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EFFECTIVITY
GUN ALL 73-21-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-255
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 11
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 11
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-255
General
GUN 201-999
The OIL SYSTEM input monitoring page lets you monitor these
oil system parameters:
* PEO (oil pressure)
* TEO (engine oil temperature)
* FILTER BYPASSED
* DEBRIS DETECTED.
GUN 001-099, 101-115
The OIL SYSTEM input monitoring page lets you monitor these
oil system parameters:
* PEO (oil pressure)
* TEO (engine oil temperature)
* FILTER BYPASSED.
GUN ALL
The OIL SYSTEM page shows you the oil system values the
EEC sends to the DEUs.
OIL PRESSURE SELECTION
The OIL PRESSURE SELECTION page shows oil pressure
values for both EEC channels. SEL PEO is the oil pressure the
EEC sends to the DEU for engine indication. INPUT CH A and B
shows the oil pressure values for channels A and B. The V1 and
V2 values are voltages from the linear variable differential
transformer (LVDT) feedback signals.
The ACT CH A shows the active channel or the channel that
controls the engine. The GMM CH A shows the ground
maintenance mode (GMM) channel or the channel that
controls CDU BITE.
OIL TEMPERATURE
The OIL TEMPERATURE page shows engine oil temperature
values for both EEC channels. SEL TEO shows the oil
temperature the EEC sends to the DEU for engine indication.
TEO CH A and B shows the oil temperature values for EEC
channels A and B.
The ACT CH A shows the active channel or the channel that
controls the engine. The GMM CH A shows the ground
maintenance mode (GMM) channel or the channel that
controls CDU BITE.
OIL FILTER
The OIL FILTER page shows the oil filter bypass switch position
values for channels A and B. FILTER BYPASSED is the oil filter
bypass status the EEC sends to the DEUs for engine indication.
The ACT CH A shows the active channel or the channel that
controls the engine. The GMM CH A shows the ground
maintenance mode (GMM) channel or the channel that
controls CDU BITE.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-257
Training Information Point
If a parameter is not available, (?) symbols are put in place of
the parameter. If the parameter is out of range, (-) symbols are
put in place of the parameter.
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
EFFECTIVITY
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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
73-21-00-257
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
EFFECTIVITY
GUN 201-999 73-21-00
Page 98.61
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
73-21-00-257
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
ENGINE FUEL AND CONTROL - ENGINE CONTROL - TRAINING INFORMATION POINT - EEC BITE - INPUT PG 13
EFFECTIVITY
GUN 001-099, 101-115 73-21-00
Page 98.62
D633A101-GUN Jun 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
73-21-00-257
General
The SPEEDS input monitoring page lets you monitor the N1 and
N2 engine speeds. Engine speed is in RPM.
The SPEEDS page shows the N1 and N2 speeds the EEC uses
for engine indication and control.
N1 SELECTION
The N1 SELECTION page shows N1 speed values for both EEC
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