AUTOFLIGHT STATUS ANNUNCIATOR

Flight Management Computer System Component Location

Figure 1 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 02 Page 3 ú Nov 15/94
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C95194
A 737-300/400/500MAINTENANCE MANUAL

ELECTRONIC HORIZONTAL SITUATION INDICATOR (EHSI)

ELECTRONIC FLIGHT INSTRUMENT SYSTEM CONTROL PANEL (EFIS CP)

Flight Management Computer System Component Location
Figure 1 (Sheet 3)

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 AND A SINGLE FMC  ú CONFIG 1 ú 04 Page 4 ú Mar 15/95
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C95199
A 737-300/400/500MAINTENANCE MANUAL
THRUST MODE
ANNUNCIATION

Flight Management Computer System Component Location
Figure 1 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 05 Page 5 ú Mar 15/96
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C95200
A 737-300/400/500MAINTENANCE MANUAL

SWITCH/ INDICATOR

VHF NAVIGATION CONTROL PANEL

VNAV SWITCH/ LNAV SWITCH/ INDICATOR INDICATOR

ALTITUDE SELECT CONTROL

DFCS MODE CONTROL PANEL (EXAMPLE)

Flight Management Computer System Component Location

Figure 1 (Sheet 5)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

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 AND A SINGLE FMC  ú CONFIG 1 ú 05 Page 6 ú Mar 15/96
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C95205
A 737-300/400/500MAINTENANCE MANUAL

FAILURE LAMP
LAMP TEST PUSHBUTTON
ELECTRICAL CONNECTOR

FUEL SUMMATION UNIT

Flight Management Computer System Component Location
Figure 1 (Sheet 6)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

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F41836
A 737-300/400/500MAINTENANCE MANUAL

FMCS BITE PRINTER RECEPTACLE (OPTIONAL)
AND DATA TRANSFER UNIT RECEPTACLE

RECEPTACLE FOR PORTABLE CDU (OPTIONAL)

Flight Management Computer System Component Location

Figure 1 (Sheet 7)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 04 Page 8 ú Mar 15/96
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C95212
A
737-300/400/500MAINTENANCE MANUAL
 (13)
 Nose Cowl Anti-Icing (Chapter 75-11)

 (14)
 Variable Bleed Valve System (Chapter 75-32)

 (15)
 Engine Tachometer System (Chapter 77-12)

 2.  FMCS Overview_____________
 A.  The FMCS furnishes lateral and vertical navigation and guidance, cost-optimal speed and thrust targets, and percent N1 limit data. These targets and data may be coupled to the airplanes Digital Flight Control System (DFCS), from the beginning of the climbout phase to glide slope intercept or flaps deployment. The FMCS is available throughout the entire flight. However, all other automatic flight control, inertial and radio navigation systems in the airplane are operative, with or without the FMCS.
　
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