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时间:2011-04-02 23:42来源:蓝天飞行翻译 作者:航空
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 D.  A single Flight Management Computer System (FMCS) is installed in the airplane. The FMCS consists of four units: two Control Display Units (CDUs) and two Flight Management Computers (FMCs) (Fig. 1).
 (1)  
The control display units are located on the pilots forward control stand electronic panel (P9).

 (2)  
The flight management computers are located on the E-1 rack in the main equipment center.

 (3)  
The FMC source select switch, located on the aft overhead panel, allows for dual FMC operation, or for one of the FMCs alone.


 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)

 (3)  
Autothrottle System (Chapter 22-31)

 (4)  
Digital Stall Warning System (Chapter 27-32)

 (5)  
Fuel Quantity Indicating System (Chapter 28-41)

 (6)  
Wing Thermal Anti-Icing System (Chapter 30-11)

 (7)  
Air Data Pressure Instruments (Chapter 34-12)

 (8)  
Electronic Flight Instrument System (Chapter 34-22)

 (9)  
Inertial Reference System (Chapter 34-28)

 (10)
 VOR/ILS Navigation System (Chapter 34-31)


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 34-62-01
 ú CONFIG ú 01 Page 1 ú Nov 15/93

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

FLIGHT COMPARTMENT

E1 RACK SEE

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

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 34-62-01

 ú CONFIG ú 04 Page 2 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C87457
A 737-300/400/500MAINTENANCE MANUAL

CRT
FLIGHT PHASE KEYS (3)

ANNUNCIATORS
CONTROL DISPLAY UNIT


AUTOFLIGHT STATUS ANNUNCIATOR FMC SOURCE SELECT SWITCH

 

Flight Management Computer System Component Location
Figure 1 (Sheet 2)

C88913
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DUAL FMC ú

 34-62-01
 ú CONFIG ú 02 Page 3 ú Nov 15/94

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

ELECTRONIC HORIZONTAL SITUATION INDICATOR (EHSI)
(EXAMPLE)

 

ELECTRONIC FLIGHT INSTRUMENT SYSTEM CONTROL PANEL (EFIS CP)


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

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 34-62-01

 ú CONFIG ú 01 Page 4 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C87471
A 737-300/400/500MAINTENANCE MANUAL
THRUST MODE
ANNUNCIATION

 

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

C87472
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DUAL FMC ú

 34-62-01
 ú CONFIG ú 01 Page 5 ú Nov 15/93

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AUTO MANUAL

SWITCH/ INDICATOR

VHF NAVIGATION CONTROL PANEL
G
VNAV SWITCH/ LNAV SWITCH/ INDICATOR INDICATOR
 
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