(2)
The flight management computer is located on the E-1 rack in the main equipment center.
E. Principle airplane systems and indicators that are connected to the FMCS are listed below:
(1)
Engine Bleed Air Compression Control System (Chapter 21-11)
(2)
Autopilot/Flight Director System (Chapter 22-11)
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A 737-300/400/500MAINTENANCE MANUAL
SEE
Flight Management Computer System Component Location
Figure 1 (Sheet 1)
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A 737-300/400/500MAINTENANCE MANUAL
ANNUNCIATOR
FLIGHT MODE ANNUNCIATOR
B
Flight Management Computer System Component Location
Figure 1 (Sheet 2)
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A 737-300/400/500MAINTENANCE MANUAL
NAVIGATION SWITCH
DRIFT ANGLE MAG/TRUE POINTER ANNUNCIATOR
HORIZONTAL SITUATION INDICATOR
Flight Management Computer System Component Location
Figure 1 (Sheet 3)
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A 737-300/400/500MAINTENANCE MANUAL
SETTING CONTROL
N1 TACHOMETER INDICATOR
LIMIT POINTER
VMO FLAG WINDOW
TARGET INDEX FLAG WINDOW
AIRSPEED POINTER
MANUAL INDEX SETTING CONTROL
Flight Management Computer System Component Location
Figure 1 (Sheet 4)
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SWITCH/ INDICATOR
VHF NAVIGATION CONTROL PANEL
Flight Management Computer System Component Location
Figure 1 (Sheet 5)
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FUEL SUMMATION UNIT
J
Flight Management Computer System Component Location
Figure 1 (Sheet 6)
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