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P61 panel.
ADIRS - COMPONENT LOCATION - IRS MASTER CAUTION UNIT
EFFECTIVITY
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ADIRS - COMPONENT LOCATION - IRS MASTER CAUTION UNIT
ADIRS - COMPONENT LOCATION - IRS MASTER CAUTION UNIT
EFFECTIVITY
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General
These are the ADIRS components in the electronic equipment
(EE) compartment:
* Left air data inertial reference unit (ADIRU)
* Right ADIRU.
ADIRS - COMPONENT LOCATION - EE COMPARTMENT
EFFECTIVITY
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ADIRS - COMPONENT LOCATION - EE COMPARTMENT
ADIRS - COMPONENT LOCATION - EE COMPARTMENT
EFFECTIVITY
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General
The pitot pressure air data modules (ADM) are in the forward
equipment compartment.
ADIRS - COMPONENT LOCATION - PITOT AIR DATA MODULES
EFFECTIVITY
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ADIRS - COMPONENT LOCATION - PITOT AIR DATA MODULES
ADIRS - COMPONENT LOCATION - PITOT AIR DATA MODULES
EFFECTIVITY
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General
The static pressure ADMs are in the forward cargo
compartment, above the ceiling panels.
ADIRS - COMPONENT LOCATION - STATIC AIR DATA MODULES
EFFECTIVITY
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ADIRS - COMPONENT LOCATION - STATIC AIR DATA MODULES
ADIRS - COMPONENT LOCATION - STATIC AIR DATA MODULES
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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General
The angle of attack (AOA) sensors are on both sides of the
fuselage. The total air temperature (TAT) probe is on the left
side.
ADIRS - COMPONENT LOCATION - AOA SENSORS AND TAT PROBE
EFFECTIVITY
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ADIRS - COMPONENT LOCATION - AOA SENSORS AND TAT PROBE
ADIRS - COMPONENT LOCATION - AOA SENSORS AND TAT PROBE
EFFECTIVITY
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ADIRU
The ADIRU operates with 115v ac or 28v dc. 115v ac is the
normal power source.
Each ADIRU has a separate ac and dc power source. The left
ADIRU gets power from these buses:
* 115v ac stby bus
* 28v dc sw hot battery bus.
The right ADIRU gets power from these buses:
* 115v ac xfr bus 2
* 28v dc sw hot battery bus.
AC Reference Voltage
The 28v ac stby bus supplies a servo reference voltage to the
left ADIRU and to the left angle of attack (AOA) sensor. The 28v
ac xfr bus 2 supplies servo reference voltage to the right ADIRU
and to the right AOA sensor.
Integrated Flight Systems Accessory Unit
The integrated flight systems accessory unit (IFSAU) gets ac
power from the 115v ac xfr bus 2. DC power comes from the 28v
dc sw hot bat bus. The IFSAU uses these inputs to control power
going to the right ADIRU and to supply power to the crew call
horn when the ADIRUs operate with dc power on the ground.
Air Data Modules
The left ADIRU supplies 13.5v dc to the left pitot ADM and to the
　
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