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
FDRS - ELECTRONIC EQUIPMENT COMPARTMENT COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
Page 11
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-005
FDAU Status Relay
The FDAU status relay is on the right side of the nose wheel
well on the J24 panel.
FDRS - NOSE WHEEL WELL COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
Page 12
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-033
FDRS - NOSE WHEEL WELL COMPONENT LOCATION
FDRS - NOSE WHEEL WELL COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
Page 13
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-033
Transmitter Locations
The tail area has these transmitters that have an interface with
the FDRS:
* Rudder position transmitter
* Left and right elevator position transmitters.
The rudder pedal force transducer is located in the horizontal
stabilizer and has an interface with the FDRS.
The left and right aileron position transmitters in the wings have
an interface with the FDRS.
Position Sensor Locations
The control column (2), control wheel (2), and rudder pedal (1)
sensors are in the forward equipment center under the flight
compartment floor.
The stabilizer position A sensor is in the tailcone adjacent to the
elevator feel and centering unit.
Accelerometer
The three-axis accelerometer is on the forward side of the right
wheel well.
FDRS - AIRPLANE COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
Page 14
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-004
FDRS - AIRPLANE COMPONENT LOCATION
FDRS - AIRPLANE COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
Page 15
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-004
FDR Location
The flight data recorder (FDR) is in the aft cabin overhead.
Access is through a hinged ceiling panel.
FDRS - AFT CABIN COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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
31-31-00-006
FDRS - AFT CABIN COMPONENT LOCATION
FDRS - AFT CABIN COMPONENT LOCATION
EFFECTIVITY
SHZ ALL 31-31-00
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
31-31-00-006
THIS PAGE IS INTENTIONALLY LEFT BLANK
FDRS - AFT CABIN COMPONENT LOCATION
31-31-00
Page 18
D633A101-SHZ1 Oct 10/2002
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
General
The flight data recorder system (FDRS) collects, formats, and
stores digital, discrete, and analog data. The FDR gets 115v ac
power from the P18 circuit breaker panel.
Power Input
These components get 28v dc power:
* FDAU status relay
* Flight recorder test module
* FDR fault logic.
115v ac goes through a system test plug to the flight data
acquisition unit. 115v ac also goes to a relay in the flight
recorder/mach airspeed warning panel to turn on the FDR. 26v
ac goes to the FDAU for reference voltage for the FDRS
sensors.
FDAU Status Relay
The FDAU status relay controls the flight recorder OFF light.
Normally, the FDAU BITE out signal causes the FDAU status
relay to energize. This removes the ground from the flight
recorder OFF light and it goes out. If the FDAU finds a fault, the
BITE out signal removes the ground from the FDAU status relay.
A ground connects to the flight recorder OFF light and the flight
recorder light comes on.
Flight Recorder/Mach Airspeed Warning Test Module
The flight recorder/mach airspeed warning test module has an
OFF light and a TEST/NORMAL switch. The flight recorder OFF
light comes on when one of these conditions occurs:
* Airplane is on the ground and both engines are off
* FDAU status relay is not energized because of a fault
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737NGAMM2(32)
