曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
bulkhead in the tail cone.
Stabilizer position sensor B is on the right side of the elevator
feel and centering unit. It shows on the graphic. Stabilizer
position sensor A is on the left side of the elevator feel and
centering unit and is not shown.
The mach trim actuator is on top of the elevator feel and
centering unit.
The neutral shift sensor is on the right side of the elevator feel
and centering unit.
Training Information Point
When you install the neutral shift sensor, follow the instructions
in this caution.
CAUTION: PUT THE CRANK ARM IN THE CORRECT UP
DIRECTION. THE CRANK ARM NOT IN THE
CORRECT UP DIRECTION CAN CAUSE DAMAGE
TO EQUIPMENT.
DFCS - TAILCONE COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 22-11-00
Page 16
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-005
DFCS - TAILCONE COMPONENT LOCATION
DFCS - TAILCONE COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 22-11-00
Page 17
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-005
Lower Control Column Component Locations
The captain’s and first officer’s pitch CWS force transducers are
between the support and the forward quadrants on the torque
tube. The torque tube is between the captain’s and first officer’s
control column.
The roll CWS force transducer is below the captain’s control
column.
DFCS - FORWARD EQUIPMENT COMPARTMENT COMPONENT LOCATIONS
EFFECTIVITY
SHZ ALL 22-11-00
Page 18
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-006
DFCS - FORWARD EQUIPMENT COMPARTMENT COMPONENT LOCATIONS
DFCS - FORWARD EQUIPMENT COMPARTMENT COMPONENT LOCATIONS
EFFECTIVITY
SHZ ALL 22-11-00
Page 19
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-006
Wheel Well Component Locations
The autopilot aileron actuators for systems A and B are in the
main gear wheel well. They are on a support bracket on the left
forward wall of the wheel well.
The aileron position sensor is on the forward wall of the main
wheel well. It is between the autopilot aileron actuators and the
aileron power control units (PCUs).
DFCS - WHEEL WELL COMPONENT LOCATIONS
EFFECTIVITY
SHZ ALL 22-11-00
Page 20
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-007
DFCS - WHEEL WELL COMPONENT LOCATIONS
DFCS - WHEEL WELL COMPONENT LOCATIONS
EFFECTIVITY
SHZ ALL 22-11-00
Page 21
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-007
Spoiler Position Sensors Component Locations
The spoiler position sensors are on the rear wing spars. The
spoiler 4 position sensor is on the left wing below spoiler 4. The
spoiler 9 position sensor is on the right wing below spoiler 9.
DFCS - WING COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 22-11-00
Page 22
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-008
DFCS - WING COMPONENT LOCATION
DFCS - WING COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 22-11-00
Page 23
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-11-00-008
General
There are several circuit breakers that supply power to the flight
control computers (FCC). Much of the power goes through other
switches and circuits before the FCCs.
Training Information Point
It is possible that a valid FCC could fail the power-up test if
some of the circuit breakers are not closed in the correct
sequence. If the AFCS A(B) FCC DC circuit breaker is closed
before the AFDS MCP DC 1(2) circuit breaker, the FCC may do
an in-air power up. The FCC may fail to power up successfully
under this condition.
Therefore, the best procedure to apply power to the DFCS
system after maintenance is to close the AFCS A(B) FCC DC
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737NGAMM1(12)
