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EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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This is the digital input data the DEUs send to the EEC:
* Total air temperature
* Corrected static pressure
* Total pressure
* Calculated mach number
* Greenwich mean time
* Clock date
* N1 target
* Flight number
* Bite data
* Landing gear position
* Start valve position
* Engine run status of other engine
* Databus status
* Start switch position
* Start lever position
* Ignition switch position
* Control mode switch position
* Air/ground
* Flap position
* Engine bleed switch position
* ACS pack switch position
* Cowl thermal anti-ice switch position
* Wing anti-ice switch position
* Isolation valve position.
This is the digital data the EEC sends to the DEUs:
* Bite data
* Engine start mode
* Engine starting status
* Ignition system status
* Engine running status
* Control mode switch position
* Minimum idle
* Idle selected
* N1 speed data
* N2 speed data
* Overspeed governor status
* Engine starter cutout
* Exhaust gas temperature (EGT) data
* Fuel flow data
* Fuel filter status
* Oil pressure and temperature data
* Oil filter status
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* Chips detected in oil
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* Thrust resolver angle (TRA) data
* Thrust reverser status
* Thrust reverser interlock status
* Engine thrust
* Values from engine Sensors
* EEC software version
* Engine serial number
* Position of engine actuators
* Fuel-air ratio in combustor
* EEC channel in control
* Start lever position
* Airplane-on-ground selection status
* Engine running
* Engine thrust rating and airplane model Incompatible
* Airplane model
ENGINE FUEL AND CONTROL - ENGINE CONTROL - INTERFACES
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D633A101-GUN Oct 10/2005
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-003
* Engine rating
* Engine options
* EEC alternator status
* Engine position
* Engine bleed load
* Air data status from ADIRUs
* Internal EEC fault.
Analog Control Data
The airplane sends and receives analog control data. This is the
analog data the EEC receives:
* Thrust lever resolver angle (TRA)
* Thrust reverser position
* Engine position
* Airplane model
* Position of engine actuators
* Control mode switch data.
This is the analog data the engine sends to other airplane
systems:
* N1 speed
* N2 speed
* Oil quantity
* HPSOV position command
* Thrust reverser interlock solenoid command.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - INTERFACES
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D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-003
ENGINE FUEL AND CONTROL - ENGINE CONTROL - INTERFACES
ENGINE FUEL AND CONTROL - ENGINE CONTROL - INTERFACES
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-003
Engine Left Side
These components of engine fuel and control system are on the
left side of the engine:
* T3 sensor
* PS3 pressure port
* EEC alternator
* PT25 sensor
* Hydromechanical unit (HMU).
ENGINE FUEL AND CONTROL - ENGINE CONTROL - COMPONENT LOCATION - LEFT SIDE
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-004
ENGINE FUEL AND CONTROL - ENGINE CONTROL - COMPONENT LOCATION - LEFT SIDE
ENGINE FUEL AND CONTROL - ENGINE CONTROL - COMPONENT LOCATION - LEFT SIDE
EFFECTIVITY
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D633A101-GUN Feb 10/2003
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-004
Engine Right Side
　
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