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
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-11-00-004
Primary Static Drain Fittings
The drain fittings in the captain and first officer static lines are in
the forward cargo compartment along the left side of the
airplane. You must remove an access panel to get to the drain
fittings.
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - FORWARD CARGO COMPARTMENT
EFFECTIVITY
SHZ ALL 34-11-00
Page 10
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-11-00-005
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - FORWARD CARGO COMPARTMENT
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - FORWARD CARGO COMPARTMENT
EFFECTIVITY
SHZ ALL 34-11-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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
34-11-00-005
Pitot Probe Location
The airplane has three pitot probes. The captain pitot probe is
on the left side of the airplane. The first officer and the auxiliary
pitot probes are on the right side of the airplane.
Static Port Location
The airplane has six static ports. There is a captain, first officer,
and an alternate static port on each side of the airplane.
Alternate Static Ports Location
The airplane has two alternate static ports. There is one port on
each side of the airplane.
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - EXTERNAL
EFFECTIVITY
SHZ ALL 34-11-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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
34-11-00-006
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - EXTERNAL
STATIC AND TOTAL AIR PRESSURE SYSTEM - COMPONENT LOCATION - EXTERNAL
EFFECTIVITY
SHZ ALL 34-11-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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
34-11-00-006
ARINC 429 Data
These items send air pressure through pneumatic lines to the
ADMs:
* Captain pitot probe
* First officer pitot probe
* Captain static ports
* First officer static ports.
The length of the pressure lines and the number of connectors
are a minimum.
The left and right static ports are connected together. This gives
an average ambient air pressure to the ADMs.
Pressure Lines
The pressure lines from the auxiliary pitot probe and the
alternate static ports go to the standby altimeter/airspeed
indicator. The pressure lines from the alternate static ports also
go to the cabin differential pressure indicator.
The alternate static ports are connected together to give
average ambient pressure.
Drain Fittings
Each static line has a drain fitting. The captain and first officer
pitot lines also have drain fittings.
The auxiliary pitot line does not have a drain fitting. The probe is
at the lowest part of the line so moisture can drain from the
probe.
STATIC AND TOTAL AIR PRESSURE SYSTEM - INTERFACE AND FUNCTIONAL DESCRIPTION
EFFECTIVITY
SHZ ALL 34-11-00
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
34-11-00-007
STATIC AND TOTAL AIR PRESSURE SYSTEM - INTERFACE AND FUNCTIONAL DESCRIPTION
STATIC AND TOTAL AIR PRESSURE SYSTEM - INTERFACE AND FUNCTIONAL DESCRIPTION
EFFECTIVITY
SHZ ALL 34-11-00
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
34-11-00-007
General
The pitot probe measures pitot air pressure.
Physical Description
The pitot probe port points forward to measure pitot pressure. A
strut moves the probe several inches from the airplane skin to
decrease airflow turbulence effects. A base plate contains the
electrical and pressure connectors. A gasket is between the
probe base and the airplane structure to form a pressure seal.
An anti-icing heater is in the probe to prevent ice. The heater is
attached to the electrical connector in the base plate.
STATIC AND TOTAL AIR PRESSURE SYSTEM - PITOT PROBE
EFFECTIVITY
SHZ ALL 34-11-00
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737NGAMM2(117)
