

Outlet guide vanes Supplies the cover over the VBV and the air

outlet when they are open.

Internal V-groove panel Changes the direction of the air out of the fan.

Fan frame strut Holds and gives rigidity to the fan frame.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Variable bleed valve door Supplies the booster air control into the core to

prevent a stall.

Variable bleed valve actuator connecting rod Fuel pressure to open the VBVs.

Variable bleed valve actuator drain line Fuel pressure to close the VBVs.

VBV actuator LVDT position feedback connector

Changes the hydraulic actuator movement into a mechanical movement, to open and close the VBVs.

VBV actuator rod line (close)

Changes the hydraulic actuator movement into an electrical position feedback signal to the EEC.

VBV actuator head line (open) Drains the fuel in case of actuator seal leakage.

LH VBV actuator One of the muscles to open the VBV doors.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Variable stator vane bellcrank

Changes the hydraulic actuator movement into a mechanical movement, to open and close the VSVs.

Variable stator vane actuator Changes the hydraulic fluid to a mechanical force to move the bellcrank assembly.

High pressure compressor forward stator case. Shows the dimension of the core for modular maintenance.

Metal core measurement placard Supports the HPC stators.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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Variable stator vane stage 1 Prevent HPCR core stalls and improves

efficiency of the engine.

Variable stator vane stage 2 Prevent HPCR core stalls and improves

efficiency of the engine.

Variable stator vane stage 3 Prevent HPCR core stalls and improves

efficiency of the engine.

Inlet guide vanes Prevent HPCR core stalls and improves

efficiency of the engine.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

ITEM NO.

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ITEM NO.

SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT Variable bleed valve door Supplies air to keep the LPT turbine stator case

cool.

Fan duct panel (removed) Supplies the booster air control into the core to prevent a stall.

LPT air inlet scoop Supplies the cover over the VBV and an air

outlet when VBVs are open.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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HPT shroud support Supplies stages 4 and 9 cooling air to the HP

turbine shroud support.

HPT air duct Supplies structural strength to the HPT shroud.

HPTACC valve Controls the clearance inside the engine

between the HPT rotor and HPT shroud.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

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SELECT THE PURPOSE THAT MATCHES THE LINE ACCESSORY OR COMPONENT HPTACC valve 9th stage bleed air duct Supplies low pressure bleed air for HPT rotor

and HPT shroud clearance control.

HPTACC valve 4th stage bleed air duct Supplies high pressure bleed air for HPT rotor and HPT shroud clearance control.

HPTACC electrical connection Supplies the hydraulic pressure to move the HPTACC valve.

HPTACC valve fuel manifold Supplies the valve position feedback to the EEC.

FFCCV electrical connection Supplies vibration monitoring data to the AVM.

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

CFM56-7B TRAINING MANUAL

COMPONENT IDENTIFICATION

FUEL, CONFIGURATION 1 (BSV)

In document Aircrft Engine (Page 21-85)

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