OFF MAX
VREF
SOURCE CONTROL PANEL
RESET
MFD
AUTO
RTO
BOTHBOTHALL ALL
ANTI SKID
RATE
ON 2ON 1
ENG SYS
ON 1 ON 2
ANTI SKID
INOP
USED
NORMAL
DU (6)
ENGINE DISPLAY DISPLAY SOURCE CONTROL PANEL SELECTORS
COAXIAL COUPLER (4)
ARINC 429 OUTPUT BUSESAIRPLANE SYSTEMS
AIRPLANE SYSTEMS DISCRETES
DISPLAY ELECTRONICS UNIT (2)
CDS - GENERAL DESCRIPTION
- 243 -
31-62-00
737-600/700/800/900 TRAINING MANUAL
CDS -- FLIGHT COMPARTMENT COMPONENT LOCATION - 1 Component location
These are the CDS components in the flight compartment:
-Left outboard DU
-Left inboard DU
-Right outboard DU
-Right inboard DU
-Upper center DU
-Lower center DU
-Captain EFIS control panel
-First officer EFIS control panel
-Captain display select panel
-First officer display select panel
-Engine display control panel
-Left remote light sensor
-Right remote light sensor
-Captain brightness controls
-First officer brightness controls
-Display source selectors.
The flight management computer system control display units (CDU) show CDS BITE data.
31-62-00
737-600/700/800/900 TRAINING MANUAL
31-62-00-003 Rev 1 01/16/1999
P5 FORWARD OVERHEAD PANEL
-DISPLAY SOURCE SELECTORS
P2 CENTER INSTRUMENT PANELP7 GLARESHIELD PANEL - ENGINE DISPLAY CONTROL PANEL
-EFIS CONTROL PANELS -UPPER CENTER DU
P3 F/O INSTRUMENT PANELP1 CAPT INSTRUMENT PANEL -F/O DISPLAY SELECT PANEL -CAPT DISPLAY SELECT PANEL
-
LEFT INBOARD DU - RIGHT INBOARD DU
-RIGHT OUTBOARD DU
-
LEFT OUTBOARD DU
-F/O BRIGHTNESS CONTROLS CONTROLS -CAPT BRIGHTNESS P9 FORWARD ELECTRONICS PANEL
-LOWER CENTER DU
-RIGHT CDU
-LEFT CDUCDS - FLIGHT COMPARTMENT COMPONENT LOCATION - 1
31-62-00
737-600/700/800/900 TRAINING MANUAL CDS -- FLIGHT COMPARTMENT COMPONENT LOCATION - 2 Coax Couplers
There are four coax couplers. Coax couplers 1 and 3 are to the right of the captain rudder pedals. Coax couplers 2 and 4 are to the left of the first officer rudder pedals.
To get access to the coax couplers, remove the access panel on the inboard side of the rudder pedals and remove the flight management computer (FMC) control display unit (CDU). If necessary, remove the pilot seat. You can now disconnect the coaxial connectors and remove the coupler bracket. The coax couplers are on the bracket.
The coaxial connectors have a spring loaded sleeve that locks the connector to the coupler. You pull the sleeve back to attach or remove the connector to the coupler.
31-62-00
737-600/700/800/900 TRAINING MANUAL
31-62-00-004 Rev 1 01/16/1999
CAPT RIGHT
RUDDER PEDAL (REF)
COAX COUPLERS
1 AND 3
ACCESS PANEL
REMOVED (REF)
COUPLER INSTALLATION
WIRE ACCESS PANEL REMOVED
FWD
ACCESS PANEL
REMOVED (REF)
FWD
COUPLER REMOVAL AND COUPLER BRACKET REMOVAL
FWD
COUPLER WIRES
(LEFT SIDE SHOWN)
CDS - FLIGHT COMPARTMENT COMPONENT LOCATION - 2
- 247 -
31-62-00
737-600/700/800/900 TRAINING MANUAL CDS -- FLIGHT COMPARTMENT COMPONENT LOCATION - 3 Remote Light Sensors
The remote light sensors are on the forward part of the glareshield. The sensors face forward.
31-62-00
737-600/700/800/900 TRAINING MANUAL
31-62-00-005 Rev 1 01/16/1999
REMOTE LIGHT SENSORS
GLARESHIELD CDS - FLIGHT COMPARTMENT COMPONENT LOCATION - 3
- 249 -
31-62-00
737-600/700/800/900 TRAINING MANUAL CDS -- EE COMPARTMENT COMPONENT LOCATION EE Compartment
The display electronics units (DEUs) are on the E3-1 shelf.
31-62-00
737-600/700/800/900 TRAINING MANUAL
31-62-00-006 Rev 1 10/13/1998
E3-1
-
DEU 2
-
DEU 1
EE COMPARTMENT (LOOKING AFT)
CDS - EE COMPARTMENT COMPONENT LOCATION
- 251 -
31-62-00
CDS -- POWER INTERFACES Power
The 28v dc standby bus supplies power to these components:
-Left outboard display unit
-Upper center display unit
-Captain EFIS control panel
-Display electronics unit (DEU) 1.
The 28v dc bus 1 supplies power to the left inboard display unit.
The 28v dc bus 2 supplies power to these components:
-Right outboard display unit
-Right inboard display unit
-Lower center display unit
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600/700/800/900培訓手冊 TRAINING MANUAL 2(2)
