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
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
34-62-01
AND A SINGLE FMC ú CONFIG 1 ú 04 Page 4 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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
34-62-01
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
34-62-01
AND A SINGLE FMC ú CONFIG 1 ú 05 Page 7 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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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本文链接地址：737-300 400 500 AMM 飞机维护手册 导航 NAVIGATION 5(27)
